EFTA01326217

MAJOR REPAIR AND ALTERATION USOwarteen haniiponiu,. or (Airframe, Powerplant, Propeller, or Appliance) . rent Amp. mimmiratim Ord to 2120<<20 Ed tr31 ICI B Electron Track ng Eiveitet For FAA Use Only INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9, Pan 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penally for each such violation. (49 U.S.C. §46301(a)) I. Aircraft Naeorekty end Registration Mark! N120JE Setter NI: 10aS Make. GULFSTREAM Model! OW Sykes: WA 2. Owner Name (As shown on reoisration cerlificare) JEGE LLC Address (As shown on reoistratiOn cortittafe) Ad*a.a: MOO RED R.304 DARTER 03 Oty ST. TMOWS SW. CORDON Sc 00002 go.roy VIRGIN MINOS 3. For FM Use Only • 4. Type & Unit Identification Regsr Meseta. UM Make Model Sorel Number O 0 AIRFRAME (As descnbed if teem I abOYO) • O POWERPLANT o O PROPELLER El . APPLIANCE 1taa wituraceser S. Conformity Statement A. Annoys Name and Address B. K nd 01Agency Name Stevens AdItC4p8O• Ma Delostir System. SC se 103 Ent Din City Mow Sum GoOrom Sc St2te Coeds United &Stela Amente a U.S. Certificated Mechanic 0 Manacturer O Foreign Certificated Mechant C. Cent-ante No. 0 Certificated Repak Swam VIB8368K O Careficated Maintenance Organdatcn 0. 1i:entry dal the repair erclror alteration made kr tie unti(.) 'denoted In item 5 above and OW..nbild on the reverse or aeactrnents hereto new been nestle In accordance with die rettirements of Pant) 430! the US. Federal Anton Regulatans and that the Intrinabon Ravished herein is true and correct iti tie best of my knowtedge. Extended rarqe Fuel Per 14CFR Pan 43 App. B O Sionstvernate of &Shafted kedual Mike Shaw , • June 03, 2019 . —7 , 4.1141 7. Approval fof cum to Service Pursuant to the autharity green persons specified below. the twit Identified in item AdminIStrator el the Federal Adidas Adrnindliaten ard IS 0 APPROVED 5 was . irepected n tie manner peSSOIbed by the REACTED BY FM FP Standards Manufacturer Maintenne Orgarizaban Person APING'S by Canadian inspect& Department of Transport FM D esignee X Repair Stamm Inspecton Aulltarizettm Otter (50900.7 Carthate Of Oesqnsuco No. CRS$ VII18388K Signature/Date of ALthonzed IntS4dual Dendall Wood iatAuttlat w6 09.0 June 03.2019 FM Form 337 oo-om SDNY_Glil_02753702 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240624 EFTA01326217 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An a,Yeration must be cornpabble with all previous atterahons ro assure continued conformity with the applicable airworthiness requirement& 8. Description of Work Accomplished (If more space Is required, attach additional sheets. Identify with se-craft nationakly and registration mark and date work completed.) N120JE Nationality and Registration Mark KaiserAir, Inc STC ST03422CH June 03-2019 Dale 1. Installed KalserAt, Inc. SIC ST03422CH - by installation of a Universal Avionics UNS•I Espw flight management system oath Unlink UL•801 datalink system and CVR-120A cockpit voice recorder to meet airworthiness requirements for FANSUA+ and optional Automatic Surveillance — Broadcast (ADS-B) Out in accordance with Master Data List. Document No. JRW1279-MDL. Revision A dated October 26. 2018 or later FAA approved revision. 2. The following FM approved Flight Manual Supplements: Universal Avionics Systems Corporation CVR-120A Codtpit Voice Recorder. Document No. JRW1280.FMS-01, Revision A. dated May 25. 2015. Automatic Dependent Surveillance Broadcast Out (ADS-B Out). Document No. JRW1260-FMS-03, Revision A. dated October 06. 2015. Universal Avionics UNS•tEspw FMS and UL• 801 Unlink Datalink Communication System, Document No. JRW1280-FMS-04. Revision IR. dated October 30. 2018 and the Unvemal Avionics Corporation CVR Operation Report No. 23-70-08-01, Rev. 2. Dated March 10. 2016. has been inserted Into the Aircraft Flight Manual. 3. Instructions for Continued Airworthiness Document No. JRW1283-ICA Revision E. Appendix A Svu E. dated June 18. 2018 has been inserted into the Customer's Supplemental Maintenance Manual. FM 8110-3 Approvals: Iridium Antenna Instalati08 FM 8110.3 • CI 490-490 indium Antenna Doubler Design B Inslalabon, Identification No. N120JE-052310-1-ECNOI. Revision N/C. dated May 23.2019 and Damage Tolerance Analysis for the Gulfstream Cy-IV CI 490-490 Iridium Antenna Doubler Insulation, Repot No. N120JE-052319-OT01, Revision N/C. dated May 23. 2019. Approved by FM Structures DERT-605818.NAL Trevor J. Sarong. Instructions for Continued Airworthiness Document No. N120JE-ICAW-052319, Revision IR. dated May 23. 2019 LED Cabin Effects Liohting FM 8110-3 - installed direct replacement LEO Caton Lighting. Identification No. Drawing No. 06-328-W03 Rev IR pages 1.9. dated May 30. 2019. Approved by FM Systems & Equipment DERT-832582-CE. Michael Casper. VHF/Comm Antenna Installation and LH Mfd Foul**. Feadthru Installation FM 81101- VHF/Communication Antenna Installation. Drawing No. 06-560-001. Revision IR. dated May 16.2019 and LH Feed•thru installation 06-560-002, revision IR. dated May 23. 2019. Approved by FM Structures DERT-605818-Mil. Trevor J. Strong. 'es Performed aircraft reweigh. updated Equipment List and inserted data into the Weight 8. Balance Manual and Flight Manual as required. FAA-8110-3 and dramngs have been inserted into the Stevens Aerospace. Customer's Supplemental Maintenance Manual. ENO cg Additional Sheets Are Attached FM Form 337 110-06) SDNY_GM_02753703 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240625 EFTA01326218 KAISERAIR, May 14, 2019 Letter Of Authorization KaiserAir, Inc. authorizes Stevens Aerospace and Defense Systems LLC the one time use of KaiserAir, Inc STC ST03422CH for the installation of Universal Flight Management System, Unilink and CVR for the requirements for FANS In Guifstream Model IV Serial Number 1085 current Tail Number N120JE. AndreaJtujan Chief Inspector KaiserAir, Inc. 2240 Airport Blvd. Santa Rosa. CA. 95492 707.528.7400 SDNY_GM_02753704 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240626 EFTA01326219 SDNY_GM_02753705 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240627 EFTA01326220 numb Shan of America Ptparhttent of tgrausportntion — Acbcral Attention Abittinistration Supplemental Zgpe Certificate AGnien, ST03422CH .Y/ti fly/Awn KaiserAir, Inc. 8735 Emhart Road Oakland, CA 946214547 rent//J 441.44,doer e:s ensi4.../ewhet /-14-wsillys-siwy/wvat averaieh.d rowirebierboo4 //muter frJ 4aareleadaCarytva ~NJ de reterreete:ionw private-Si 1:4e/ 25 r/46 Federal Aviation .W.cownchb..4. (See Page 3 of 4 for complete certification basis) /1;yjyafcci:Oww4w/. • .-3,2,y ely/Awn v Wwweer.• Al2EA Oulfstraan 04V. GV CerlierOdeava 1.4*.iowe P.r.ifivor Installation of a Universal Avionics C/NS-IDPW night management system "WI UnilAnk UL-1501datalink system and CVR-120A cockpit voice record".to moat aim:inhalant requirements for FANS 1/A+ and optional Automatic Depaulan Surveillana — Broadassi (ADS-3) Oct in accordance with KaiscrAir, Inc. Master Dula List JR9/1279-MDL. Revision J, dated October 30.2018. or later FAA approved revision. Vatenthe/tiva owegveativaa: 1. The installa must determine nib:Ilia this design change is compatible with previoirdy approved modifications. 2. FAA approved Hight Manual Supplements, KaiscrAir, Inc. !bemoan No. JRW 1280-FMS-0 I RevisMn A, approved May 25, 2015, JRW I280-FMS-02. Revision B. anwoval Octoba 6, 2015. JRW 12804MS-03, Revision A dated October 6, 2015 and JRW 12804-MS414, Revision -. dated Octoba 30. 2018 or later FAA approved revisions me required onboard the modified aircraft 3. The modified aircraft must be maintained in Accordance with Ainvorthinois Limitations containedin KairerAir.'Ine. Document No. JRW1 283-ICA, Chapter 10 0 Airworthiness Limitations. Revision approved October 30, 20 I It, or later FAA approval revision, in addition to the basic aircmft niaintenance manuals. 4.11the holder agrees to permit another person to int this certificate to alts the product, the hoWer must give the other paron written evidence of that pimnbsion. arronwayt snide 4.yerretiese AA, evf he a. I p, A, 4440nweeir fir Werbeehrite Josavvmdarei mawavoini: errnevire or Arneriteehave .4,4 r Arebrib ouleinatin," /dr •Alaimaivaillow/or .Zialetv/. Zivie/navo . tefitraidasalaira. late Vor,r4;whiv. :July23.2014. Jamey 27. 2015 Vark et:maaaanry• :WWI 03. 2015 lir* wecbavy/.. Vark 'naval May 25. 2015. °ciao 30.20t8 /Ay" r//4. Zetintividnv/er Armature) Brenda L. tilditickl ODA Admiiiigralor ElflOy Aerospace. LIZ OCA431240-CE Aar afopiat too et iris aaa• It!.?.,. 1, itsnirbrd• ay a fib of b. brridler ropirioonset not onallag 1 bars, or tot". TM raw PAGI I at I PARS Ibis .vat/lean ay b canasta In better* with ratt ZI.47. SDNY_Glvl_02753706 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240628 EFTA01326221 SDNY_GM_02753707 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240629 EFTA01326222 ltnite Stoke of Aumito pepa r bumf of transportation - Adorn( A0 butitt ist t ion Suppletztental type ffertifirate Mantinuation Ailed) ...441t/10,170 ST03422CH firok rAZatoovor: March 03, 2015 %eft smov4, May 25, 2015 miww4./ October 30, 2018 eitAwlint .92w4: The certification basis for the changed Gulfstream G4 V aircraft as described in this certificate is as follows: a. The type certification basis for Gulfstrenm G4V ninslanes is shown on TCDS Al2EA for parts not changed or not affected by the change. b. The certification basis for parts changed or affected In the change since the reference dai of application, July 23, 2014, is shown on TCDS Al2EA. In addition. the npphcant has complied with 14 CFR Part 25 as specified in the sections listed below. Regulations as shown on TCDS Al2EA [Amendment 25-0 through 25-56i: 25.301(a), (b); 25.303; 25.305(a), (b); 25.307(a); 25.341(a); 25.365(a), (b), (O, (d); 25.561(e); 25.581(a), (b), (e); 25.601: 25.60300. (b). (a); 25.606(a); 25609(a). (b): 25.611; 25.613(a). (b). (d): 25.615(a); 25.619(a), (b). (c); 25.625(a). 25.771(a); 25.777(a), (e); 25.789(a); 25.1301(a), (b), (o), (d); 25.1309(a), (b), (e), (d), (a), (g); 25.1322(a), 0O, (e). (d); ;5.1333(a). (b), (c): 25.1353(a), (b); 25.1357(a), (e); 25.1431(a), (b), (e); 25.1501(a), (b); 25.1523(n), (b); 25.1529; 25.1585(a), (b). Regulations at a later amendment level than specified In TCDS Al2EA: 23.29 [Am& 25.721; 2.5.571(a). (b) [Arndt 25-45j; 25.86900(4) [Arndt 25.1131; 25.1307(e) [Arndt 25-721; 25.1329(e), (i) [Arndt 25.1191: 25.1351(a) [Muth 25.721: 25.138100, (b) (Amdt 25-72); 25.1457(a), (b), (c), (d)(1)0),(2),(3).(6), (e), (g) 'Arndt 25-124); 25.1581(a), (b), (d)(Amdt 25-72), 25.1583(h) (Am& 23-72). Spotlit Conditions 25-665-SC, Special Conditions: Gulfstream Aerospace Cotpomtion, Model GV-SP Airplane; Non-Rechargeable Lithium Battery Installations, Docket No. FAA-2017-0367 (Applicability Limited to Universal Avionics UNS- 'Espy Flight Management System installed in Configurations -04 and -05). The certification basis for the changed Gulfstream GV aircraft as described in Ibis certificate is as follows: a. The type certification basis for Gulfstream GV airplanes is shown on TCDS Al2EA for pans not changed or not affected by the change. b. The certification basis for pans changed or affected by the change since the reference date of application. January 27, 2015, is shown on TCDS AI2EA. In addition, the applicant has complied with 14 CFR Pad 25 as specified in the sections listed below. (Continued on µage 4) Any eltorotion of this artlelooco Is panish.41* by • has of eat Oireupelaf $1.000. or trivisaist Inc Inroatizoo 3 rues, w Cerra. DA Tam 0110.:.1(30.4,) IASI 3 of I PAGES This corcltleat• wy b• troduncroci Zr. 110741tifill,W ZAR 21.47. SDNY_GM_02783708 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240630 EFTA01326223 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SDNY_GM_02753709 15, and 17 I EFTA_00240631 EFTA01326224 %Whit *Ws of pAmerita !apartment of ggranspo dation - eberati Ablation Abministration $upplementui Zgpe Certificate (Continuation Alpe° Verk r/f:"MeMet: March 03, 2015 %ter- 07.4.:4;44se May 25, 2015 rink ittivowtf./ October 30, 2018 en.e0;w4;34 • 4.4.46rvi/4w”.9.- Regulations as shown oa TCDS Al2EA 'Amendment 254 through 25411: 25.29; 2$.301(a), (b); 25.303; 25.305(a). (b); 25.307(a); 25.341(a); 25.365(x), (b), (c), (d); 25.561(e), (d); 25.571(a), (b); 25.581(a), (b), (e); 25.601; 25.603(a), (b). (a); 25.60500; 25.60900. (b); 25.611; 25.613(a), (b), (c), (d); 25.610(a). (b), (c); 2362500: 2527100; 25177(4 (a); 25.789(a); 25.1301(a), (b) K2 (d); 25.1307(c); 25.1309(0), (b), (e), (d), (e), (0, (g% 25.B16(b), (a); 25.1322(a), (6), (e). (d); 25.1333(4 (b), (o); 25.1351(a); 25.135300. (b); 25.1357(a), (a); 25.138100, (b); 25.1431(a), (b), (c); 25.1501(a), (b); 25.1523(o), (b); 25.1529; 25.1581(o), (b), (d); 25.158309; 25.1585(a), (b). Regulations at a later amendment level than specified In TCDS A l2EA: 25.869(ng4) [Am& 25.113); 25.1329(c), (i) (Arndt 25.1191: 25.1457(a), 00, (c), (d)(IX0,(2),(3).(6), (a), (0, (g) [Arndt 25-124) Special Conditions 25-ANM-I08, Special Conditions; Gulfstream Aerospace Corporation, Model Gulfstream CV, High Altitude Operations. Docket No. NM-112; Paragraphs 1(aXbX4 25465-SC, Special Conditions:. Gul fstream Aerospace Coq/oration, Model GV-SP Airplane, NonIFIechargeabk Lithium Battery Installations. Picket No. FAA-20I7-0367. (Applicability Limited to Universal Avionics UNS￾lEspw Flight Management System installed in Configurations 44 and .05). —END-- My ****** tam of ells cortlelomo L puelaluebe by • tine or we 114*.enril *Lear or IsprUpon tut esesollag I imam. or both. FM Feu I110-2-10.4•11 Pia 4 of 4 Pal This corn/lost* ,say to trossferrod Is *mordant Ida yet 11.0. SDNY_GM_02753710 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240632 EFTA01326225 SDNY_GM_02753711 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240633 EFTA01326226 0 US Dremnort MAJOR REPAIR AND ALTERATION e Ting:futon (Airframe, Powerplant, Propeller, or Appliance) &woe esaotion Ads1risibton feeteme e 21100010 wagon Eliontne crew, ream sot eiliA uneasy INSTRUCTIONS hull or type as entries. See Title 14 CFR §43.9. Part 43 Appendix 8. and AC 4194 (or subsequent foremen thereof) for instructions and disposition of this form This report is required by law (49 U.S.C. §44701). Failure to report can road? in a ovil penaky for each such violation. (49 U.S.0 §46301(a)) 1. Aircraft Nationality and Registration Mark N120JE Serial No. 1085 Make Gulfstream Aerospace Model G-IV Sores a. Owner Name (As shown on regostraDon certificate) JEGE LLC Address (As Shown on registration carnivore) Morin 6100 RED HOOK QUARTER 83 cry St. Thomas sm. Foreign be 00802 cage, Virgin Islands 3. For FAA Use Only 4. Type 6. Unk Identlfkatifin Repair AllefillIOn Unit Make Model Serial NO. al 0 AIRFRAME (As CIOSChbed ifl MINI I above) 0 ID POWERPLAt4T 0 0 PROPELLER 0 0 APPLIANCE Type Alenutectiger I. Conformity Statement A. Agency's Name and Address B Kind of AgenCy isms Gunstream Aerospace Services COrpOration U S Collated Mecherie I laerulacturer &Ss 7 Char Drive Fetal:, Centagel Methane C. Certificate No. cie Westfield am MA i Coble: al Repair Sieben be 01085 own, USA Cans:sew maintenance Organs/bon LEGRO39G D. I candy that he repair andlor alteration made to the unit( ) identified in item S above and described on the reverse or attachments hereto have been made in accordance with the requiremee4s of Pan 43 of the U.S. Federal Aviation Regulations and that the information Nmished herein is true and cared to the best of my knowledge. re Extended range fuel Per 14 CFR Pin 43 0 APP. 8 Signature/0mo of Authorized Intkviduat , Benjamin Thomas Jones z .....4—.... -- 09 November 2018 7. Approval fo Wurn to Se Pursue I to the authority given persons &Pealed below, the unit identified in item 5 was nseecteo in the manner presorted by Me Administrator of the Federal Aviation Administration and is 2 Approved 0 Rejected BY FAA Flt Standards Inspect« Maintenance Organization Persons Appeared by Canavan Department or Transport FM Designee I Repair Station Inspection Au cation Other (Specify) Corti ale Of Designation No. LEGRO39G Signature/Date of Aumon 1101 Dean Mathew Dickman c.... --09_November 2018 FAA Fenn 3370041i SDNY _ GM_ 02753712 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240634 EFTA01326227 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be Compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished Minor° space is ragweed attach addrional shears Idenlify min soccer nahonabty and regOkation mark and dale work comaierca) N120JE 159 November 2018 Nationale),and Registration Mark Date Performed Major Repair to the Forward Lower Side of the Baggage Door in accordance with 1159RD13459-3 and Forward Upper Side of the Baggage Door in accordance with 1159RDB459.5 Standard Repair Intl - Frame Cracks. Baggage Door. Gulfstream Standard Repair Drawing 1159RDB459 Rev. J is FAA Approved per Gulfstream GIV SRM 52-00-02 Rev. 16 Dated December 15. 2017 and Engineenng Disposition 50019580.1.1 by Stephen Alois Dated November 7, 2018. This Repair Does Not Impact Aircraft Weight and Balance or the ICA. END Additional Sheets Are Attached FAA Fenn 137 (Wai SDNY_GM_02753713 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240635 EFTA01326228 ee us oftwonn MAJOR REPAIR AND ALTERATION et Orntoenol on (Airframe, Powerplant. Propeller, or Appliance) Federal Aviation winawasten 14/....,77703 core 2.21/2011 Eleceobc Weeny Nun. erFAA UN Only INSTRUCTIONS: Pnnt or type all entnes. See Tele 14 CFR $43.9. Parl 43 APperdix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is requred by law (49 V.S.C. $44701). Fatale report can resiA in a civil penalty for each such holabcn. (49 U S C §46301(a)) 1. Aircraft Nationality and NegntrabOn Mark N120JE Serer No. 1085 Make GULFSTREAM AEROSPACE Model G-IV Senes N/A t. Owner Name (As shown on teolfration cerflficate) JEGE LW Address (As shown on/migration contralto) Meese 8100 RED HOOK QUARTER 83 G., ST THOMAS sew FOREIGN z,,, 00802 cony VIRGIN ISLANDS 3. For FAA USO 0 ly 4. Type a Unit Identification Repair Alteration Unit Make Model Serial NO. IZI O AIRFRAME (As descnbect in nem 1 above) O O PON£RPLANT El CI PROPELLER O . APPLIANCE Type mraacia, 6 Conformity Statement A. Agency: Name and Address B. Kind of Agency an Galmmargigaenaces ration man. 7 Char Drive u 5 corencesee Mechanic I lAanuhaurer Foreign CerlaCated Mechem C. Certificate No. cq Westfield Sine MA / Cannoties Raper 3NbOn a. 01085 Canty USA Certif.:ad atenterence Organzatan LEGRO39G O. [certify that tne repair and/or aeration made to the unlit ) identified in item 5 above and described on the reverse or attachrnems hereto have been made in accordance with the restatements of Part 43 of the U.S. Federal Aviation Regulahons and that the intortnatson furnished herein is Ina and correct to the heft of my knowledge. Extended range fuel per 14 CFR Part 43 App. B • SignaturerDate of Authorized Ince/ -1 Benjamin T. Jones 26/JUIJ2018 „.,..--t_--_... - . pproval for R talcs Pursuant to the authority given persons specified below. the Linn identified in item 5 was inspected n the manner prescribed by the Administrator of the Federal Aviation Administration and is 2 Approved O Rejected BY FM Fit. Standards inspector manufacturer Maintenance Organization Person, ANNOYS by Censaen orpartmen of Transport FM Designee 1 Repar Station Inspection Authorization Other (Sporty) Certificate or Designation No. LEGRO39G Signature/Date reed indwismil Dean M. Di ___ 26/JUL/2018 FAA Forrn 337 rioter SDNYGM02753714 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240636 EFTA01326229 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued contort* with the applicable einvorthiness requirements. a. Description of Work Accomplished (It more space is required. attach additional sheets. Identify wen aircraft nationality and reetstrabon mark and date work completed.) N120JE Nationality and RegitratiOn Mark 26/JUU2018 Date 1.) Reworked the LH Thrust Reverser P/N 1159P41460-3 S/N A088 LH Fwd Mount Holes 2L - 4L and 7L - 11L. Installed The Following Repair Bushing Part Numbers In Locations Listed; 21. - GSL405420001.11-5474 31. - GSL405420001-11-5312 4L - GSL405420001-11-5474 7L - GSL405420001.11-5312 8L - GSL405420001.11-5940 9L - GSL405420001-11-5312 10L - GSL405420001-11.5940 11L - GSL405420001-11.5312 2.) Reworked the RH Thrust Reverser P/N 1159P41460-4 S/N A088 RH Fwd Mount Holes 3R,7R,13R -10R. Installed The Following Repair Bushing Pan Numbers In Locations Listed; 2R - GSL405420001.11.5746 3R - GSL405420001.11.5320 4R - GSL405420001-11-5781 5R - GSL405420001-11-5322 7R - GSL405420001-11-5312 BR - GSL405420001-11-5946 9R - GSL405420001-11-5312 10R - GSL405420001-11-5754 11R - GSL405420001-11-5312 Repairs Accomplished in Accordance with and Substantiated By Gulfstream General Service Letter GSL405420001 Rev B., Engineering Disposition SC18934.14.9.1.1 and SC18934.16.1.1.1 This Repair Does Not Impact Aircraft Weight And Balance. Or The ICA. 3.) Reworked the LH Inlet P/N 1159P41100-69 S/N A086 LH Fwd Mount Holes 13L. 151. - 20L and 231. - 25L then Installed Repair Bushings PIN GSDD405411001-11 as required. 4.) Reworked the RH Inlet PIN 1159P41100-71 SIN A086 RH Fwd Mount Holes 6R, 12R, 17R - 19R and 24R then Installed Repair Bushings PIN GSDD405411001.11 as required. Repairs Accomplished in Accordance with and Substantiated By Gulfstream General Service Letter GSL405411001 Rev C., Engineering Disposition SC18934.14.10.1.1 and SC18934.16.11.1.1 This Repair Does Not Impact Aircraft Weight And Balance. Or The ICA. END Addnional Sheets Are Attached FAA Form 337 {torn SDNY_GM_02753715 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240637 EFTA01326230 9Ilbf 1 vs oromurer MAJOR REPAIR AND ALTERATION a transponsess (Airframe, Powerplant. Propeller, or Appliance) From Annie, Aantatistration Fr, Amos! pre No 1000020 moon Elena"K Treaing Nuen: .. FAS Use Puy INSTRUCTIONS: Pont or type aN entries. See Tele 14 CFR §43.9. Pan 43 Appendix 8. and AC 43.9.1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 544701). Failure to report can result in a civd penalty for each suCh violation. (49 U.S.C. §46301(a)) 1. Aircraft Nationality and Registration Mark N120JE $erial No. 1085 Make GULFSTREAM AEROSPACE Model G4V N/A 2. Owner Name (As shown on mixers:ion certracate) JEGE LLC Address (As shown on registration certificate' Mann 6100 RED HOOK QUARTER B3 cc, ST THOMAS sm. FOREIGN 20 00802 cowr y VIRGIN ISLANDS 3. For FAA Use Only 4. Type S. Unit Identification Reis* Alteration Unit I Make Model Serial No Z 0 AIRFRAME (As clescncecl on Item 1 above) El • POWERPLANT El • PROPELLER El 0 APPLIANCE type Merestectiew 6. Conformity Sta ernent A. Agency's Name and Address B. Kind of Agen y ere Gulfstream Aerospace Services Corporation u. s. Garlaraterl Meehan I Sran...ackrer Mons 7 Char Drive Foreign Cathcatee Mechanic G Certificate No Ger Westfield Si." MA i Certificated Repair Staten a• LEGR039G 01085 cwwv USA Coreficateo Ulaimenance OrgarCakin O. I certify that the repair andior alteration made to the unit( ) id nofied in item 5 above and described on the reverse or attachments hereto have been made in accordance vett the requirements of Part 43 of the U.S Federal Aviation RegAations and that the information furnished herein is true and Coned to the best of my knowledge. Extended range fuel per 14 CFR Part 43 n00. B El &puha Authorized Indi t min e j - ; ----T---" 26/JUN/2018 7. Approval for Return to Service Pursuant to the authority g ven persons specified below. the unit identified in item 5 Adnwestralor 01 the Federal Aviation Administration and is 9 Approved was IMI -nspected in the manner prescnbed by the Rejected BY FAA Fn. Standards Inspedor Manufacturer MaintenanceOrganization Meintenan Persons Approved by Gainsays Department of Transport FAA Designee I Repair Station Inspection Autnonzation Other (Savory) Ceti Kate or Designation No. LEGR039G Signature/Date of Authorized Individual Wiliam Stucklen 26/JUN/2018 FAA Form 337 norm SDNY_GM_02753716 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O240638 EFTA01326231 NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. I. Description of Work Accomplished (II more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N120JE 26/JUN/2018 Nationality and Registration Mark Date Performed rework of rudder actuator forward attach fitting - F.S. 757.562 in accordance with Gulfstream drawing No. 1159RDB729, No Revision, -901 inst. This major repair is substantiated by FAA form 8100-9. dated 06/15/2018, Project No. TR-07-2018-0014. from Gulfstream Savannah Authorization# ODA-511131-CE. cert 0336099. This repair has no effect on current ICA. Weight and Balance effect: None AFM Supplement: None Performed the following repairs to flight control hinge fittings in accordance with Gulfstream drawing No. SE05000102. Rev. E. STD. Repair - Control Surface Hinge Fittings: 1) Performed repair SE05000102-913D6-20 to UH #3 Aileron hinge fitting P/N 1159WM20202-5. Bore measures .4065", installed 5E05000901-913D6-20 bushing. 2) Performed first increment 0/S repair to UH Aileron #1 hinge holes (3 places). Bores measure .3280". installed NAS6605D4OX. NAS6605D54X, AND NAS6605066X 0/S hardware. 3) Performed repair SE05000102-911P5-21 to UH Elevator hinge #4. Bores measure .3906" - .3911", installed SE05000102-911P5-21 repair sleeve. 4) Performed repair SE05000102-912S88-1 to UN Elevator trim tab hinge# 1 inboard lug. bore measures 3905". installed SE05000102-912588.1 bushing. 5) Performed repair SE05000102-911P2-5 to UH Elevator trim tab hinge# 1 outboard lug, bore measures .4063", installed SE05000102-911P2-5 sleeve. 6) Performed repair SE05000102-911P1-5 to R/H Elevator trim tab hinge# 1 outboard lug, bore measures .3905", installed SE05000102-911P1-5 bushing. 7) Performed repair SE05000102-911P1-5 to R/H Elevator trim tab hinge# 2 outboard lug, bore measures .3905", installed SE05000102-911P1.5 bushing. 8) Performed repair 5E05000102-914P1-28 to Rudder top hinge and fitting. bores measure .389r. installed 5E05000901.914P1-28 bushing. 9) Performed repair SE05000102.914P1-27 to Rudder middle hinge and fitting, bores measure .3898", installed SE05000901.914P1.27 bushing. Et Additional Sheets Are Attached FAA Form 337 i loos) SDNY_GM_02753717 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240639 EFTA01326232 DEPARIWO CR TRASSPC*TAIX.4410IIPLU. AY.A7O.1•ZAI0SSTRAT 1O4 STANDARD AIRWORTHINESS CERTIFICATE polinounams a ists/if Fearempalk N$201 1 OUUSTREMINEM (SAGE MN K••••••21 . tiSileteerna•laillsnois• a SC 114111.••••••• • I es -Owe linsennisini•••• atininte.nto ow in owl•••••••••• 'Mb s ••••••••••••Manlailatermal••• One •INtent••••••••••Ytaii•leeniss • I sow!. Maus revert NONE •••teratem• MOS Maori* 90./00 ROSIV2CCO az:Az, waste Flews, ZarSer2S as, wealle 11•SCOMICATIMST “ClUth/0•11•11A/00// reit,e ~Jig rtptivi sturtrattildratil ••• SDNY_GM_02753718 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240640 test Raw. EFTA01326233 _ SONY_GA.4_02753719 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 0024064I EFTA01326234 0.40 VS/ I CO illOisca CEPARTMEN1 Of TRANSPORTATION MEWL AVIATOIMMISTRATION STANDARD AIRWORTHINESS CERTIFICATE i alevort op I sntiniCitata NO litCtl I MOW/ KRA& I unwire WSTWO.1100. Walla N212JE Gultatreas G-IV 1085 Tramline t AVICW, MOVISI Twessaim sea maw •••••••14C 6001011.140••••••••••••sto nil DSO /anat. mad Dan leadele YM st= Imintossis ern ant* pep is 0.0moiningapsiOnlialson•Ina innate nem es • plait wits NONE • toms mensal** b1101 bFYKI It 05/23/2000 A.S.S•ppla • Arm minus". 4.* nese. V rwisms• an" henna marital WE MI IPMAPVIIIIJAMPL PIP PallaW06 nal aphigypelpiakki owns mini — —a at ®yeti h. wit Pete. Wel teSOIP.M.5w S019 1.0.• non 4 9141$1,1 SDNY_GM_02753720 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240642 EFTA01326235 SDNY_GM_02753721 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240643 EFTA01326236 to co UNITED STATES OF AMERICA m A pa p H 0 Xl o 1 NATIONALITY AND H REGISTRATION MARKS N120JE DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 2 MANUFACTURER AND MODEL . - ft.. ..;.: GULFSTREAM AEROSPACE-a:IV 3 AIRCRAFT SERIAL NUMBER 1085 4 CATEGORY Transport 5 AUTHORITY AND BASIS FOR ISSUANCE / c:"..-\ ••• - ..„. , . t / • , m This airworthiness certificate is issued pursuant to 49 U.S.C. § 44704 and certifies that, as of the date otissuance, this aircraft has been inspected and found to O conform to its type certificate and be in a condition for safe operation. This aircraft meets the requirementief the applicable airworthiness standards in Annex 8 Civil Xi to the Convention on International Ariabon. except as fellows: CI . i. • 1 ;f t'fl 70 Xl C) 70 6 TERMS AND CONDITIONS LE) NONE ea. Unless sooner surrendered, suspend, revoked, or a termination date is otherwise established by the FAA, this airworthiness certificate is effec ive as long as maintenance, preventative maintenance, and alterations are performed per the applicable FederatAviation Regulations and the. aircraft is registered in the United States. DATE OF ISSUANCE FAA REPRESENTATIVE .10 R 05/23/2000 PZ-L: ag t. cm a Any alteration, misuse, or reproduction of this certificate for a fraudulent purpose may be punishable by certificate revocation, fine, and I or imprisonment UT o THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT PER THE APPLICABLE FEDERAL AVIATION REGULATIONS. ; AA Form 8100.2 (11-2016) Previous Edition Dated 0.4-11 May be Used Until Depleted La, CL Co 1,3 DESIGNATION NUMBEF AEA-FSDO-25 EFTA01326237 VIIONV1)10 Alto VINOHY1)10 Se Tr WEI 6 90U Uhl US NOUNii/S10311 141,210WV V114 HIIA1 031Id SDNY_GM_02753723 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240645 EFTA01326238 co m -o 0 m n 0 m -0 -o 9° 9) E p a) •@, P, ••-•1 • tr • , - UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION . STANDARD AIRWORTHINESS CERTIFICATE , mr,e,m„,I., NC ractorionar Doty N 1 20JE . a IMOSACTU.0 NO Oa ,'...........—• 0," -C ' • GULFSTREAM AE, RDSFACE—G:IV -rinv i e,. . —: : roes 1 7 A • . cartoore Transport / eLs,, ...en. ri ,.. Mt ennnesarteceb b WI Fame faille i "Ma menu Wee annet Si eye ha tan ithAtm eaWV in b le basalts Wide art No Sint telleillitit tor liplcatio inners II Cotten Owe mica skl se zurdn•kne. . b as -wets, a" irinabv Oil sall • law % .... NONE • IteallmOccoarail • • ,.' UMW MOW el lontate. skis is ~So ~ALSO try to FM. Ea suntnar rye.; • entrthepose ands is Seiko bie Wawa al Sett a mm' grey., on pricaned serfs woke* ireplrithissal anion aim nil irre0.10. 1 . asWiwi Stela . WM CI illiatba 80523/2000 OA.etitsemera ' f,, . 0....:I.Alle. PONS AEA.FSDO-25 cajt, •J; • OS.i • AffiNnim eat a twneosio. at IN* was, Poe Wsam Mi ts eing. by ream, motion rm. Ardis Inebsellent ..."-....-....._.,.....-.- DIM CERTIFICATE 41ST IIE OiSPLAYED ti ME PaalAFT PER THE APPLICAKI FECtIV4 AVIATION REGULA11048. ftham II1C04 01401M Orwais San Ofted04.116,/ tio UndUndlOsprobill EFTA01326239 All0 V1)40 so u nu LIU as N • lignSI0311 14 8W Ind HAIM 031Id SDNY_GM_02753725 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00240647 EFTA01326240 MAJOR REPAIR AND ALTERATION ' 0 (Airframe, Powerplant, Propeller, or Appliance) Orni APPOY00 OMB 0,2007 No. 2120-0020 117 on< Ime.00 ionow For Pm um OW US Deortmont of Tronsocnssol 'Odin, Animon mminstroson INSTRUCTIONS: Pnnt or type as entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for and disposition o this form This report is required by law (49 U S C 44701) Failure to report can result in a civil penalty violation (49 U.S C. 46301(a)) instructions for each such 1. Aircraft Nationally and Registration Mark USA N212JE Serial No. 1085 Model G-IV Series Make GULFSTREAM AEROSPACE 2. Owner Name (As storm on registration certificate) JEGE LLC Address (As shown on registration certificate) Mans 6100 Red Hook Quarter 83 ay ST Thomas Stud Zo 00802 ciikrov Virgin Islands 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. 0 9 AIRFRAME (As described in item 1 above) 0 0 POWERPLANT 0 0 PROPELLER 0 0 APPLIANCE is Maitaciett 6. Conformity Statement A Agency's Name and Address B Kind of Agency I Manufacturer International Jet Interiors 2221 Smithtown Ave Ronkonkoma, New York 11779 USA Certificated Mechanic C. Certificate No. 'Mc _U.S. Foreign Certificated Mechanic Certificated Repair Station CRS I1JR439Y Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the unit s) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 0 App B Signature/Date of Authorized Individual . Thomas Norden Date. 2/20/2014 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation ACITiniSIta000 and is tE) APPROVED 0 REJECTED FM Fit. Standards Inspector Manufacturer Maintenance Organization Persons Approved by Canadian Department of Transport BY FM Designee X Repair Station Inspection Authorization Other (Specify) r ...\ Certificate or Designation No. CRS I1JR439Y Signature/Date of Authorized Indrodual Thomas Norden Date: 2/20/2014 • ,Kl aca e....4._ FAA Form 337 rio-osi SDNY_GM_02753726 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240648 EFTA01326241 NOTICE Weight and balance or operating limitalico changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and dale work accomplished.) USA N212JE Nationality and Registration Mark KGS ELECTRONICS II5VAC, 60FIZ, I000VA INVERTER SYSTEM INSTALLATION DATE 2/20/2014 I.) Removed 20. PIN: AK-55140M 28-I2VDC converters. 2ca. PIN: XD600-1 amplifiers, lea. P/N: XD600-6 amplifier, and lea. P/N: BBK-2AH keep alive battery. Installed a KGS Electronics I I SVAC, 60HZ, 1000VA inverter system in accordance with DB Integrations, LLC document No. 140121001 titled I I5VAC 60HZ Inverter Wiring Diagram, revision (0), dated February 5, 2014 which was approved under FAA form 8110.3 dated Febuary 11, 2014 (attached) for systems and equipment. 2.) The structural aspects of the inverter installation were accomplished in accordance with DB Integrations, LLC document No. 140205001 titled 60HZ Inverter Structural Installation, revision (0), dated February 5.2014 which was approved under FAA form 11110-3 dated February 13.2014 (attached) for structures. 3.) The structural aspects of the outlet and circuit breaker installations arc deemed a minor alteration, which were performed in accordance with applicable sections of AC43.13-I B and AC43.13.2G. 4.) The equipment list has been revised. 5.) The weight and balance has been revised. 6.) An electrical toad analysis has been performed and found not to exceed 80% of the full generator capacity. 7.) Instructions for Continued Airworthiness (ICA) are incorporated into DB Integrations. LLC document No. 140213002. revision (IR.). dated February 13, 2014 and have been provided to the operator for incorporation into the aircraft inspection/maintenance program. 8.) A Logbook entry has been made reflecting this modification. 9.) The work described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. Work Order No. 14104, on file at this agency, covers the above described work. No Further Entries CEI Additional Sheets Are Attached FM Form 337 (10-06) SDNY_GM_02753727 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240649 EFTA01326242 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 1. DATE February 11.2014 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Gultstream Aerostat. 3. MODEL NO. G.IV 4. TYPE MeV* E Sint PMCOSIV. arc I Airplane 5 NAME OF APPLICANT DS mtegraiions. I.LC LIST OF DATA 6. IDENTIFICATION 7. TITLE Report:0000214.1085. Rev. Wt. Dale: 02/11/2014 130 Hz T50 Invader Modification' NOTES: t. This approval coven Medial. design aspects onhr on Airplane Model G-IV. sin I 065 ands not intalialion approval. 2. The au0lorted agency retumng the Wadi to sena is responsible to determine compeance *II the above data. 3. This approval is lot ele*foal engineering design data only. It indraiNs IS data listed above densanstees coerces** or* with the regubtions specified by paragraph and subparagraph listed below as 'Applies* Rechirernents" 8. PURPOSE OF DATA To support Major Alteration FM Form 337 for sin 1065. The approval is design data approval only and Is not instate* approval. O. APPLICABLE REQUIREMENTS (List specific sectcas) 14 CFR Pan 25.0; 25.135100M Nerd 25:72; 25.1357 (aKb)(c)Ard 25.123 10. CERTIFICATION • Under authority vested by direction of the appointment under 14 CFR Part 183. data listed above and an alleChed in accordance with established procedures and found to comply 0 Recommend approval of these data I (1M0) Therefore a Approve Mose data Administrator and in accordance with conditions and limitations of sheets numbered have been examined with applicable reenactments of the Airworthiness Standards fisted. II. SIGNATURES) OF DESIGNATED ENG7RING 5 'SENTATivE(SI 12 DESIGNATION NUMBER(S) 13. Cl ASSiFICATION(S) , f David J Richards .2( ..............t.k .., 42.../ DERT 955091-NE Systems and Ethripnera Eleclncal FAA Form 8110-3 (01,10) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753728 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240650 EFTA01326243 SDNY_GM02753729 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240651 EFTA01326244 U.S. DEPARTMENT OF TRANSPORTATION FEOMAL AVtATiOn ADMINISTRATION STATEMENT OF COMRUANCE WITH AIRWORTHINESS STANDARDS I DATE 2/13/2014 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Gulfstream Aerospace Corporation 3. MODEL G-IV a TYPE (Aircraft. Engine. Propeller. etc.) Aircraft S. NAME OF APPLICANT DB Integrations UST OF DATA 6. IDENTIFICATION 7. TITLE 140205001 60 Hz Inverter Structural Installation, Sheets I through 4, Initial Release, dated February 5, 2014. Notes: 1. This approval is for engineering design data only. It indicates the data listed above demonstrates compliance only with the "Applicable Requirements." Compliance with additional regulations not listed here may be required. This form does not constitute FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. 2. TCDS is Al2EA. 8. PURPOSE Of DATA: Drawing 140205001 installs a 60 Hz inverter on an existing shelf on Gulfstream Aerospace Corporation Model G￾IV, A/C S/N: 1085, as a major alteration. 9. APPLICABLE REQUIREMENTS (List specific sections): 14 CFR dated February 1, 1965, including Amendments 25-1 through 25.56: 25.301 Loads, 25.303 Factor of safety, 25.305 Strength and deformation, 25.561 Emergency Landing Conditions —General, 25.601 Design and Construction —General, 25.603 Materials, 25.605 Fabrication methods, 25.607 Fasteners, 25.789 Retention of items of mass in passenger and crew compartments. 10. CERTIFICATION-Under authority vested by direction of the AdrniMstrator and in accordance with conditions and limitations of appointment under 14 CFR Part 183, data listed above and on attached sheets numbered have been ermined in accordance with established procedures and found to comply with applkable requirements of the Airworthiness Standards listed. O ROCOMMadd SPINOVil of these data I (We) therefore a Approve these data 11. SIGNATURE(S) Of DESIGNATED ENGINEERING REFIIESENTATIVE(S1 12. 0CSIGNATION NUMEIER(S) 13. ClASSIFICATION(S) CAT \ CLVN ICi)m)liN￾DERT-831129-CE STRUCTURES FAA Fpm $110.3 (O3/1O1SUPERCEDES PREVIOUS REVISION SDNCGM_O275373O SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240652 EFTA01326245 SDNY_GM02753731 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240653 EFTA01326246 U. S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I DATE 2/18/2014 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE Gulfstream 3.MODEL NO. • G-IV 4.TYPEfAhOwre. Craw. Propellor. It) Airplane sNAME OF APPLICANT International Jet Interiors LIST OF DATA tit IDENTIFICATION 7,11TLE TP 268821-14 Rev A Dated 02/18/2014 Skandia. Inc. Flammability Test Report Bunsen Burner Testing Test Specimen P/N's 1 (represents floor covering) 2 (represents floor ducts) 3 (represents seat bases) 4 (represents cockpit. sidewalls & pedestal) Notes: 1) Work accomplished under Skandia Inc. WO 0 268821.14, Ref Document ID 94995. 2) Flammability test witnessing only, does not constitute installation approval of materials. 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for SIN 1085 9.APPLICABLE REQUIREMENTS dist specific sections) 14 CFR Pan 25.853 (a) Arndt 25-116 Appendix F Pad I (a)(1Xi) Amdt 25-111 14 CFR Part 25.853 (a) Arndt 25-116 Appendix F Pan I taxixie 10.CERTIFICATION - Under authority vested by direction of the Administrator of appointment under 14 CFR Pail 183. data listed above and on attached examined Si accordance with established procedures and found to comply Standards listed. 0 Recommend approval of these data I (ibb)Therefore )tiaprove these data , and in accordance with conditions and imitations sheets numbered have been with applicable requirements of the Airworthiness I I.SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE 12.DESIGNATION NUMBER(S) 13.ctASSIFicATiOmS) )4Q \bObit 'xi 1 gl Ja- Biberstein -FAA DER DERY-832780-CE Structural Special orm 8110-3 (03ile)•SUPERSEDES PREVIOUS EDITION SDNY_GM_02753732 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240654 EFTA01326247 SDNY_GM02753733 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240655 EFTA01326248 0 MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) US Doperonant of Trecepflon Fedenl Avladon Adminievetion ram Approved iEllevonc OMB iirk NO 2120-0020 oncor Trseiro Noce' Fee FArtUe•Only INSTRUCTIONS Print or type all entries See FAR 43 9 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for instructions and disposition o this form. This report is required by law (49 U.S.C. 44701). Failure to report can result in a civil penalty for each such violation (49 U.S C. 46301(a)). 1. Aircraft Nationality and Registration Mark USA N212JE Serial No. 1085 Model G-IV Series Make GULFSTREAM AEROSPACE 2. Owner Name (As shown on registration certificate) JEGE LLC Address (As shown on registration certificate) Aedess 6100 Red Hook Quarter cay St Thomas sine A, 00802 corm Virgin Islands 3. For FAA Use On 4. Type 6. Unit Identification Repair Alteration Unit Make Model Serial No El i7i AIRFRAME (As described in item 1 above) 0 0 POWERPLANT 0 PROPELLER 0 • APPLIANCE T10F hiestellOlaW 6. Conformity Statement A. Agency's Name and Address B Kind of Agency I Manufacturer International Jet Interiors 2221 Smithtown Ave Ronkonkoma, New York 11779 USA U.S. Certificated Mechanic C. Certificate No. Foreign Certificated Mechanic k Certificated Repair Station CRS I1JR439Y Certificated Maintenance Organization D. looney that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the reverse or enactments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 0 APP. 8 Signature/Date of Authorized Individual Thomas Norden Date: 9/19/2013 C---- Il aelAl .t ) elra -....1 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is (2) APPROVED 0 REJECTED FM ect« Fit. Standards Insp Manufacturer Maintenance Organization Persons Approved by Canadian Department of Transport Y FM Designee X Repair Station Inspection Authorization Other (Specify) Certificate or Designation No. 'Signature/Date of Authonzed Individual CRS I1JR439Y ", . Thomas Norden Date: 9/19/2013 kil a eir FM Form 337 0005) SDNY_GM_02753734 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240656 EFTA01326249 NOTICE Weight and balance or operating limitation changes snail be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets, Identify with aircraft nationality and registration mark and date worn accomplished) USA N212JE Nationality and Registration Mark DATE 9/19/2013 Modified the existing Cabin Entertainment System in accordance with Electrical Drawing listed below ( Note: reference FAAIDER approved Structural Drawings for provisions for all Audio and Video equipment installed at this time on FAA 337 Form, this date). Dwe No. Date Rev Title PA-G1V-1085.2501 8/21/13 B CABIN ENTERTAINMENT SYSTEM (MOD) ELECTRICAL DRAWING The above listed wiring diagram is FAA/DER approved by W.C. Janzer (DERT-510187-CE), Systems and Equipment, Electrical Equipment via FAA Form 8110-3 dated 8f2 I /13, attached to this 337 Form. Electrical Load Change is negligible & dots not exceed the 80% electrical power generating system on the aircraft. Complied with a EMI-RFI Test Flight, there were no adverse effects on any other systems. The Aircraft's Scheduled Maintenance Program is not altered by this installation. The cabin entertainment system components are considered to be "On Condition Items". A supplement to the aircraft equipment list and copies of the wiring diagrams listed above has been provided to customer and must be added to the aircraft's records. The work described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. Work Order No. 13127, on file at this agency, covers the above described work. A Logbook entry has been made reflecting this modification. No Further Env' 0 Additional Sheets Are Attached FM Form 337(10-06) SDNY_GM_02753735 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240657 EFTA01326250 us CenOnigetir CO MAKSPCIOAHON rECERAL AVIATION ADWNGTRATIO11 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS T. WI: AUG 21, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE GULFSTREAM 2. MODEL NO. G-IV 4. TYPE (Aircraft &Kant Aromatic. ate.) AIRPLANE S. NAME OF APPLICANT PRODIGIOUS AVIONICS LIST OF DATA S. menwicknon 7. DILE PRODIGIOUS AVIONICS PA-GIV-1085-2501 9 SHTS REV: B DATE: 8.21.2013 DRAWING: CABIN ENTERTAINMENT SYSTEM (MOD) ELECTRICAL DRAWING NOTES: I- THIS APPROVAL IS FOR THE ELECTRICAL ASPECTS ONLY. 2- THIS APPROVAL IS FOR THE DESIGN ASPECTS ONLY AND DOES NOT CONSTITUTE INSTALLATION OR OPERATIONAL APPROVAL. 3- IF THIS APPROVAL IS PROVIDED FOR A FOREIGN REGISTERED AIRCRAFT, ACCEPTANCE OF THIS APPROVAL IS AT THE DISCRETION OF THE CIVIL AVIATION AUTHORITY OF THE STATE OF REGISTER. 4- THE INSTALLER MUST DETERMINE THE COMPATIBILITY OF THIS DATA WITH THE AIRCRAFT CONFIGURATION. S. PURPOSE OF DATA TO APPROVE THIS MAJOR ALTERATION ON GULFSTREAM AEROSPACE G-IV AIRCRAFT N423TT SERIAL NUMBER 1085 IN SUPPORT OF FAA FORM 337. I. APPLICABLE REOURIEMENTS (UM *milk IMKtioas) 14CFR25.603(b) Arndt. 25-46 14CFR25 1301(a)(b) Arndt. 25-123 14CFR25.869(a) Arndt. 25-123 14CFR25.1309(a)(b)(c)(e)(g) Arndt 25-123 14CFR25 1353(x) Amdt. 25-123 ID CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under 14 CFR Pan 183, data listed above and on attached sheets numbered XXXXXXXXX have been examined in accordance with established listed. I (We) Therefore O L procedures and found to comply with applicable requirements of the Airworthiness Standards Recommend approval of these data Approve these data 11. SIONATUREIS) OF DESIGNATED ENONEEMNG REPRESENTATIMM D. DESRVIATON NUMSER(S) 13. MASSiFiCATC/410) W.C. Janzer .....-------- DERT-5 I CH 87-CE Systems & Equipment Electrical Equipment GULFSTREAM FAV-ENTERTAINMENT-N42317- ISM FAA Form 81104 SOnteM41ERSEDES PABACus EDTIC•I SDNY_GM_02753736 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA ())24(X158 EFTA01326251 SDNY_GM_02753737 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240659 EFTA01326252 MAJOR REPAIR AND ALTERATION eji (Airframe, Powerplant, Propeller, or Appliance) us Oningren1 01 Trartgelab3n Federal Mit., AdmInIstralon Form Approved CUB No 2120-0020 1100/2007 .astitonic Trion; NW OP For FAA On On, INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for and disposition of this form. This report is required by law (49 U.S.C. 44701). Failure to report can result in a civil penalty violation. (49 U.S C. 46301(a)). instructions for each such 1. Aircraft Nationality and Registration Mark USA N212JE Serial No. 1085 Model G-IV Series Make GULFSTREAM AEROSPACE 2. Owner Name (As shown on registration certificate) JEGE LLC Address (As shown on registration certificate) Pants 6100 Red Hook Quarter B3 on ST Thomas sw. zo 00802 co.my Virgin Islands 3. For FAA Use Only 4. Type 5. Unit Identification Repair Altmann Unit Make Model Serial No. 0 Er AIRFRAME (As described in item 1 above) 0 0 POWERPLANT • 0 PROPELLER • 0 APPLIANCE n" OilaMaconer 6. Con ormi Statement A. Agency's Name and Address B. Kind of Agency Manufacturer International Jet Interiors 2221 Smithtown Ave Ronkonkoma, New York 11779 USA U.S. Certificated Mechanic C. Certificate No. Foreign Certificated Mechanic x Certificated Repair Station CRS I1JR439Y Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the reverse or have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that t furnished herein is true and correct to the best of my knowledge. attactrnents • hereto tMn Extended range fuel per Signature/Date of Authorized Individual Date: 9/19/2013 7. Approval for Return to Sento. Pursuanl to the authority given persons specified below. the unit identified in item 5 was invected in the manner prescribed Administrator of the Federal Aviation Administration and is el APPROVED 0 REJECTED by the FM FN. Standards Inspector Manufacturer Maintenance Organization Persons Approved Department of Transport by Canadian BY FM Designee X Repair Station Inspection Authorization Other (Specify) Certificate or Designation No. Signature/Date of Authorized Individual CRS I1JR439Y Thomas Norden Date: 9/19/2013 e\INWIS FM Form 337 most SDNY_GM_02753738 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240660 EFTA01326253 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previota alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work accomplished.) USA N212JE DATE Nationality and Registration Mark 9/19/2013 (I) Fireblocked and reupholstered Six (6) existing single cabin chain, two (2) existing double cabin chairs and one (1) existing jump seat with Edelman Leather: Royal Hide RH32. Fireblocked and upholstered one (I) new replacement (Goodrich PN 960014.49) divan with Brentano Fabric: Simplicity￾Carrara 1010-01. Rewebbed the existing PAX seat and shoulder harness belts by C&M Marine Aviation Services Inc., CRS V05R749Y, under W.O. 5006. 8130-3 dated 8/8/13. Aircraft seat cushions have been fireblocked as pa the requirements of tine 14 CFR, 25.853(c) Amendment 25 - 116 Appendix F Part II and 14 CFR, 25.853(a) Amendment 25- 116 Appendix F Pan l(aK I x ) Results of Oil Boma Testing arc documented on (attached)Skandia Inc. FAA/D.E.R. approved 8110-3, dated 9/19/13, document ID 94288, WON 25830443, Test Flan 122867 Rev B, dated 8/01 /2013, by Jennifer Paluza FAA/DER (DERV-832779-CE). (2) The Crew Scats were snipped and reupholstered with Edelman leather. "Royal Hide, RH32, Dead White" and Aircraft Sheep Skin Co.: Sheepskin 3CCOOI, White. Rewebbed two (2) crew seal Spt seat and shoulder harness belts by C&M Marine Aviation Services Inc, CRS V05R749Y, under W.O. 4991, 8130-3 dated 8/13/13. Flammability Testing (Spec 12) was approved via Skandia Inc. (WO 1257726-13. Test Plan 0 21306) Vertical Flammability Test Results Report dated 6/24/13(attached) by PANDER lane Biberstein. (3) Stripped and recovered Baggage Area / Jeppesen Storage Box in Tapis, Grospoint Black 0091, Lot R. Flammability Testing (Spec /land Spec II) was approved via Skandia Inc. (WON 257726-13, Test Plan SI 21306) Vertical Flammability Test Results Report dated 6124/13 (attached) by FAA/DER Jane Biberstein, (4) Stripped and recovered Forward Closet and Aft Lavatory Storage in Tapis Fabric Grospoint, Muse Blue-FR, 0018. Flammability Testing (Spec (5) was approved via Standee Inc. (WO 0 257726-13. Test Plan N 21306) Venice! Flammability Test Results Report, dated 6/24/13 (attached) by FAA/DER lane Bibermein (5) Fabricated new Entry Rain Curtain in Willowtex list Leather Snow, FR2250A/SKD-I and Ebony Izit Leather, FR2250Bakd-7. Flammability Testing (Spec 0) was approved via Skandia Inc. (WON 257726-13, Test Plan 121306) Vertical Flammability Test Results Report dated 6/24/13 (attached) by FAA/DER lane Bibastein. (6) Recovered the Existing Forward/ Aft Lavatory Side Panel Bulkheads in Willowy Fabric: Snow hit Enhanced A. FR2250A/SKD-L Flammability Testing (Spa N 7) was approved via Skandia Inc. (WON 257726-13, Test Plan N 21306) Vertical Flammability Test Results Report, dated 6/24/13 (attached) by PANDER lane BibersIcin. (7) Recovered the Existing Headliners. Valances and PSU's and Hand Rails in Tams- Ullrasue0e, 3723 Pak Beige. Flammability Testing (Spec 19 and 10) was approved via Skandia Inc. (WON 257726-13. Test Plan a 21306) Vertical Flammability Test Results Report, dated 6/24/13 (attached) by FAA/DER lane Bibersitin (8) Stripped and recovered the existing Window Line Panels and Aft Lay Side Wall panels in Brentano Fabric: Simplicity-Cara 1010-01. Flammability Testing (Spec II l) was approved via Skandia Inc (WO N 257726-13. Test Plan 0 21306) Vertical Flammability Test Results Report, dated 6/24/I) (attached) by PANDER lane Biberstein. (9) Stripped and recovered the existing Lower Side Wall Panels in Edelman Woven Leather. WVNC50. Flammability Testing (Spa 012) was approved via Skala. Inc (WON 257726-13, Test Plana 21306) Vertical Flammability Test Results Report, dated 6/24113 (attached) by FAA/DER Jane Biberstein. (I0) Stripped and recovered the existing Aft Cabin Bithd and Fwd Aft Galley Mild in Acrospecialtia..125 Polycarbonate Minor, 16004102. Flammability Testing (Spec NI 5) was approved via Skandia Inc (WON 257726-13. Test Plan 0 21306) Vertical Flammability Test Results Report. dated 6/24/13 (attached) by PANDER Jane Blear:win. (1 1) Stripped and recovered the existing Divan End Arms. Divan Lower Doors and Lower Side Walls in Edelman Leather: Royal Hide. RH32, Dead White. Flammability Testing (Spec 116) was approved via Skandia Inc. (WOI 25772643, Test Plan 121306) Vertical Flammability Test Results Report. dated 6/24/13 (attached) by FAA/DER hale Biberstein. (18) Stripped and recovered the Entry Area and Baggage Compartment Floor in A1P: Aermat, 37R/SV/1000/985/20R/54. Flammability Testing (Spec N20) was approved via Skandia Inc. (WON 257726-13. Test Plan 21306) Venial Flammability Test Results Report. dated 6/24/13 (attached) by FAA/DER lane Bibentein. (19) Installed new nplacanau Aft Galley and Lay Countertops with Evans & Paul..187, Designer White Corian. Flammability Testing (Spec121) was approved via Skandia Inc. (WO 125772613, Test Plan It 21306) Vertical Flammability Ten Results Report, dated 6/24/13 (attached) by FAA/DER /the Biberslea. (20) Stripped and recovered the existing Aft Lay Closet Sliding Doers in ACt0SpeCiallieS, .125 Polycarbonate Clear. Minor and Tpis,0018 Muse Blue-FR Grogram, Fabric. Flammability Testing (Spec 122) was approved via Skandia Inc. (WON 257726-13. Test Plan 1 21306) Vertical Flammability Test Results Report, dated 6024/I) (attached) by FAA/DER lane 8ibasttin. Additional Sheets Are Attached FM Form 337 (10-C6) SDNY_GM_02753739 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240661 EFTA01326254 NOTICE Weight and balance or operating limitation Changes shall be entered in the appeopnate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished (If more space is required, attach additional sheets, Mealy with aircraft nationality and registration mark and date work ished) USA N212JE Nationality and Registration Mark DATE 9/192013 (21) Fabricated and Installed new replacement Baggage Flap in MP. Hematite Red, /80, 0001,Vinyt. Flammability Testing (Spec /23) was approved via Skandia Inc.(W01 257726-13, Test Plans 21306) Vertical Flammability Test Results Report, dated 6/24/ I 3 (attached) by FAA/DER lane Biberslein. (22) Stripped and recovered the existing FWD Cabin Bulkheads in Brentano Fabric: Simplicity-Carrara 1010-01. Flammability Testing (Spec N24) was approved via Skandia Inc. (WO a 257726-13. Test Plan /1 21306) Venial Flammability Test Results Report, dated 6/24/13 (attached) by FAA/DER Jane Biberstein. (23) Stripped and recovered the existing FWD and AFT Potty Seats and Shrouds with Edelman: Woven Leather, WVNC50. AM 3FL. Flammability Toting (Spec I8, N I4) was approved via Skandia Inc. (WON 260097-13, Test Nana 21306) via FAA Form 8110-3 (attached) dated V I V I 3 by FAA/DER lane Biberstein (DERV-1)2780-CE). (24) Fabricated new Conference Table Top using Indiana Architeautal Plywood, laminated with Makore Pom, Veneer. Flammability Testing (Spec 113) was approved via Skandia Inc. (WO N 260097-1). Test Plan N 21306) via FAA Form 8110-3 (attached) dated 8/13/13 by FAA/DER Jim Biberstein (DERY-832780-CE). (25) Installed a new Carpet throughout the cockpit, main cabin. and Floor Ducts areas using ABC Carpet - Wootston Plaid Shoreline. Flammability Testing (Spec I 17./18, 119) was approved via Skandia Inc. Rcfacnce (anached) Skandia Inc. FAA/D.E R. approved 8110-3. dated 9/18/13. document ID 94212, WON 261824-13, Test Plan II 21306 Rev UR by Jennifer Paluzzi FAA/DER (DERV-832779-CE). (26) Modified the following existing cabinetry in accordance with the following FAA/DER approved Drawings ' ;:rtimNo... ! :. A . ter .2", • WIGIVIMS IR INFERIOR INSTL UIGIVIOSSA IR MONITOR MOD INSTL4tH FWD UIGIVII0858 A CONFERENCE TABLE MOD INSTL LIIGIV1085C IR DIVAN INSTL-LH AFT LIIGIV1085D IR LH AFT CLOSET MOD INSTL IJIGIV1085E IR DIVAN ARMREST INST1.4.11 AFT IJIGIV1085F A ENTERTAINMENT EQU1PT MOD INSTL-CREDENZA UIGIVI0850 IR MONITOR MOD INSTL414 AFT UIGIVI08511 IR RH GALLEY MOD INSTL UIGIV101151 IR LH GALLEY MOD INSTL LIIGIVI085K IR VANITY MOO INSTL UIGIVIMI5L IR PSU MOD MIL All above listed structural drawings were approved via attached; FAA PRIM 8110-3, doted Mg 22,2013 Tin Sept 16.2013 by FAA/DER Brian C Adamson, DERT-830137-CE and Donald E. Shepherd. Jr. DERT-230307-CE. Passenger ante width maintained per Title I4 CFR 25.815. A supplemental equipment list has been supplied. A logbook entry has been made reflecting this alteration. All Cabin Interior Fumishings listed above have been Bum Tested in accordance with Title 14 CFR Pan 25.853 (a) Amdl. 25-116 Appendix F Part I (IXI MO Arndt 25-III and Tide 14 CFR Pan 25.853 (a) Am& 25-116 Appendix F Part I (a)( IRO as applicable . This Modification/Repair to the existing Cabin Interior furnishings requires No Scheduled Maintenance Tasks or Ainvonhiness Limitatiens, refer to the Gulfuream Maintenance Manual, and all other existing aircraft ICA's. The Aircraft's Scheduled Maintenance Program is not altered by this installation. The work described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness aitcna under which it was originally certificated Work Order No. 13127, on file at this agency, covers the above described work. No Further Entries 0 Additional Sheets Are Attached FAA Form 337 (10-06) SDNY_GM_02763740 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240662 EFTA01326255 SDNY_GM_02753741 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240663 EFTA01326256 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIANON ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE August 22 2013 AIRCRAFT OR AIRCRAFT COMPONENT umanncAnort 2 MAKE Gulfstream 3 MODEL NO. G-IV sin 1085 4. TYPE Wreak Env* Ropey Pt) Airplane 5 NAME OF APPLICANT International Jet Interiors, Inc. Ronkonkoma. NY UST of DATA 6 I3DRIFICATION 7 TITLE Drawing: IJIGR/1085 Rev (IR) 05/13/2013 IJIGN1005D Rev (IR) 06/11/2013 Report: IJIGIV1065DSA Rev (IR) 013/22/2013 Structures Note: Interior !me sht 1 - 4 LH Aft Closet Mod Instl slit 1 - 5 Structural Analysis LH Aft Closet Mod Intl Gulfstream G-IV Aircraft 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements". 2) This form does not constitute FAA approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and requires separate approval. S. PURPOSE Of DATA. To provide type data for FAA approval of structure in support of a Major AJteration for Gulfstream G-IV sin1085. A ApPUC48LE REOUREMENTS OM Wed& ma** 14 CFR Part 25, Amdt 25-1 through 25-56 as specified in TCDS Al 2EA; Paragraphs: 25.301(a-b) Amdt 25-23.25.303 Arndt 25-23, 25.305(a, b) Amdt 25-54, 25.307(a. b) Arndt 25-54, 25.341 Arndt 25-0, 25.561(a-c)Amdt 25-23, 25.601 Arndt 25-0.25.603(8c) Arndt 25-46, 25.605(a) Arndt 25-46, 25.609(a) Arndt 25-0, 25.611 Arndt 25-23, 25.613(a, b, d, e) Arndt 25-46, 25.615(a) Arndt 25-23, 25.619(a-c) Arndt 25.23, 25.623 Arndt 25-0, 25.625(8c) Arndt 25-23, 25.769(a) Arndt 25-46. 10. CERTIFICATON - Uncle, autalty vested by Onettlan of the Adrrenstmer and in ecconlinca Me ceetalens and limiteen Pat 189. dm Wed abOva end on attached sheets numbered 91a._. nate been exarened h accedence we* esistashed 440 apploalatt readramens of the Airtrolhoen Stilr4Srd, INGO ❑ Recommend approval of those dab I OVIOThetefcce 0 Approve these Oat/ of *papered under 14 CFR ceacelotes and loved to co.rVy 11. SIGNATURE/S)OF DESCANTED ENGINEERNG REPRESENTATIVE(S) 12. DESSIATON MAMMAS(S) 13. (1 ASSLTICATOMS) Brian C. Adamson ofe seLc.0 ,.... ....c.---- DERT-830137-CE Structures FAA Refs 11104 (131I0) SUPERSEDES PREVIOUS EIXT04 3-494-4 SDNY_GM_02753742 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240664 EFTA01326257 SDNY_GM_02753743 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240665 EFTA01326258 U.S. DEPARTMENT OF TRANSPORTATICN FEDERAL AV1ATION ADIAMSTRATICN STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS i. (»TE September 16, 2013 AIREFtAFT OR AIRORAFT COMPONENT IDEN TIFICATION 2. MAKE Gulfstream t IACIDEL MD. G-IV s/n 1085 4. TYPE Sttrorali Eniiva Pitrosim. ec.) Airplane i MANE OF "CM« International Jet Interiors, bc. i Ronkonkoma. NY UST OF DATA S VENTIRCAT 04 2 lime Drawing: - . IJIGIV1085F Rev (A) 09/13/2013 Report IJIGIV1085FSA Rev (A) 09/16/2013 Structures Note: Entertainment Equipt Mod Instl-Credenza slit 1 - 6 Structural Analysis Entertainment Equipt Mod Instl. Credenza Gulfstream G-N Aic i ,.: fi 1) The structural aspetts only of the above listed data are approved herein. Tres approval is oSy for the engineering data. It indicates the data listed above demonstratas compliance onty with the regulations specifled by paragraph and subparagraph listed below as "Applicable Requirements". 2) This form doer not constitute FAA approval of all the engineering design dala necessary for substantiation of compliance to necessary requirements for tie ente alteration. The requirements of Electrical Systems and Equipment and Flammabityae ,- not induded in this approval and require separate approval. 3) Aircraft kilenot compliance inspection is not included m this approval and netaines separate approval. 8. PUFtPOSE OF DATA To provide type data for FAA approval of structure in support of a Major Alteration for Gulfstream 6-1V ski:DE& 9...APPLICABIE REOUIRENENTS (UR Nedla inceini) 14 CFR Part 25, Arndt 25-1 through 25-56 as specified in TCDS AI2EA; Paragraphs: 25.301(a-b) Arndt 25-23, 25.303 Arndt 25-23, 25.305(a, b) Arndt 25-54, 25.307(a, b) Anst r)-54. 25.341 Arndt 25-0, 25.561(a-c) Arndt 25-23, 25.601 Arndt 25-0, 25.603(a-c) Arndt 25-46, 25.605(a) Ami 25-65, 25.609(a) Arndt 25-0, 25.611 Arndt 25-23, 25.613(a. b, d, e) Arndt 25-48, 25.615(a) Arndt 25-23, 25.619(wcikatt 25-23. 25.623 Arndt 25-0, 25.625(a-c) Arndt 25-23, 25.789(a) Arndt 25-48. 10. OERTIRCATION • under suNortry vred by terecloe d Om Administrator and In aeccidence trim condMons and IiiraMOrd d SCI2 e Ill Pan 183. CM* mel *hove and on *trad sheMs nemt:sed uta vere bal dernned in scoordanca sei estioddied eveceatra sed bed t =ME iiai apeacotro requirements ot IMAinvortrinees Standard, 4,164. 0 ReCommend approval of til I (pq?Therekn ISI APprove tinn. data 11. SIGNATIMEiS)OF CESIGNATED ENGINEERNG REPRESENTAI~ 12. DESIGNA/KN NULIBERS(S) 13. EIASSIF~E4 Donald E. Shepherd, Jr. den eid r..$4.4År - DERT-230307-CE Structures FM Fordi $1104 (03110) SUPERSEDES PREVIOUS EDITION i 3 - Mat SDNV_GM_02753744 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240666 EFTA01326259 SIDNYGM 02753745 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240667 EFTA01326260 U.S. DEPARnair OF TRANSPORTATION FEDERAL AviimoesOliveSTRAMON STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I. DATE August 30.2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Gulfstream 3 MODEL NO. G-IV sin 1085 4. TYPE To0110. Engu* Moran a) Airplane 3. NAME OF APPLICANT International Jet Interiors, Inc. Ronkonkoma. NY UST OF DATA 6 DemncAnoN 7. TITLE Drawing: IJIGIV1085B Rev (A) 08/29/2013 Report UIGIV10858SA Rev (A) 08/30/2013 Structures Note: Conference Table Mod InstI see 1 - 5 Structural Analysis Conference Table Mod InstJ Gulfstream G-IV Aircraft 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements'. 2) This form does not constitute FM approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and requires separate approval. 4) See sheet 2 for additions drawings supporting drawing WIGIV10858 Rev (A). & PURPOSE OF DATA To provide type data for FM approval of structure in support of a Major Alteration for Gulfstream G-IV s/n1065. 9. APPLICABLE Reotsserts its walk wen) 14 C0R. Part 25, Amdt 25-1 through 25-56 as specified in TCDS Al 2EA: Paragraphs: 25.301(a-b) Amdt 25-23, 25.303 Amdt 25.23, 25.305(a, b) Amdt 25- 54, 25.307(a, b) Amdt 25-54, 25.341 Amdt 25-0, 25.561(a-c) Amdt 25-23, 25.601 Amdt 25-0, 25.603(a-c) Amdt 25-46.25.605(a) Arndt 25-46, 25.609(a) Arndt 25-0. 25.611 Amdt 25-23, 25.613(a, b, d, e) Arndt 25-46, 25.615(a) Amdt 25-23, 25.619(ac) Amdt 25-23, 25.623 Amdt 25-0, 25.625(a-c) Amdt 25-23, 25.789(a) Arndt 25-46. 10. CERTRCATON . Under au/berity reeled by direction of the Adoatnitor and in accordance vats condition rd irmamea of wren oaf la CFR Pan 133. date Wed above and on ached sheets nurnbered 2 o12 haTo poor eom-.ed In woo/dare.. An, esttlAbbed procodufee and bind b comply well applealio requirements of De Alfocoddnesa Standards lama. O Recommend approval of these data I tWo)Therefae 0 Approve Thee data II. 304ATUROSIOF DESIGNATED ENCNEER1NG REPRESENT/LINOS) 12. DESIGNATION fiUMBETASOI 13 CLASSIFICATIONS) Brian O. Adamson ( Oa ts_ DERT-830137-CE Styr:tures FAA Fern, 1110-3 OW SURERscr-Fs PREVIOUS EDITION r2 -001-9 SDNY_GM_02753748 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240668 EFTA01326261 SDNY_GM_02753747 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240669 EFTA01326262 VS. IMPART ENT OF TRANSPORTATION FEDERAL AVIATION ADIANiSTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I. DATE August 19.2013 AIRCRAFT Oft AIRCRAFT COMPONENT IDENTIFICATION Z. IMRE Gulfstream 3. MODEL NO. G-IV s/n 1085 4. TYPE (Alta Engine. Propstaef, era) Airplane S. NAME OF APPLICANT Intemabonal Jet Interiors, Mc. Ronkonkoma, NY UST OF DATA IL IDENTIFCAPON T TIRE Drawing: LlIGIV1085J Rev (IR) 07/16/2013 IJIGIV1085H Rev (IR) 07/16/2013 Report: IJIGIV1085JSA Rev (IR) 08/12/2013 IJIGIV1085HSA Rev (IR) 08/12/2013 Structures Note: LH Galley Mod Insti sht 1 - 4 RH Galley Mod Instl sht 1 • 4 Structural Analysis LH Galley Mod InsU Gulfstream G-IV Aircraft Structural Analysis RH Galley Mod Inst1Gulstream G-IV Aircraft 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and ' subparagraph listed below as "Applicable Requirements". 2) This form does not constitute FAA approval of all the engineering design dab necessary for substantiation of compliance to necessary requirements for the ate alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and rterSas separate approval. & PURPOSE OF DATA To provide type data for FM approval of structure in support of a Major Alteration for Guttstream G4V sen10135. ; i tcAPPUCABLE REOUIRDAENFS ,. speak mama) 14 CFR Part 25, Arndt 25-1 through 25-56 as specified In TCDS Al2EA: Paragraphs: 25.301(a-b) Arndt 25-23, 25.303 Amdt 25-23, 25.305(a, b) Amdt 25-54, 25.307(a, b) Arndt 25-&-.. 25.341 Arndt 25-0, 25.561(a-c) Arndt 25-23, 25.601 Amdt 25-0, 25.603(a-c) Arndt 25-46, 25.605(a) AMA 254B. - 25.609(8) Arndt 25-0, 25.611 Arndt 25-23, 25.613(a, b, d, e) Arndt 25-46, 25.615(a) Arndt 25-23, 25.619(a-4A:sit I 25-23, 25.623 Arndt 25-0, 25.625(a-c) Amdt 25-23, 25.789(a) Arndt 25-46. i 10. CERTIFICATION • Una( authority pee Ity, maa ems !bore end On wth Amicable reatfiemama a/ the vaned by claccton of the Admidaastm we In madam, MP unarm and InglatIceeMigeeetrmarea -A OR may sea ri,mbcod Mi... Mae been sominad In eccoMance 4eth antennae Resmeares ltd tete C =ate .. Atwanfiness Standards fisted apetovel of ems* deb thin data • Recommend I (/ft) Thereby Cll APPFave II. SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTATTVELS) 12 DES/GMMONNUMBERS(S) 13. CLASSIRCATOCS Brian C. Adamson _ _.,..- 3 „....-- C...- ------ DEBT-630137-CE Structures FM Form $110.3 (03110) SUPERSEDES PREVIOUS EDITION 13-002-4. SDNY_GM_02753748 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240670 EFTA01326263 SDNY_GM_02753749 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240671 EFTA01326264 STATEMENT OF U.S. DEPARTMENT OF TRANSPORTATION AIRWORTHINESS STANDARDS 1. DATE FEDERAL AVIATION ApiEUSSTRATTON August 22 2013 COMPLIANCE WITH AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. LAKE Gulfstream 3. Meal NO. G-IV s/n 1085 A TYPE (Alma EVAN. PNE4407, n7c) Airplane 5. NAME OF APPLICANT International Jet Interiors, Inc. Ronkonkoma, NY UST OF DATA 6 CEINIFICATION 7 TRIE Drawing: IJIGIV1085A Rev (IR) 07(16/2013 Report: LIIGIV1085ASA Rev (IR) 08/21/2013 Structures Note: Monitor Mod Instl-RH Fwd slit 1 - 3 Structural Analysis Monitor Mod Intl-FtH Fwd Gulfstream G-IV Aircraft 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements". 2) This form does not constitute FM approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and requires separate approval. S. PURPOSE OF DATA To provide type data for FAA approval of structure In support of a Major Alteration for Gulfstream G-IV s/n1085. 9. APPLICABLE REQUIREMENTS MN soma sceftm) 14 CFR Part 25, Amdt 25-1 through 25-56 as specified in TCDS Al 2EA; Paragraphs: 25.301(a-b) Arndt 25-23, 25.303 Amdt 25-23, 25.305(a, b) Amdt 25-54, 25.307(a. b) Amdt 25-54, 25.341 Amdt 25-0. 25.561(a-c) Amdt 25-23, 25.601 Amdt 25-O. 25.603(a-c)Amdt 25.46.25.605(a) Amdt 25-46, 25.609(a) Amdt 25-0, 25.611 Amdt 25-23, 25.613(a, b, d, e) Amdt 25-46, 25.615(a) Arndt 25-23. 25.619(a-c) Arndt 25-23, 25.623 Amdt 25-0, 25.625(a-c) Amdt 25-23. 25.789(a) Aral 25-46. 10. CEITDREADON • UM* nullinAly moo, by atecncA of the PM I83. On GAM ken end on abed abs nettled oiM me** roodienwers ol to Almalltwas Damara Wed 0 RoOmmooltd oPproyol Sews@ don I DVIN TAMEN, 0 APPloys those data AdminNINsar end ale nave been in a:Godard MA oremon and Umitakte 01 aNneintinerninclor it CFR canted in aNtordance MD ellatATITA3 procedures end Nunn to WWI 11. SIGNATURE(S) OF DESIGNATED ENG04F.EAR40 REPRESENTATIVE(9) 12. DESIGNATION NumitERS(S) ii. ciessinrAnoiks) Brian C. Adamson -c:, .. DERT-830137-CE Structures FAA Form 51104 (01/10) SUPERSEDES PREVIOUS EDITION O-tier t -7 SDNY_GM_02753750 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240672 EFTA01326265 SDNY_GM_02753751 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240673 EFTA01326266 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATKIN ACOMISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I. DATE August 19, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Gulfstream 1 MODEL NO. G-IV s/n 1085 4 TYPE Stara &pink Propeller; art) Airplane S. NAME OF APPLICANT International Jet Interiors, Inc. Ronkonkoma. NY LIST OF DATA 6 IDENTIFICAIION 7 TITLE Drawing: IJIGIVI(P35B Rev (IR) 06/0512013 IJIGIV1065K Rev(IR) 07/05/2013 Report: IJIGIV108513SA Rev(IR) 08/19/2013 IJIGIV1035KSA Rev(IR) 08/1212013 Structures Note: Conference Table Mod Instl sht 1 - 5 Vanity Mod 'mil sht 1 - 4 Structural Analysis Conference Table Mod Insti Gulfstream G-IV Aircraft Structural Analysis Vanity Mod Intl Gulsfteam G-IV Aircraft 1) The structural aspects only of the above listed data are approved herein. TMs approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements". 2) This form does not constitute FAA approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and regales separate approval. t PURPOSE OF DATA TO provide type data for FM approval of struchne in support of a Major Alteration for Gulf stream G-fV s/nl0$5. 9. APIMCABLE REQUIREMENTS (UN Met eardkos) 14 CFR Part 25, Amdt 25-1 through 25-56 as specified in TCOS Al2EA; Paragraphs: 25.301(a-b) Arndt 25-23, 25.303 Amdt 25-23, 25.305(e, b) Arndt 25-54, 25.307(a, b) Amdt 25-54 25.341 Arndt 25-0, 25.561(a-c)Amdt 25-23, 25.601 Amdt 25-0, 25.603(a-c) Amdt 25-46, 25.605(a) Arndt 25-48, 25.809(a) Arndt 25-0, 25.611 Amdt 25-23, 25.613(0. b, d, e) Amdt 25-46. 25.615(a) Amdt 25-23, 25.619(apc) Ala 25-23, 25.823 Arndt 25-0, 25.625(a-c) Amdt 25-23, 25.789(a) Arndt 25-48. io. carifiFICATON .Unclor *Mod* PM In 000 ate] ' led on 00 000icable multenrs 0 re . 0 Recommend tistied by catectice of Re sheets nunixted Meatiness Standards Imo approval of these these OM AthnkatiflOr and Na have been In accordance MA ccedelorts AM MUM. of morolrenet mar t4 CFR ermines In actordfrea Mn forablfichod maks and lc r 0 CO* arts I (ele)Thetefoie 0 Morove II. SIONATURE(3)06 DESIOPATED ENGNEERMG REPPESENTAME(S) IT DESIGNATION NUOMSERSMI t3 ci.AssrncAnotest Brian C. Adamson t5s4Z. EVe., DERT-830137-CE Structures — FM Fon. 81104 (MO) SUPERSEDES PREVIOUS EDrniat SDNY_GM_02753752 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240674 EFTA01326267 SDNY_GM_02753753 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240675 EFTA01326268 US. DEPARTMENT OF 1RANSPOITFADON FEDERAL AVIATION ADIANISTRADON STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I DATE August 21, 2013 AIRCRAFT OR AIRCRAFT COMPONENT 'DEMME/CATION 1 ?WE GLII1SDOSITI 3. MOMS NO. G-IV sin 1085 a ME (Arend &tee. Now:4e. at! Airplane 5. NAME OF APPLICANT International Jet Interiors, Inc. Ronkonkoma, NY UST OF DATA 6 IDENTiRCADON Y. TOSE Drawing: IJIGN1085C Rev(IR) 06/10/2013 IJIGN1085E Rev(IR) 06/28/2013 Report IJIGIV1085GSA Rev(IR) 08/1W2013 Structures Note: Divan Intl-LH Aft sht 1 - 3 Divan Armrest instl-LH Aft sht 1 - 4 Structural Analysis Divan Intl-LH Aft Gulfstream G-IV Aircraft 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineenng data. It Indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements". 2) This torn does not constitute FAA approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the enure alteration. The requirements of Flammablity are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not Included In this approval and requires separate approval. S. PURPOSE OF OATA To provide type data for FAA approval of structure in support of a Major Alteration for Guffstream G•h/ s/n1085. 9. APAlldJJ3LE REPAREUEMS NM RCM staked) . 14 CFR Part 25, Amdt 25-1 through 25-56 as specified In TCDS Al2EA; Paragraphs: 25.301(a-b) Amdt 25-23, 25.303 Amdt 25.23.25.305(a. b) Amdt 25-54, 25.307(a, b) Amdt 25-54, 25.341 Arndt 25-0, 25.561(a-c) Arndt 25-23, 25.601 Amdt 25-0, 25.603(a-c) Arndt 25-48, 25.005(a) Amdt 25-46, 25.609(a) Amdt 25-0, 25.811 Amdt 25-23, 25.813(a. b. d, a) Arndt 25-46, 25.615(a) Amdt 25-23, 25.819(ac) And 25-23, 25.623 Arndt 25-0, 25.625(a-C) Amdt 25-23, 25.785 (i1.13) Amdt 25-51, 25.789(a) Arndt 25-46. to currocKriou • under aulthety Part 183. data Wed Sae and on ilith spoest4eroperrents of to A/worminess 0 Recommend I (We) Therefore E Appease waled by Creedal of the Adak:trate and arm:fed Mods mnaftbeded Na move bean In moxdance Mt condemns end frnerms of this:thareri sedir SI CIR1t eminthed in actiordance MU' eatitthice postathes end Inflows, i Standards lett approval of Mene date these data II. SIGNATURE(S) OF MIGRATED ENGINEERING REPRESENTARYEMLia MIGRATION NUIMERSM II- CLASSIECATIONISI Brian C. Adamson DERT-830137-CE Structures FAA Fan,, *110-3 (02-40 SuPERScosSeREVIOuS 13-4v2 -r SDNY_GM_02753754 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240676 EFTA01326269 SDNY_GM_02753755 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240677 EFTA01326270 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL Melee AJMONISTRA110.1 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I. DATE August 20, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Gulfstream 3 MODEL NO G-IV sin 1085 4- TYPEPee, GAM After. M[.) Airplane I NAME OF APPLCANT International Jet Interiors. Inc. Ronkonkoma, NY LIST OF DATA 6 CANTIFICATION 7 TITLE Drawing: IJIGIV1085L Rev (IR) 06/27/2013 IJIGIV1085G Rev (IR) 07/16/2013 Report' IJIGIV1085LSA Rev (IR) 08./12(2013 IJIGIV1085GSA Rev OR) 08/08/2013 Structures Note: PSU Mod Intl sht 1 - 4 Monitor Mod Inset-LH Aft sht 1 - 3 Structural Analysis PSU Mod Instl Gulfstream G-IV Aircraft Structural Analysis Monitor Mod Instl-LH Aft Gulfstream G-IV Aircraft 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. it indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and Subparagraph listed below as 'Applicable Requirements". 2) This form does not Constitute FAA approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and requires separate approval. S. PURPOSE OF DATA To provide type data for FAA approval of structure in support of a Major Alteration for Gulfstream G-IV sin lass. 9. APPUCA9tE REOUIRAJAEITIS (UN some sem) 14 CFR Part 25, Amdt 25-1 through 25-56 as specified in TCDS Al 2EA: Paragraphs: 25.301(a-b) Amdt 25-23. 25.303 Amdt 25-23, 25.305(a, b) Amdt 25-54, 25.307(a. b) Amdt 25-54, 25.341 Amdt 25-0, 25.561(a-c) Amdt 25-23, 25.601 Amdt 25-0, 25.603(a-c)Amdt 25-46, 25.605(a) Amdt 25-46, 25.609(a) Amdt 25-0, 25.611 Amdt 25-23, 25.613(a, b. d, e) Amdt 25-46, 25.615(a) Amdt 25-23. 25.619(a-c) Amdt 25-23, 25.623 Arndt 25-0, 25.625(a-c) Amdt 25-23, 25.789(e) Amdt 25-46. 10. CERTIFICATION • Under awe* eel by diem a( Re AOrrarasnIof and In amorderat MU mete and lealtalens of notentment under 14 CFR Pan 163, data led above and on Shea shaets numbered _e_ have been seined In accoNance eh estakeed PoCeAdUtall and foe to coney MO% onkablorterements d the Almodesse Steeds Idled. 0 Recommend approval of these data I °Ye) Ilmeore 0 Approve thou data 11. SIGNATURE(S) OF DESIGNATED ENGINEEFteIG REPRESENTATNE($1 12. DESMNATION MILMERS(S) 13. CLASSIFCATION(S) Brian C. Adamsof c::e________ DERT-830137-CE Structures FAA Form 6110-3 (00110) SUPERSEDES PREY/DVS EDITION /3-ern.-* SDNY_GM_02753756 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240678 EFTA01326271 SDNY_GM_02753757 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240679 EFTA01326272 U. S. DEPARTMENT OF TRANSPORTATION FEOERAt. AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I OATE 8/1512013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE Gultstream 1 NODE,. NO. G-IV 4 TyPE(Amame. Engine. Not* ere.) Airplane 5 NAME OF APPuCArrr International Jet Interiors UST Of DATA 6 IDENTIFICATION Design Data $280145 Rev NC Skandia, Inc Flammability Bunsen Burner Testing Test Specimen P/N S (represents Notes: 1) Work accomplished under 2) Flammability test witnessing 3) IAW Skandia Flammability Test Results forward/art storage) Skandia Inc. WO 0 260145-13. Ref Document ID 94116. only, does not constitute installation approval of materials. Streamline Testing Test Plan 21306. Rev IR. Dated 11/03/11 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for S/N 1085 9.APPUCABLE REQUIREMENTS (UM spseibc sections) 14 CFR Part 25.853 (a) Arndt 25-116 Appendix F Pan I (a)M0) Arndt 25-11 I 10.CER11FICATION • Under authority vested by direction of Ilse of appointment under 14 CFR Pan 183, data listed above and on examined in accordance with established procedures and found Standards listed. 1(We) Therefore 0 Recommend approval of these data *Approve these dale Administrator attached to comply end in accordance with conditions and limitations sheets numbered have been with applicable requirements of the Airworthiness ii.SiGNATUISE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE 12.0t&IGNATiON NUMBERS) i3.ClASSIFICATION(S) /is, 1.- tkS/1 ck I . i \K-Aili Iti() Jane Bibehtein -FAA DER DERY-032780-CE Structural Special FAA Form 8110-3 (03/10) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753758 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240680 EFTA01326273 SDNY_GM_02753759 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240681 EFTA01326274 U S DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS ELATE 8/13/2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE Gulfstream 3.MOOEL NO. G-IV 4.TYPE(AtTano. Ear,. Awe*? tic) Airplane 5 NAME OF APPLICANT International Jet Interiors LIST OF DATA 6 IDENTIFICATION 711T1F Design Data S260097 Rev NC SKandia, Inc. Flarnmabildy Test Results Bunsen Burner Testing Test Specimen P/N's B (represents potty seats. fwd/aft) ' 13 (represents conference table) 14 (represents potty seats. fwd/af 0 Notes: 1) Work accomplished under Skandla Inc. WO # 260097.13. Ref Document ID 94098. 2) Flammability test witnessing only, does not constitute installation approval of materials 3) UAW Strand* Flammability Streamline Testing Test Plan 21306. Rev IR. Dated I unit &PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for S/N 1085 1 9.APPLICAEILE REQUIREMENTS (List specific secesns) 14 CFR Pan 25.853 (a) Arndt 25-116 Appendix F Pan I (a)(1)(ii) 14 CFR Part 25.853 (a) Arndt 25.116 Appendix F Pan I (a)(1)(i)Amdt 25.111 tO.CERTIFICATION - Under authority vested by direction of the Administrator of appointment under 14 CFR Pan 183. data listed above and on attached examined in accordance with established procedures and found to comply Standards listed. 0 Recommend approval of these dela 1 (We) Therefore ,... • )2C1pprove these data and in accordance with conditions and limitations sheets numbered have been with applicable requirements of the Airworthiness i 1.SIGNATURE(5) OF DESIGNATED ENGINEERING REPR SENTATIVE 12.06 IONA 10 NUMBER(S) 13.0 IFATION($) ..1..___. \ (') 3. k3. W ug J Jane Stherstet ...FAA DER DERV-832780-CE Structural Special FAA Form 8110.3 (0110) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753760 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240682 EFTA01326275 SDNY_GM_02753761 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240683 EFTA01326276 U. 5_ DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I.DATE 9/19/2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.A4AKE Gulfstream 3.MOOEL NO. G-IV 4.TYPEMATA44. &Ott Prootate. et) Airplane 5.NAME OF APPLICANT International Jet Interiors LIST OF DATA ILIDENTIFICATION 7 TIME 1? 22867 Rev B Dated 08(01/2013 Skandia, Inc. Flammability Test Report Oil Burner Testing and Vertical Burner Testing Notes: 1) Work accomplished under Skandia Inc. WO X 258304-13, Ref Document ID 94288. 2) Flammablity test witnessing only, does not constitute installation approval of the materials. 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair 8 Alteration for SIN 1085 SAPPLICABLE REQUIREMENTS Oast specific sections) 14 CFR Part 25.853 (c) Amendment 25118 Appendix F Part II 14 CFR Part 25.853 (e) Arndt 25.118 Appendix F Part I (a)(1)(11) 10.CERTIFICAT1ON - Under authority vested by direction of the Administrator of appointment under 14 CFR Part 183. data listed above and on attached examined In accordance with established procedures and found to comply Standards listed. 0 Recommend approval of these data I 04 Therefore 0 Approve these data and in accordance with conditions and limitations sheets numbered have been with applicable requirements of the Airworthiness tt.SIONATURE(S) OF DESIGNATED ENOINEERmo REPRESENTATNE 12.0ESKINATION 'WM8EP(S) 13.CLASSIFICATION(S) t pci tyr• J niferPaluzzi -FAA E DERV-832779-CE Structural Special FAA Form 81104 (03710) SUPERSEDES PREVIOUS EDMON SDNY_GM_02753762 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240684 EFTA01326277 SDNY_GM_02753763 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240685 EFTA01326278 Li S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I DATE 9(19/2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION ?MAKE Gulfstream 3.MODEL NO G-IV 4.7 YPE(Avatmo. &Vat PI T etc 1 Airplane 5. NAME OF APPLICANT International Jet Interiors UST OF DATA 6 IDENTIFICATION 7 ITT Design•Data S261931 Rev NC Skandia, Inc. Flammability Test Results Bunsen Burner Testing Test Specimen P/N 17 (represents floor covering being installed unbondedl Notes. 1) Work accompliShed under Skandia Inc. WO # 261931-13, Ref Document ID 94289. 2) Flammability lest witnessing only, does not constitute installation approval of materials. 3) IAW Skandia Flammability Streamline Testing Test Plan 21306, Rev IR, Dated 11103111 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair 8 Alteration for SIN 1085 9APPLICABLE REQUIREMENTS plat SPCCAC WOODS) 14 CFR Part 25.853 (a) Arndt 25-118 Appendix F Part I (a)(1Xii) _.. 10.CERTIFICATION • Under authority vested by direction of the AdmIniShater of appointment under 14 CFR Part 183, dale listed above and on attached examined in accordance with esiebilshed procedures and found to comply Standards listed. I (We) Therefore 0 Recommend approval of these data *Approve these data and in accordance with conditions and limitations sheets numbered have been with applicable requirements of the Airworthiness It SiGNATuRE(S)OF DESIGNATED ENGINEERING REPRESENTATIVE 12.0ESIGNATION NUMBER(S) i3.ClASSiFiCATIOR(S) • t'l i.1‘ ...._ , k ../.) '11211-0—.) Jane Bibtrsteln -FAA DER DERV-832780-CE Structural Special FAA Fo 8110.3 (03110) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753764 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240686 EFTA01326279 SDNY_GM_02753765 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240687 EFTA01326280 IL S DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I DATE 9/ 18/2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE Gutfstream 3 MODEL NO G-IV ATYPE/Anw. Foyers. ens etc) Airplane SNAME OF APPLICANT International Jet Interiors lir OF DATA 8 ICENIWICATION 7 Ern F Design Data 5281824 Rev NC Skandia, Inc. Flammability Test Results Bunsen Burner Testing Test Specimen P/N's 18 (represents floor covering. cockpit) 19 (represents floor covering, ducts) Notes: 1) Work accomplished under Skandia Inc WO # 261824.13. Ref Document ID 94282. 2) Flammability test witnessing only, does not constitute Installation approval of materials 3) IAN/ Skandia Flammability Streamline Testing Test Plan 21306, Rev IR, Dated 11103111 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair 8 Alteration for S/N 1085 9APPLICABLE REQUIREMENTS (List specific seetion11 14 CFR Part 25.853 (a) Arndt 25-116 Appendix F Part I (8)(1)00 10.CERTiFICATION • Under 8UlhOlity yelled by direction or the Administrator of appointment under 14 CFR Pao 183, data listed above and on attached examined in accordance with established procedures and found to comply Standards listed. i 004 Therefore 0 Recommend approval of these data pApprove theSe data and in accordance with Conditions and limitations sheets numbered have been with applicable requirements of the Ainvocthiness 11.81GRATURE(8) OF OESIGNATED ENGINEERING REPRESENTATNE 120ES(GNATION NUMBER(S) Is CU>SSiFICATIONa) 9 ,44fi s fej ein • J niter Paluzzi -FA DER DERY-832779-CE Structural Special FAA Form 81104 (nto) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753766 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240688 EFTA01326281 SDNY_GM02753767 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240689 EFTA01326282 U S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS '.DATE 9117/2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2MAKE Gulfstream 3 MOOEL NO. G•IV 4.TYPE(MPIms. &WOK Propose. ere) Airplane 5.NAME OF APPLICANT International Jet Interiors LIS1rnI FATA 6 IDENTIFICATION 7 TITLE Design Data S257726 Rev NC Skandia, Inc. Flammability Test Results Bunsen Burner Testing Test Specimen P/N's 2 (represents crew seats) 3 (represents jeppesen box, aft baggage) 4 (represents aR baggage) 5 (represents Ned closet and Finlay storage) 8 (represents rain curtain) 7 (represents fwd lay side panel, blkhds, aft lay all bulkhd) 9 (represents headliners, valences, pates) 10 (represents hand rails) 11 (represents window line, aft lay side wall) 12 (represents lower side wall panels) 15 (represents aft cabin blkhd. Md aft galley blkhd) 16 (represents divan end arms, divan lower doors, lower side walls) 20 (represents entry area, baggage floor) 21 (represents aft galley, lav countertops) 22 (represents aft, lay closet sliding doors) 23 (represents baggage nap) 24 (represents hod cabin bulkheads) Notes: 1) Work accomplished under Skandia Inc. WO 0 257726-13, Ref Document ID 94278. 2) Flammability test witnessing only, does not constitute installation approval of materials. 3) IAW Skandia Flammability Streamline Testing Test Plan 21306, Rev IR, Dated 11/03/11 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for SIN 1085 9.APPLICABLE REOUIREMENTS(tisi specific sections) 14 CFR Pan 25.853 (a) Arndt 25-116 Appendix F Pan t (a)(t)(i) Amdl 2`5-111 14 CFR Part 26:853 (a) Arndt 25.116 Appendix F Part 1 (a)(1Xii) IOCERTIFICATION • Under authority vested by direction of the Administrator of appointment under 14 CFR Part 183, data listed above and on attached examined in accordance with established procedures and found to comply Standards listed. I (We) Therefore CI Recommend approval of these data y ..Approve these data and In accordance with conditions and limitations sheets numbered have been with applicable requirements of the Airworthiness i i .SIGNATURE(S) Of DESIGNATED ENGINEERING REPRESENTATIVE 12.DESIGWVION NUMBER( $) I 3.0 SSI ION(S) c r") ,14/1- a 1 Ai) Jane Bi4rstern FAA DER DERY-832780-CE Structural Special FAA FOND 8110-3 (03/10)SUPERSEDESPREVIOuS EDITION SDNY_GM_02753768 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (x124(169() EFTA01326283 SDNY_GM_02753769 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240691 EFTA01326284 wait STATES CF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE NATIONALITY MO NEW:STRAD:Al MARKS N212JE 5 AUTHORITY AND BASIS FOR ISSUANCE Tm troenness wics1464sn1pocoel ti U SC. 1N 101v/ cots ta. d be On <I Sam to mot 44 %No Aug tab* rsmad and bac 99 orkm try to ceSS:V• Dotty. • el n anidoi tilde toribi.v1 W bol *We 11NI Nilootn015iN Art ceryntrit aNdebNd ~Sea Da as "Wad Wain It N Cznyterko M Ines CAA ASIA JINN N ION 1446/. SAS 2 OAANUFAC IVREA AND MCOEL Gulf stream G-IV 1 AIRCRAFT SERIAL KAISER 1085 1 CATEGORY, Transport NONE 6 TERMS AND CONDITIONS Wets Nay seen6N41 442.4444 Al a a woe ts Menem WatilhOity NAGA As artiothea AMES ad. a in /1 At tefrOrl• gre•eirMita Antall a* prima coact AM Pan 1.4.9•40 • SI cl !WAN Mar 9 as at II IN UMW] SIAN DATE OF ISSUANCE R 05/23/2000 AllIbrikhrAndanns.se cootait /*be *by. Ite 4ci auttfrq fl12 a a tales 144•192 CEPRFICATE MAT et DISOLA AF DC PI CROWE MTN APPLOStEFECOAL BA PGIAAACK5 FM Form 51004 (044 I ) SW* DESIGNATION WISER S019 • Ed1:01 SDNY_GM_02753770 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240692 EFTA01326285 SDNY_GM_02753771 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240693 EFTA01326286 ...me new ;arc COMTIST a TIWC•0011.010%-etptiltaiL ikna,TIM•0•01.8MATOI STANDARD IURWORTHINESS CERTIFICATE T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00240694 EFTA01326287 I SDNY_Ghl_02763 3 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240695 EFTA01326288 elsr MAJOR REPAIR AND ALTERATION arOwerwent unsoonnon (Airframe, Powerplant, Propeller, or Appliance) Fedmil minion AdmitAttr•Ilon weft& 2, 204t20 E*to ino 1 4 Emmett Teeming MINX( wefts wean INSTRUCTIONS- Print or type all entries. See Title 14 CFR §43.9. Pal 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) fOr instructions no disposition of INs form. This report Is required by law (49 U.S.C. §44701). Failure to report un result in a ail penally for each such violation. (49 V.S.C. 146301(a)) 1. Aircraft Nationality and Registration Mark USA N423TT Serial No. 1085 make GULFSTREAM Model GIV Series GIV 2. Owner Name (As snown on registration certificate) JEGE LLC Address (As shown on registration CLYMCOM) Aeress or, ST , rows Sole Fonda„ hp 00002 Caney VIRGIN SAWS 3. For FAA Use Only 4. Type S. Unit identification Repair Alteration Vial Make Model Serial No. O 0 AIRFRAME (As described in Item 7 above) 0 O POWERPLANT O O PROPELLER O O APPLIANCE Type Mil/IttliCtOrOf 6. Conformity Statement A. Agencys Name and Address B. Kind of Agency ewe GuLFSTREAU V. S. Certificated Mechanic I MilMEOChiref Agm,... OK PtitelYI 00 Foreign Corteretrod Mechenic C. Cenificale No. Car WEST PALM BEACH um FL X CM/4MM Repair Swim z • wee Ca011y USA Confutes Mardimanca Orme/nen PB8R624N O. I certify that the repair and/or alteration made to the unit(s identifier' in item S above and described on the reverse a atlachrneMs hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is but and correct to the best of my Extended range fuel per le CkR, n 43 AFP' Bist bog ❑ Signature/O rlz WM Thomas J. Choynowski 06/13/2013 7. • oval for Return to Service Pursuant to the autherily g'ven persons specified below. the unit identified in item 5 we! Inspected in the Manner prescribed by the Administrator Of the Federal Aviation Administration and * plApproved riRejected BY FAA Fit. Sundards InSpeCtOr Manufacturer Maintenance Organiza tion Foment APOMved by Canadian .Desionnient of Tranicen FAA Designee X Repair Sleben Inspection Authorization Omer (Specify) CertifiCate or Designation No. PB8R624N Signature/Dale of ' d Individua ,r.77s. oar.; Jim Fishburn 06/13/2013 FAA Form 337 (10/06) Page I SDNY_GM_02753774 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 it EFTA 00240696 EFTA01326289 NOTICE Weigh end balance or operating arretation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the sleekest:Oa airworthiness requirements. a. DncripUon of Won Accomplished Of more space i9 required. attach adthbonal MOWS Men* wan aware nabonatly and registration mark and date work completed.) USA mann 0611312013 NolienaltY and negastratein Mark Oat. Aircraft Make: GULFSTREAM AEROSPACE Aircraft Model: GIV Aircraft Serial Number: 1085 Reference Gulfstream PSI Wodc Order: SCI3300 Complied with STC ST04257AT-D - Installation of GAViS System- IAW Gulfstream Aerospace Index List CE513358001, Rev. A dated April 9, 2012 and Gulfstrcam Document CE4960458 dated 06/13/2013. The display for the GAViS System is installed JAW ASC 476A and Customer Engineering Drawing List DL No. CE41 4960458 approved by Gulfstream form 8100-9 dated 06/13/2013. Reference Airplane Flight Manual Supplement CE51335M%14, Rev.-, dated April II, 2012 and Accepted Instructions for Continued Airworthiness CE51335A001, Rev. A, dated April 5, 2012. Items Removed: Qty. Description 6 Ea. DU-880 I Ea. FMS Data Loader DL-950 2 Ea. CRT Fan Commutating Module 2 Ea. Fan Any. 2 Ea. ATC Transponder Manufacturer Honeywell Gables Rotron Rottman Collins Pan Number 4053000-901 07226.02 508534 508617 622-9210-309 Weight/Lbs. 30.4 (Ea.) 1.17 1.5 1.15 8.5 (Ea.) F/S 90.0 166.0 147.5 73.0 40.5 Items Installed Qty. Description Manufacturer Pan Number Weight/Lbs. F/S 6 Ea. DU-885 Honeywell K9321061A02 19.6 (Ea.) 90.0 I Ea. XM Data Receiver Honeywell 4092743.901 1.5 151.0 I Ea. XM Antenna Honeywell C1420-1 0.2 174.5 I Ea. FM Data Loader DL-I00 Gables G7228.02 1.17 166.0 2 Ea. Cursor Control Device Esterline 73E8202 2.6 109.0 I Ea. Video Amp Audio Intl VA-401-2 0.6 112.0 2 Ea. ATC Transponder Collins 622.9210.409 8.5 (Ea.) 0.5 Notes: I. The electrical load analysis statement is contained in Gulfstream Document CE4 I 4696425. 2. Deviations to STC 476A arc shown in Cull-Stream Document CEA I 6990073. 3. Deviations to Gavis STC ST04257AT-D arc found in Gulfstream Document CE4 I 3350049. 4. A logbook entry reflecting this installation was completed and entered into the aircraft logbook. 5. The aircraft Equipment List has been updated to reflect this installation. 6. Weight and Balance data has been revised and inserted into the Weight and Balance Manual. 7. Maintenance instructions for continued airworthiness are contained in FAA Accepted Instructions for Continued Airworthiness CE51335A00 I Rev. S dated April 05, 2012 (or later). 8. FAA Approved Flight Manual Supplement CE51335M004 A dated April II, 2012 has been inserted into the AFM. ClAdotuonattneets AM Attached _ 4.,.1 FAA Form 337 (10/06) Page 2 SDNY_GM_02753775 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240697 EFTA01326290 0 MAJOR REPAIR AND ALTERATION US Dated Miry aponasan (Airframe, Powerplant, Propeller, or Appliance) Rani Avid... MIEMIstaillon Rim hetione Or ha 2NOCON Ora /2007 marecoic inewhe /*mini IAA We Only INSTRUCTIONS: Print or type as entries See Title 14 CFR §43.9. Pan 43 Appendix 8. and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of this form. This report iS reputed by taw (49 U.S.C. §447O ). Failure to report can result in a civil penally for each such violation. (49 U S.C. §463O1(a)) 1. Aircraft Nationality and megistrabon Mark USA N423TT Serial NO. 1085 Make Gulfstream Aerospace Model G-IV beats 2. Owner Name (As shown on registration ceshficate) TRT Leasing Address (As sheen on reipsfrolkon testate) Kona 515 N Flagler Drive, STE P400 Car West Palm Beach stew Florida no 33401-4320 Carty USA 3. For FM Use Only The actrankal date herein gas keen mood to comply wok applailagra tirwortif4. P. racjwiredicate and is hon:by enameled MT N69 Cillbr PI tie above described aircraft, subject to conformity tfaaft00840414 a ea anction33.7. , \n, - aim tr io,S.AlAit _- ,S‘x 4. Type S. unit Identification Repair Mention Unit Make Model Serial No. O 0 AIRFRAME (As clescnbed in Item 1 abetter) 0 . POWERPLANT E O PROPELLER o O APPLIANCE Type Uanufackre• 6 Conformity Statement A. Agencys Name and Address B. Kind of Agency iaoki CE Amnia Inc. U. Comecon:I Mechanic I ManAacturve ArMnn 2789 Frightline Avenue Foreign Contralto MeChailiC C. Certificate No. eta Sanford tam FL x Cartnicateci Repay Stanco OE4R411M Al 32773 twiny USA Congested Maimenance Organdaton D. I certify that the repair andlor alteration made to the tine s) Identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the remarements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel pet 14 CFR Part 43 O APP. B Signe a o Irld.iduat 2 JAN 2 9 1013 7. Approval for R urn to Service PUIllant to the authority given persons specified below. the unit identified in item 5 was inspected in the manner prescribed by the Administrator of Federal Aviation Administration and is I21 Approved El Rejected BY FAA Fit. Stanclals InSpOCICH Manufacturer Maintenance Organization Poisons Approwed try Canadian OSpartinent Of Trengal FM Designee X Repair Station Inspection Authorization other (specify) Certificate or Destgnation No. 0E4R411M Signature/Date of AlithOrized InteVidell —leen..-4 4c/ -. 4" --c----- JAN 2 9 2013 orm 5370040 SONY_GM_02753776 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 1O, 15, and 17 EFTA_00240698 EFTA01326291 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements B. Description of Work Accomplished (If more space is requited. Mach adcktional sheets. mien:Wrath aircraft nationality and reefs:catkin mark and date work completed) USA N423TT JAN 2 9 2013 NationaMy and Registration Mark Date Removed 2 each, CMC Electronics CMA-1100 EFB EEMU's and Part No. 217-601933-215 Cable Assemblies previously installed on FM Form 337 dated April 9, 2007 (CRS X91R092Y). Removed circuit breakers, capped and stowed power wires. Remaining connectors bagged and properly secured. END O Additional Sheets Are Attached 0 Pages FAA FOOT, 3371,0.41 SDNY_GM_02753777 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240699 EFTA01326292 0 Ow MAJOR REPAIR AND ALTERATION A°YBwn zwrir 11f'101001 VS Bean Warsaw tweet Oteatirnee 0/f/lAWS1Sell a Traritieerd01 (A irf rame, Powerplant, Propeller, or Appliance) Nerd A* Admisslaretle. INSTRUCTIONS: PAM or type as entries. See TAB 14 CFR §43.9. Part 43 Appendix B. and thereof) for nstruCtions and disposnon of (Ns form. This report is required by law (49 U.S.C. §4470 la earn such violation. (49 U.S.C. §463O1(a)) AC 43.9-1 (or subsequent revision ). Fein I0 feint CIA Mull in a bvil Panay 1. Aircraft Nationality and Registration Mark USA N423TT Senal No 1085 Make Gulfstream Aerospace MOCtel G•IV bents 2. owner Nun* (As shown on tegostrobon cerfincato) TRT Leasing morass (As Shown on regeshalfron certificate) Arms 515 N Flagler Drive, STE P4OO cay West Palm Beach our Florida SO 334O1.432O Qatar USA & For FAA Use Only Ihi essioleal dati herein on t‘z.tia aataa: la MAIO TO eltalYASIO shwoutli,,, c reavivreetents ant iii lamb; topiva.t1 IN IP9 fflil/ itil 'be above atscapal A aircraft, subloct to gugonnity ii,Vi0 WA W ti a seoloa33.7. r SS `TM ASU•ADO-15 4. Type 5. Unit Identification Repair Alteration Unit make Moat Serial No • g AIRFRAME (As descnoed in Item I above) • O PONERPLANT 0 0 PROPELLER • 0 APPLIANCE Type laantartebaer 6. Conformity Sta ement A. Agency's Name and Address 8. Kind of Agency caw CE Avionics Inc. U S. Certificated Mechanic I Mantairclumr mews 2789 Flightline Avenue Altair bananas mechanic C. Certificate No. oo Sanford Va.• FL x Ocala; OW OE4R411M re 32773 cony LISA Ceti/dated Pilaintensnc•Oroandaeon D. !certify that the repair and/or alteration made to the unit s) identified in Rent 5 above and described on the reverse a attachments neitio have been made n accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and coned to the best of my knowledge. Extended range fuel per 14 CFR Part 43 APP. 8 Signature/Date of Authorized Individual 7 1-z:-/-ie f e7K/ JAN 1 9 NU 7. Approval for Return t Service Pursuant to the authority given persons specified below, the unit identified in item 5 was nspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Approved 0 RejeCted FAA Fe Standards Inspect Manufacturer 8v Maintenance Organization Persons Approved by Canacban ment of Transport FAA Designee X Repair Station Inspection Authorization Other (Speedy) Certificate ix Designation No OE4R411M Signature/Date of Authorized I 7. JAN 2 9 2013 one 337nocei SDNY_GM_02753778 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240700 EFTA01326293 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished RI more space is required. Misch additional sheets. Identify yarn am a nat y and repstrat ion mark and date non( completed) USA N423TT JAN 2 9 2013 Nationally al Regesiration Mark Date Removed AirCell P12192-002 Corded Handset and replaced with P121357-002 cordless handset. Installed AirCell ATG 4000, Pan Number P13989 Air-To-Ground (ATG) Broadband Transceiver in the aft fuselage equipment bay at F.S. 724 with AirCell ACM. Part Number P14126 Configuration Module in the forward cabin RH equipment bay at F.S. 159. Mounted two each AirCell Pan Number P12344 Remote Diversity Antennas on the inside of the forward right hand storage cabinet at station 193A+7.0. Installed two each. AirCell Pan Number P12949 ATG UHF Antennas on the bottom of the fuselage per DDH Group Drawing Number ER02222-001, Revision 0 (Approved on FM Form 6110-3 dated January 18. 2013 by David E. Haralson, 0ERT-810028-SW. Structural at F.S. 598 and 749. Interfaced the AGT 4000 System per the attached CE Avionics. Inc. Drawing Number 66268-1VVD, Revision IR (Approved on FM Form 8110-3 dated January 18, 2013 by Leslie S. Roblin, DERT-510335-SW, Avionics/Electrical Systems & Equipment). The system is powered by the cockpit controlled cabin bus. Cabin wireless intemet is not enabled at this time pending incorporation of approved STC. Primary AGT 4000 power is connected to il 5-amp circuit breaker and primary ACM power connected to a 1-amp circuit breaker per manufacturer's specifications. Electrical load computed and found to be within acceptable limits. Instructions for continued airworthiness for the ATG 4000 System are contained in the attached CE Avionics Inc. Document Number 64961-1ICA. Installation of the above made in conformance with AirCell ATG 4000 Installation Manual Pan Number 013928. Revision C dated April 2011; AirCell kocess Installation Manual Part Number 012004, Revision E dated March 2010; AirCell Antenna Installation Manual Pan Number 800-10355, Revision E dated May 2009; Gulfstream IV Maintenance Manual. Revision 63 dated September 30. 2012, Chapter 6, Sections 06-00-00 and 06-50-00; Chapter 20, Sections 20-24-00, 20-25-07, 20-28-00, 20-28-09, 20-42.00 and 20-70-11; Chapter 24, Sections 24-004)0. 24-02-00. 24-02-01; 24-03-00 and 24-03-02; Chapter 34. Section 34-02-00; Chapter 51, Section 51-00-00; Gulfstream IV Wiring Manual, Revision 46 dated September 30, 2012, Chapter 20. Sections 20-00-00, 20-24-00. 20-25-00. 20-25-01. 20-25-03. 20-25-05, 20-26-00, 20-26-01, 20-26-03, 20-26-07, 20-2741, 20-27-03, 20-28-01, 20-28-05 and 20-28-07; Chapter 34, Section 34-60-00; and in compliance with FAR 25.1301, 25.1309, 25.1351, 25.1353, 25.1357 and 25.1431. ND El Additional Sheets Axe Attached 11 Pages FAA Form 337neen SDNY_GM_02753779 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024070I EFTA01326294 Attachment FM Form 337 (AGT-4000) Dated January 29. 2013, N42377. Gttlistrearn G-IV. SIN 085 Sheet 0111 it ii &! I .•A - ii i .. Hlli "I IOW n ils |||||| iiii if g !Hill Ifilks 1 — • i IF, ..... -- Ati i hp E !E 9 SDNY_GM_02753780 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240702 EFTA01326295 SDNY_GM_02753781 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240703 EFTA01326296 N C n -0 7a 0 n H 70 7a 70 Gl 70 00 LD O /- 1 I ‘.(11 t NJ a Hs IS 2 -011 FWD MRCELL BROADBAND ANTENNA INSTALLATION LOWER FUSELAGE SKIN VIEW LOOKING RIGHT LHS -012 AFT MRCELL BROADBAND ANTENNA INSTALLATION LOWER FUSELAGE SKIN VIEW LOOKING RIGHT LHS h•SIOnon Mil ofteate. Wt_ ca.rea .oto. ass twieftnseyiepots /Le soma. a t. csinsoa. ape hts• Doe wan rannata en, rim oil NOW( I ER02222401 I 0 2 OS 4 1 0 O EFTA01326297 SDNY_GM_027.783 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240705 EFTA01326298 In co n H -O 0 H rn n H 0 7u G') -c) (f) Co nW P I-, 10 Oa '6,4 r 0- / I. • • A0006 COWIT 1.011.0150.01 /0/404/0 • • • •. .• (4/4 ••••. (4- A.. I j ../ / „ec - • It•D i 11 ••• el'el0640 Oen SECTION AA (411) LOWER FUSELAGE COVER PLATE VIEW LOOKING DOWN (Co am •eist• 1MYI.R CMC wont 00, 02017C101,1k w Inc '4—.— 001 001001.111 k02001.104 L001100.0000•14010 paw 14/0011402T10111.11•100.40•01 COMMA, NOLO V.COMPMD CITIL0 0.0 - 00 0 ,1 COW* COMONOt LCCATION Vent0401,•3 • ••••• • • =KW 0118.115 Mr) Natal MG Arnim& pol ' • • • • O O 0 0 0 • • • • •••• " SECTION BB (-011) SECTION 0-0 (412) VIEW LOOKING NORMAL TO ANTENNA ATTACH SURFACE. Nos rte....err me era ors-. are Olirturrar a:mealier am no !PQM Orr. red ter..0.• 0.00. rrO••• ter • 0.0.00./11 6040 interrIO ./ ER02222401 3 OF. i y I EFTA01326299 SDNY GM 02753785 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240707 EFTA01326300 Attachment: FM Form 337 (AGT-4000) Dated January 29. 2013, N423TT. Gut!stream G.IV, SIN 1085, Sheet 4 of 11 SDNY_GM_02753786 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240708 EFTA01326301 SDNY GM 02753787 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240709 EFTA01326302 Attachment FM Form 337 (AGT-4000) Dated January 29. 2013. N423TT. Gu*Stream G.N. S/N 1085. Sheet 5 of I I DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE January 18, 2013 MRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream MODEL NO. G-IV TYPE Verdant Redly licaceper.ek.) Airplane NAME OF APPLICANT CE Avionics. Inc. LIST OF DATA IDENTIFICATION TITLE ER02054-001, Rev — ER02054.002. Rev— ER02222-001. Rev 0 ER02222 Rev 0 Aircell Antenna Tapered Adapter. 12.4 Deg, Sht 1-4 Aircell Antenna Tapered Adapter. 7.4 Deg. Sht 1-4 Aircell Broadband System Antenna Installation, Sht 1.4 Structural Substantiation — Aircell Broadband Antenna Installation for Gulfstream G-IV, sin: 1058 NORM: I) Per FAA Order 8110.37D Chapter 4-12.h. a) This approval is for engineering design data only. It indicates the data listed above demonstrates cornpliance only ugh the regulations spedlled by paragraph and subparagraph listed belOw as Applicable Requirements. b) This bent may not constiluM FAA approval of all ling tearing data necessary to. the substantiation of compliance to necessary requirements for the entire alteration. c) Structural aspects are approved. d) Approval of °lethal aspects and equipment Installed are not included. 2) The instalth must determine the correatibuity S this data with the aircraft configuration. Alter the repak or alteration the aircraft must be retuned to service hymned:tee personnel. PURPOSE OF DATA To approve structural aspects of an alteration to Gulfstream G-IV. sin: 1085 APPLICAIRE REQUIREMENTS (Liu speak armor) 14 CFR 25.301 25.303 25.305(a)(bxc) 25.307(a)(b) 25.601 25.603 25.605 25.607 25.609(a)(b) 25.611 25.613(811) 25.615 25.619 25.625 TCDS Al2EA Certification Basis: 14 CFR Part 25 through Amdt 25-56 (except 25.571 Amdl 25-22) CERTIFICATION • Under authority vested by direction of the Administrator and in accordance with contagions under Part 183 of the Federal Aviation Regulations. data ksthd above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recceimend oppeovelol these delt I ea< Therelom brow,* Item Sm. and limitations of appointment 0 have been exemineo Aviation Regulations. SIGNATUREIS) OF DESIGNATED ENGINEEFUNG REPRESENTATIVES) DESIGNATION NUMBER(S) CLASSIFICATIONS) David E. Haralsonj:):e eg,.. it - DERT-810028-SW Structural FM Form 8110-3 00) SUPERSIOES PREviOUS !ONION 010222240 oat SDNY_GM_02753788 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 10 EFTA01326303 SDNY GM 02753789 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240711 EFTA01326304 Attachment FM. Form 337 (AGT-4000) Dated January 29, 2013, N423TT, Gulfatream Gall, WI 1085, Sheet 6 of 5 a g A a • SDNY_GM_02753790 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 12 EFTA01326305 SDNY_GM02753791 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240713 EFTA01326306 Attachment FM Form 337 (AGT.4000) Dated January 29, 2013, Na233T, Gultatmarn G-N. SIN 1085. Sheet 7 all 3 Ix SS￾41 O 9: E *0! Fp a IyyI ;I'1 SDNY_GM_02753792 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 14 EFTA01326307 SDNY_GM_02753793 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 15 EFTA01326308 Attachment FAA Form 337 (AGT.4000) Oated January 29, 2013, N423TT, Gulfstream G-11/, SIN 109S, Sheet 8 of II SDNY_GM_02753794 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 16 EFTA01326309 SDNY GM 02753795 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 17 EFTA01326310 Attachment FM Form 337 (AGT-4000) Dated January 29. 2013. N423TT. Gulfstream Gar. SIN 1085. Sheet 9 of 1 1 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS L DATE January 18, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MANE Gulfstream Aerospace 3. MODEL NO G-IV 4 TYPE (Aim,* Err* Proponor, Mc/ AIRPLANE 5 NAME OF APPLICANT CE Avionics Sanford, Fl. LIST OF DATA 6 IDENTIFICATION 7. TITLE 66268-1WD. Rev IR, dated 12/27/12 Aircell ATG 4000 High Speed Internet System END Nola: 1) The electrical aspects way erigineereg design data only. Writhe regulations specified Requirements'. 2) Compliance With stsiionsi FM approval of all the engineering necessary requirements for approval. 3) Mar the Alteration, the aircraft 4) Cabin Wireless Internet capability Cerillication. of the above listed data are It Indicates the data listed by paragraph and subparagrarn regulations not listed may data necessary for the The approved herein This approval is for above demonstrates corerlance onq listed below as 'ARROW* be rewired. This form does not constitute substanballon of compliance to stnicturel aspects are not Inckeded In this by FM Authorized personnel. Incorporation of Supplemental Type entire alteration. mull be retuned to senke is NOT enabled; Pending 5 PURPOSE OF DATA Design approval in support of installation modifications to Gullstream G-IV Series aircraft, serial number 1085. registration no. N423TT. Avionics/Electrical Systems 8 Equipment Design Approval Only. 9 APPLICABLE REOUIREMENTS OF !TILE II CFR (del specific seams) FAR 25.869 (a)(4); Arndt 25-72 FAR 25.1353 (b)(d)(1)(2); Amdt. 25-113 FAR 25.1301 (8)(1)(2)(3); Arndt. 25-123 FAR 25.1357 (a) Amdt. Orig. FAR 25.1307 (c); Amdt. 25-72 ici CERTIFICATION -Under aulhority veiled by direchon Cl Ike Admnislator and in accordance war GOIldia04$ WA Ihrstabons of appointment under 14 CFA Pail 183. WO baled abaVO and on ottecned sheers mantesei None have been examined In aCcordenCe Nth eslatdshed procedures and found lo comply yea applicable IOCMIanlatAll al ma Nrwortirmss Standards kited 0 Recommend approval of these data I pot) Mesita 0 Approve these data II. SIGNATURE(S) OF DESIGNATED ILGNEE RING REP S IJTATIVEISI 12 DESIGNATION NUMBERS(S) 13. CLASSIFICATIONS) Lewd S. Roblin Ire SP 1 DERT-510335-CE Avionics/Electrical Systems 8 Equipment FAA Form 8110-3 (03no)SuPERCEDES PREVIOUS ED4DON (ON recelt4 doe) 13010 SDNY_GM_02753796 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 0024071 S EFTA01326311 SDNY_GM_02753797 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240719 EFTA01326312 Attachment: FAA FO1111 337 (AGT-4000) Dated January 29. 2013. N423TT, Gulista:tam G-N. Sm 1085. Sheet 10 0111 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, AIRCELL ATG 4000 HIGH SPEED INFLIGHT INTERNET SYSTEM CE Avionics Inc. Document No. 66278-1ICA, Rev. IIR I. Introduction Aircraft that has been altered: Registration No. — N423TT, Make — Gulfstream, Model —G-IV, Serial No. 1085 Content, Scope, Purpose and Arrangement: This document identifies the Instructions for Continued Airworthiness for the modification of the above aircraft by installation Man AirCell ATG 4000. Applicability: Applies to aircraft altered by installation of the AirCell ATG 4000. Definitions and Abbreviations: None, N/A. Precautions: None, N/A. Units of Measurement: None, N/A. Referenced Publications: AirCell ATG 4000 Installation Manual Pan No. D13485. AirCell Antenna Installation Manual Pan No. 800.10355. AirCell ATG Quick Reference Troubleshooting Guide Part No. D14748. Distribution: This document should be a permanent aircraft record. 2. Description of the Alteration Installation of the AirCell ATG 4000 System with interface to the Number 2 Flight Management System. Refer to Section 10 of the AGT 4000 Installation Manual for interconnect infomiation. 3. Control, Operation Information Refer to Section 4 of the AGT 4000 Installation Manual. 4. Servicing Information N/A 5. Maintenance Instructions Maintenance of the AirCell Alt 4000 System is 'on condition' only. Periodic maintenance is not required. 6. Troubleshooting Information Refer to Appendix A of the ACT 4000 Installation Manual. 7. Removal and Replacement Information Section 3 of the AGT 4000 Installation Manual. If the unit is removed and reinstalled, a functional check of the equipment should be conducted in accordance with Section 4 of the AGT 4000 Installation Manual. 8. Diagrams Refer to Section 10 of the AGT 4000 Installation Manual. 9. Special Inspection Requirements N/A 10. Application of Protective Treatments N/A II. Data: Relative to Structural Fasteners N/A 12. Special Tools N/A Page I oft SDNY_GM_02753798 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240720 EFTA01326313 SDNY_GM_02753799 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024072! EFTA01326314 Attachment: FAA Form 337 (AG7-4000) Dated January 29. 2013. N423TT, Gulfstream S/N 1085. Sheet 11 oftt 13. This Section is for Commuter Category Aircraft Only A. Electrical loads: N/A. B. Methods of balancing flight controls: N/A. C. Identification of primary and secondary structures. N/A. D. Special repaii methods applicable to the airplane: N/A. 14. Overhaul Period No additional ovedmul time limitations. IS. Airworthiness Limitation Section N/A. 16. Revision To revise this ICA, a letter must be submitted to the local FSDO with a copy of the revised FAA Form 337, and revised ICA. The FAA inspector accepts the change by signing Block 3 and including the following statement: "The attached revised/new Instructions for Continued Airworthiness (date X X-XX-XX ) for the above aircraft or component major alteration have been accepted by the FAA, superseding the Instructions for Continued Airworthiness (date X X -X X - X X )" 17. Assistance Flight Standards Inspectors have the resources to respond to questions regarding the ICA. 18. Implementation and Record Keeping For major alterations performed in accordance with FAA field approval policy, the owner/operator operating under Part 91 is responsible foi ensuring that the ICA is made part of the applicable section 91.409 inspection program for their aircraft. This is accomplished when a maintenance entry is made in the aircraft's maintenance record in accordance with section 43.9. This entry records the major alteration and identifies the original ICA location (e.g., Block 8 of FAA Form 337, dated X X-XX-XX ) along with a statement that the ICA is now part of the aircraft's inspection/maintenance requirements. Page 2 of 2 SDNY_GM_02753800 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240722 EFTA01326315 SDNYGM02753801 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240723 EFTA01326316 MAJOR REPAIR AND ALTERATION or Iron...rein,' (Airframe, Powerplant, Propeller, Or Appliance) Friend ANS* Aaninistracien FrmApasual OMB No 2120=0 Ilan/200? Elmircnic Trader; tancra FAA Use Only INSTRUCTIONS: Print or type al entries. See Title 14 CFR §43.9. Parl 43 Appendix B, and AC 43.9-1 (ce subsequent revision thereof) for nstructions and disposition of this form. This report is required by law (49 U.S.C. 44470 ). Failure to repel can result in a civ4 penally for each such violation. (49 U S.C. §46301(e)) 1. Aircraft Nationally and Registrabon Mark USA N42317 'Make senaI NO. 1085 Gulfstream Aerospace G-IV Series 2. Owner Name (As shown on registration cerbitcate) TRT Leasing Address (As shown on tegisfrabon certificate) mwen 515 N Flaoler Drive, STE P40O ay West Palm Beach Son Florida so 33401-4320 cans USA 3. For FAA Use Only 4. Typo 6. Unit Identification Repa , Morahan Unit Make Model Serial No. El g2 AIRFRAME (As described in teem f above) El I:l POO/ERRANT El ii PROPELLER 0 0 APPLIANCE Type 'Manufacturer 6. Conformity statement A. Ageneys Name and Address 8 Kind of Agency i... CE Avionics Inc. U S Contra...1 mechrmc I Manufacturer ••••••• 2789 Flightlme Avenue ;weir Certhcala0 M•CnanC C. Certificate No. ou Sanford ash FL x _ Cerebrated Reps. Stabta 0E4R411M a 32773 ohms USA ceinissite4 maintenance Organization D. I certify that the repair andior alteration made to the unfi(s) identified in Item 5 above and °escrow on the reverse a attachments hereto have been made in accordance with the requirements of Pad 43 of the U.S. Federal Aviation Regulations and that the inkurnaliOn furnished herein is the and correct to the best of my knowtedge. Extended range fuel per 14 CFR Pat 43 O APO. B SgnalurelDale of Authonz era i 7‘f a — tk esaV - -Z Michael. E. Hughes January 29. 2013 7. Approval for Return to Service Pursuant to the arthartY g yen persons speciierl whs, the unit identified in item 5 was Administrator of the Federal AVOMIOn Administration and Is 2 Approved • inspected in the manner prescribed by the Rejected BY FM Fit Standards Inspector Manufacturer Maintenance Organization PerionS Append by Canadian DepartmeN of Tronspon FAA Designee X Repair Staban Inspection Authorization r (Bleary) Certificate or Designation No. OE4R411M Sonaluremate of kuthorized i.. ... I es Michael, E. Hughes January 29. 2013 ore 337ncau SDNY_Girl_02753802 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240724 EFTA01326317 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Descent/cm of Work Accomplished of m003 Space is requited. attach additional Sheets aleatory with *Mae nettOrialay and registration mark and date work completed) LSA N423TT January 29, 2013 Naborialey and RegisUalion Mark Date Completed activation of AirCell ATG 4000 Wireless High-speed *nternet in compliance with Duncan Aviation STC Number ST01625W1-D and the following Duncan Aviation Documents: Master Document List Document Number 110121028, Revision E. Follow On Installation and Configuration Document Number 110315014, Revision E. Follow On Ground Test Procedure Document Number 110121020, Revision D. Instructions for Continued Airworthiness Document Number 110121022, Revision C. Duncan Aviation FAA Approved Flight Manual Supplement Document Number 110121021, Revision B placed on board the aircraft in the Approved Airplane Flight Manual Supplements binder. Weight and Balance information not affected. ❑ Additional Steels We reached Pages FAA Form 337 flow SDNY_GISI_02753803 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240725 EFTA01326318 }unlit! Atha of America 4fiepartment of tEransportation Atbernl "thiattion Abininistrution $upplemental 'Type aertifiratt FL err4earwar itauentio Aam4. ST01625V/I-D Duncan Aviation, Inc. 3701 Aviation Road Lincoln, NE 68524 STC No. ST01625WI-D Enable WLAN System for use on Gulfstream G-IV sin 1085 if:4A da/14 okra doinoriviinfraGALAt elatzlihAtikaiw aaaferaiahavat denyevo abl +1041.avera nosa.0 Gee aercontesenu esperthradwa eMent25 e/66 Federal Aviation i iegattrivel. r aviatatileluel- -.54,gienceealeiglnds, Aga Al 2EA Gulfstream Aerospace Corporation GV 91110•9•6•.• 0/3;•• fkleic4gra,s11A' Enable Wireless Local Area Network (WLAN) system for use with Transmitting Portable Electronic Devices (TPEDs). Data Required: (I) Duncan Aviation Inc., Document List No. 110121028, Revision A, dated March 18, 2011, (2) AAA Approved Airplane Plight Manual Supplement, Duncan Aviation Inc., Document No., 110121021, Revision A, dated March 18, 2011, or later FAA Approved Revisions to (1) or (2). SeirIdahh•J 044111:•••414W,' This system is intended to provide internist connection and email services using TPEDs. Any other intended function of this equipment will require a re-examination of the certification basis. Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. FL twes4n4..z.,,,a4myr e,c4,44, add.) [4 law gornivaidarreowan 4. r/~idanahe.n.a4id .vereertied meaty a Ardi.eloiva .44 a tdiertoas eatted.,44. Addeuileata. 04.5;raigoiates SethAtlina 44 eiscpriaohivs Fans.). 1,2011 .944 *ea :wagon. Moat 11,2011 git4 taws( floks an/waled May 27,2011 4 o) atrick M. Chick, Jr. ODA administrator, ODA-501013-CE Duncan Aviation, Lincoln, Nebraska (Mk) anttr K a4 pal Jtttra 4 1•• • Sr a ft.ae tag . or y,tallaat nee toscacligmies. Or Leto. ha rah oho-too-4h Ma I or r air tete certified. ••• to convents: in •ecordase• with IAA V. O. SDNY_GM_02753804 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240726 EFTA01326319 SDNY GM 02753805 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240727 EFTA01326320 DINCAN AVIATION I II Authorization of STC use: Date: January 15, 2013 To: CE Avionics Inc. Attn: Brian Rannie 2789 Flightline Ave Sanford, FL 32773 In reply please reference: 2013-028L Authorization is herby given for one time usage of FAA Supplemental Type Certificate Number ST01625WI-D to enable WLAN System. This installation is approved for Gulfstream G-IV sM 1085 only. Deviations to this subject data are the sole responsibility of CE Avionics Inc. If your engineering department has any questions about this STC, feel free to contact me at r by email at Douglas Bates Engineering Records Tech Duncan Aviation 3701 Aviation RD Lincoln, NE 68524 USA Lincoln Anpoti P.O. Jinx 81887 Lincoln. Nebraska 68501 402.475.2611 Pax 402.475.5541 www.diencannvincion von, SDNY_GM_02753806 1 1 1 1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240728 EFTA01326321 SDNY_GM_02753807 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240729 EFTA01326322 e l leo MAJOR REPAIR AND ALTERATION us Osentro a Trtnspennon (Airframe, Powerplant, Propeller, or Appliance) Fake& Aetna, 1 ids-billed. Form naretwed We to 21204020 traVIO., Navas imam Muster For FAA UR CsiO INSTRUCTIONS: Print or type all envies. See Title 14 CFR §43.9. Part 43 Appendix B. and AC 43.9.1 (or subsequent revision thereon for Instructions and disposition of Mis form. This report is required by law (49 U.S.C. §44701). Failure IC repot can result in a civil penally for each such violation. µ9 U.S.0 448301(0)) 1. Aircraft Nationality and Registration Mart USA N423TT Serial No. 1085 Make GULFSTREAM Model GIV Series 2. Owner Name (As shown on regatrabon certificate) TRT LEASING INC Address (As shown on foist:anon Certificate) Mtn 51S Ist Fl Ant FR nR STF PAM O,1 WEST PALM BEACH flee FL no 33401-4320 Cony USA 3. For FAA Use Only 4. Type 5. Unit Identilkation Repair Alteration Una Make Model Serial No. El 0 A/RFRAME (As eaSenDed,n nem i abate) O O POIAERPtAP4T O O PROPELLER 0 O APPLIANCE Type Manutedwar S. Conformity SO ement A. Agency's Name and Address B. Kind of Agency sere (WI FSTRFAM U.S. Cenicated Nahum I mentiouunse AMMO 1500-C PERIMETER RD. Fcreign Cenificese Methane C Cenific.ste No. car WFST PM M REACH en Fl / CertAcezed Repair Stamm Da 33408 co CRS PB8R624N , USA Cerukraect Meneenenoe Organization 0. I eitetey Mal the repair and/or aaeration made to the unit( ) idenlifienl in item S above and descried on the reverse or attachments hereto have been mode In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished eerekl Is true and correct to the best of my knowledge Extended range fuel pet 14 CFR Part 43 O App. 8 Signature/Ds IAuthorized I iveual m I. 4 Terry Barker 08/15/2012 7. Approval for Return to Service P masa to the authority given specified below. the unit identified in item S was inspected in to manner prescribed by the Administrator of the Federal Aviation ministration and is R Approved Rejected 8Y FAA Flt. Standards Inspector Manufacturer Manufacturer MairiteMACe Organization ..O Permed APIXO7W by Canaan ed Transpon FM Designee I Repair Station Inspection Authorization Other (Speedy) Certificate or Des ignation No. CRS PB8R624N Signal° at Authorized Inc* „. 0,y t p James Fishburn 08/15/2012 FAA Form 337 noon SDNY_GM_02753808 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240730 EFTA01326323 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (If more space is required, attach addiffonal sheets. Identity with aircraft netIona* - and repiygapn Tat* and date work completed.) USA N423TT Nationality and Registrabon Mark Aircraft Model: Gulfstream GIV Aircraft Serial Number 1085 Reference Gulfstream Pal Work Order: SC11231 08/15/2012 Date Complied with STC ST00544LA - Installation of Concorde Battery sealed lead-acid Battery Model No. RG-380E/44 UAW STC ST00544LA and steps II A 2 & 3 of Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E144 Lead acid batteries. Rev A dated August 28 2000. Permanently removed the following equipment: 2 ea. Saft Nickel-Cadmium Main Battery, Model 4076-11 Installed the following new equipment: 2 ea. Concorde sealed lead-acid Battery, Model RG-380E-44 No Weight and Balance change required by this action (weight change negligible). No Airplane Flight Manual Supplement required by this action. Airplane records updated to reflect this action. Aircraft electrical load not affected by this action. Instructions for Continued Airworthiness can be found in Concorde document No. 5-0171 Rev. M. dated 03/15/2012. Note: This amendment, dated 08/1512012, supersedes the original 337 dated 08/06/2012, and the amendment dated 08/08/2012. and removes 'Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E/44 Lead Acid Batteries, Rev. A dated 08/28/2000" from the ICA statement. END ❑ Additlifiel.Shaels Are Attached FAA Form 337 nom SDNY_GM_02753809 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240731 EFTA01326324 \.,--i// form.prowe MAJOR REPAIR AND ALTERATION US eopsersent el TWOKSICA (Airframe, Powerplant, Propeller, or Appliance) Fedstil Mines A•alalwaece OMB No 2I2POCQO WiffaiI Eno.* Tredire veneer fee FM Ur OW? INSTRUCTIONS: Print or type all enthes. See Title 14 CFR 643.9. Pan 43 Appendix EL and AC 43.9-1 (or subsequent revision thereof) for Instructions and dIsposeion of this form. This report is required by law (49 U.S.C. §44701). Failure to report an result in a dig penalty for mach such violation. (49 U.S C §48301(a)) 1. Aircraft Nationality and Repistrason Mark USA N423TT Serial No. 1085 Make GULFSTREAM Model GIV Series 2. Owner Name (As snown on recestratron certificate) TRT LEASING INC Address (As shown on registration cerbficate) meow Kin N Fl Anl FR nR TIT PAM On WFST PALM BEACH set. FL zo 33401-4320 Cann; USA 3. For FAA tied Iv 4. Type 5. Unit Identification Reps( Alteration Unit Make Model Serial No. El IZI AIRFRAME (As deSonbed in an 1 above) O O POWERPLANT El O PROPELLER O O APPLIANCE Type manwarmer 6 Conformity Statement A. Agency's Name and Address S. Knd of Agency rem MO FSTRFAM U 5 Congealed Mechanc I Naumann:. mew. 1500-C PERIMETER RD. Faeign Calif.:OS Mecmnic C. Certificate No. ow WEST PAI M RFACH sow. Fl / CeMeateii Repair Medal v. 33406 ewe., USA Courcared maintenance Oranizethe CRS PB8R624N D. I Certify that the repair and/or alteration made lo the unit( ) denbried in item 5 Move and described on the reverse or anachments hereto have been made in accordance with the requirements 01 Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and cared to the best of my knowledge. Extended range fuel per 14 CFR Penal) App. 6 II Signature/0 trd Ind ual .. p28 Terry Barker 08/08/2012 7. Approval for Return to Service Pursue 1 to me aulhontY 9 en ;sons Specified below, the unit identified in Rem 5 was Administrate( of the Federal Aviation Administration and a 2 Approved inducted n the manner presaibed by the II Rejected BY FM Ft. Standards Inspector Manufacturer maintenance Organization Peewee ApPaasee by Can110451 Department 04 Tramped FM Designee I Repair Station Inspection Aulhonzabon Other (SpeCif y) Dedicate or Designation No. CRS PB8R624N Signature/Date Authorized I den t James Fishburn 08/08/2012 FAA Form 337 once) SDNY_GM_02753810 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240732 EFTA01326325 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be Compatible with all previous alterations to assure continued confonniry with the applicable airworthiness requirements. IL Description of Work Accomplished (II mote space p teetered. Mace acklemnal sneers. Identify waft aircraft nattonably and reed:ration mark and date work completer') USA N423TT tlitoommy and Repistratco Mark Aircraft Model: Gulfstream GIV Aircraft Serial Number: 1085 Reference Guffstream PBI Work Order: SC11231 08/08/2012 Date Complied with STC 51005441A - Installation of Concorde Battery sealed lead-acid Battery Model No. RG-380E144 IAW STC ST00544LA and steps II A 2 & 3 of Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E144 Lead acid batteries. Rev A dated August 28 2000. Permanently removed the following equipment: 2 ea. Saft Nickel-Cadmium Main Battery, Model 4076-11 Installed the following new equipment: 2 ea. Concorde sealed lead-acid Battery, Model RG-380E-44 No Weight and Balance change required by this action (weight change negligible). No Airplane Flight Manual Supplement required by this action. Airplane records updated to reflect this action. Aircraft electrical load not affected by this action. Instructions for Continued Airworthiness can be found in Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E/44 Lead Acid Batteries, Rev. A dated 08/28/2000, and Concorde document No. 5-0171 Rev. M. dated 03/15/2012. Note: This amendment, dated 08/0812012, supersedes the original 337 dated 06/06/2012, and adds the Instructions for Continued Airworthiness. END O AQdeIMA4)neets Are Attached FAA Form 337 now Nei SDNY_GM_027538t 1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240733 EFTA01326326 0 MAJOR REPAIR AND ALTERATION us DIDIMMOI at Tromoortrion (Airframe, Powerplant, Propeller, Or Appliance) Foam, aviation Aasenlernace ran APWIhea mwomen 3129CO20 EMCItrOC TWOS ( I Ninte, 6 • yen Vas Orer INSTRUCTIONS: Prom or type all entries. See Tile 14 CFR 643.9. Part 43 Appendix B. and AC 439.1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 944704 Failure to report can result in a civil penalty br each such vtolabon. (49 U.S.C. §46301(a)) 1. Alreraft Nationality and Registration Mark USA N423TT Serial mo. 1085 Make GULFSTREAM Model GIV Series 3. Owner mamk (As ShoWlIOn registration certificate) TRT LEASING INC Address (As shown on registration certificate) Amon MR N Fl Ant FR nR STF Pa00 Car WEST PALM BEACH Seri. Fl To 33401-4320 cosh, USA 3. Fa FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. O p AIRFRAME (As describer:tin neon I above) 0 O POWERPLANT O O PROPELLER O O APPLIANCE hype MarntaClurat 6. Conformity Statement A. Agency's Name and Address B. Kind of Agen y own Fall FSTRFAM U S. Certificated Mechanic I Manufacturer mem 1500-C PERIMETER RD. Forage Cenncares Mechanic C. Certificate No. ow MST PALM BFACH on. FL j Cenecaoss RaPai, Station Le 33406 cam, USA Centered Membrane* Organization CRS PEI8R624N D. I certify that the repair and/or alteration made to the unit( ) identified in item 5 above and described on the rove 'se Or a ttathrnants hereto la been made in accordance with the requirements of Part 43 of the U S Federal Aviation RegullitiOns and "•'.il the I-1 ormaliOn furnished hereon is true and correct t0 the best of my itnewledge. Extended range fuel per is CFR Part 43 APP. B MI Si nature/Dat0 o fined OF g Terry Barker 06/06/2012 . Approval for Return to Service Pursuant to the authonty given rsons Specified below. the unit .dented In item 5 was Inspected in the manner prescribed by the Administrator of the Federal MOW Administration and is O Approved O Retooled BY FAA FR. Standards InSpettOr Manufacturer Maintenance Organization Persona AFprovad by Camden Departmental Ocisartment Transport FAA.Designee ,/ Repse Station Inspection Authorization Other (SPearn carificii. or Designation No CRS P88R624N S James Fishburn 06/06/2012 ignature, ate of Au Individual 03 , FAA Form 331 (loo) SDNY_GM_02753812 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240734 EFTA01326327 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be Compatible with all previous alterations to assure continued Conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (it more space is required, attach additional sheets Identity well entree nationality end registration mark and dare wore carom Wed USA N423TT NaloMMY and Degreiration Mark Aircraft Model: Gulfstream GIV Aircraft Serial Number: 1085 Reference Gulfstream PSI Work Order: SC11231 06/06/2012 Oate Complied with STC ST00544LA • Installation of Concorde Battery sealed lead•acid Battery Model No. RG-380E144 IAW STC ST00544LA and steps II A 2 & 3 of Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E/44 Lead acid batteries. Rev A dated August 28 2000. Permanently removed the following equipment: 2 ea. Saft Nickel-Cadmium Main Battery. Model 4076.11 Installed the following new equipment: 2 ea. Concorde sealed lead-acid Battery, Model RG-380E-44 No Weight and Balance change required by this action (weight change negligible). No Airplane Flight Manual Supplement required by this action. Airplane records updated to reflect this action. Aircraft electrical load not affected by this action. END heels Are Attached J FAA Form 337 yeah SDNY_GM_02753813 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240735 EFTA01326328 MAJOR REPAIR AND ALTERATION Fon" atOmnta OM Na 21204020 11 2007 /30. Iltetac mixing Mower am FAA1)•• Only LIS Doporbwr oi Inonrpriso” (Airframe, Powerplant, Propeller, or Appliance) roes Artesia Adiekrusein INSTRUCTIONS: Print or type at entries. See Tide 14 CFR §43.9. Pan 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of the teem. This report is required by law (49 U.S.C. §44701). Failure o report can result in a civil penaity for each such violation. (49 U.S.C. §48301(a)) 1. Aircraft Nationality and Registration Mark N423TT Serial No. 1085 Make Gulfstream Model G -IV Series 2. Owner Name (As shown on registratton certificate) TRT LEASING INC Address (As shown on registration certificate) Alone 05 N Fiedler Drive Suite P400 tier West Palm Beach thus Ft As 33401.4320 _ . tear USA 3. Far FAA Use Only 4. Type 5. Unit Identification Reese Mershon Unit Make Model Serial No. 0 0 AIRFRAME (As descrtbed An Item I above) 0 o powERRANT • 0 PROPELLER 0 O APPLIANCE Type Manulacturs 0 Confonnity StatiesseM __ A. Agency's Name and Address B. Kind of Agency rem tleneral Dynamic, Aviation Services u. S. Condkated Mechanic I htersitscsser *emu 1500-C Perimeter Road FOreign Unmated Latahant C. Certificate No. oft trftitSt Palm Beach lam FL j Caellkalad Repair Station z, 33406 Caw" USA CO41114104 Izamenanee 0rgenvation PB8R624N D. I certify that the repair and/or alteration made to the unit a) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the intOnneion furnished herein is true and correct to the best of my knowledge. Extended range fiat PM 14 CFR Pali 43 O App. 8 Signature/Date of Authorized Individual Ali, elti.__.--- Stephen G. Paulsen 21 September 2007 7. Approval for Return to Service Pursuant to the authority given persons specified below. the unil identified in Item 5 was Inspected in the manner prescribed by the Administrator of the Federal Aviation AdrrinialnillOn and is O Approved O Rejected BY FAA Fn. SlandardS Inspector Manufacturer Maintenance Organization Panora ADP.Oved Ist Canadian I Depwtmem of Tranwort FM Designee x Repair Staten Inspection Authorization Other (Specify) Certificate or Designation No. CRS PB8R624N SignaturerDere of Authorized Ince/duel ...XS St dit-----.. Stephen G. Paulsen 21 September 2007 FAA Form 337 nee FAA SDNYGfil02753814 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240736 EFTA01326329 NOTICE Weight and balance or operating limilabbn changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (II more space is required. WWII additional sheets. Identify with aircraft nationality and registration mart and date *orb completed.) Aircraft Model: G-IV Aircraft Serial No.: 1085 USA I N423TT Nationality and Registration Mark Aircraft Total Time: 6728.0 Aircraft Total Landings: 3057 Work Order No.: 17964 21 September 2007 Date Accomplished upgrade of existing Allied Signal Enhanced Ground Proximity Warning System from a software version 104-104 to 218-218 UAW Gulfstream STC ST01851AT-D and Gulfstream Custom Engineering Drawing List CE41 4960458 and EGPWS Windshear (218-218) (MOD) Electrical Drawing CE41 3490238 approved under FAA Form 8110-3 dated 9/17/07. Updated Flight Manual Supplement with Gulfstream G-IV Flight Manual Supplement No. CE41 349M001 and provided EGPWS Instructions for Continued Airworthiness Report No. CE41 349A001. Change to Electrical Load negligible. No change in Weight or Balance. END 0 Additional Sheets Are Attached FAA Form 337 ilea Fax SDNY_GM_02753815 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (x)244)737 EFTA01326330 0 MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) Form Approved 0148 No. 2120-0020 For FAA Use Only aronpoowion Nowa ease Adirenianwee Office Identification INSTRUCTOONS NM or type as entries. See FM43.9. FM 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. The report 4 required by law (49 U.S.C. 1421). Failure to report can ream in awl penalty not to exceed $1.000 for each Such vioUlion (Section 901 Federal Aviation Act of 1958) 1. Aircraft Make GULFSTREAM MCdelG-IV Serial No. 1085 Nationality and Registrabon Mark N877RP. 2. Owner None (As show, on registration certificate) TRT LEASING INC Address (As shown on egssftation certificate) 515 N FLAGLER OR STE P400 WEST PALM BEACH FL 33901-4320 3. For FAA Use Only The alter atterabon(s) authorized David Kelm Mien identified henn are compatible in FAR 43.7. nas been reviewed and found to be complete and eligible for use on the above described aircraft, U.14/...,_ MA Pr nil DOI 5t-) with appropriate DER approvals. All aspects of the subject to conformity Inspection by a person 1 ‘I — n s o il ---a—...---1Y 4. Unit Identification 5. Type tint Make Model r Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PRCPELIER APPLIANCE Type Manufacturer 6. Con enmity Statement A. Agency's Nana and Address B. Kind of Agency C. Certificate No. CAPITAL AVIATION. INC. 5500 PHILLIP J. RHOADES HGR. 2. WILEY POST AIRPORT BETHANY OK 73008 U.S Cortiliesee liKheniC Fannon Certificate Nernst MZIR092Y X Caninesisa ReNir Minion Illanidechat D. i Caney mat ea row macs ataneen nude to the unite) denoted neer 4 above and 00•01trier on Inc reverse et erinolvnenrs memo have been mese n 41O:Ordend web Vie requinernenrs or Part 43 or tie V S Federal Mabee Regulate,,, and MN the Somalia, Ournonee hem e tee and COMPC113 the belt or fry sroirieope. Date e/ D1-2€297 Signature of Authorized MICHAEL S. ROPER 1 7. Approval for Return To Service P rsuant to the authority given pe sons specified below, the tint identified in item 4 was i ded en manner preSalbed by Me Administrator of the Federal Aviation Administration and is IM APPROVED O BY FM Flt. Standards Inspector Manufacturer Inspection Authorization Other (30.O69 FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Reaction e le/iai s249, 7 Certificate or Designation No. X91R092Y Signature of Authorized I ual MICHAEL S. ROPER FAA Form 337(1201 EleattriC Yawn (MOW) SDNY_GM_02753816 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240738 EFTA01326331 Work cpndetad tot IN677RE) al NOTICE Weight and balance or Operabng Mrstabon changes Shall be colored in MO SparOpiate mraall MOM M Steredlan musi be Calipabble web apeman alteratiOrb 1001WO COntInUedCOnlarnily WI Me appeals anworthtless reqdrernent5 8. oeso.e..cel el Work Accomplished GULFSTREAM G-IV N677RP S/N 1085 W/O 1658 ELECTRICAL MODS The following is a list of drawings used for dte Mixliftcations and Alterations to the Phone, Entertainment and Electrical Systems: I. Report - ELA 06-10318, Electrical Load Addendum Gulfstrearn G-IV-S/N 1085, Rev.1/R, dated 03.26-2007. (4 Sheets) 2. 06-10319, Lay-Gut-G-IV, sin 1085 Cabin Modifications (4 Sheets) 3. 06-10320. W/D-G-IV S/N 1085 Drawing Notes. Rev. I/R dated 03.26-2007. (I Sheet) 4. 06-10321, W/D-G-IV S/N 1085 Vendor Information, Rev. UR dated 03.26-2007. (I Sheets) 5. 06-10322, W/D-G-IV S/N 1085 Cabin Equipment/Wiring Renitnials, Rev.1/R dated 03-26-2007. (14 Sheets) 6. 06-10323, W/D-G-IV S/N 1085 Ciricut Breaker Panel Mods, Re;/.1/12 dated 03-26-2007. (5 Sheets). ' 7. 06-10324, W/D-G-IV SIN I085 .Terminal Block Layout, Rev.1/R dated 03-26-2007. (3 Sheets). 8. 06-10325, W/D-G-IV Sthl 1085 Galley Systems, Rev.1/R dated 03.26-2007. (9 Sheets). 9. 06-10326, W/D-G-IV S/N 1085 Aft Lavatory Systems, Rev. I/R dated 03-26-2007. (3 Sheets). 10. 06-10327, W/D-G-IV SIN 1085 Upwash/Downwash Lighting, Rev. UR dated 03-26-2007. (3 Sheets). 11. 06-10328, W/D-G-IV S/N 1085 Cabin Reading and Table Lihgts, Rev. I/R dated 03-26-2007. (3 Sheets). 12. 06-10329. W/D-G-IV 1085 Cabin Aisle Lighting, Rev.1/R dated 03.26-2007. (3 Sheets). 13. 06-10330, W/D-G-IV SIN 1085 Ordinance Signs, Rev. UR dated 03-26-2007. (3 Sheets). 14.06-10331, W/D-G-IV S/N 1085 Entry Lights, Rev.1/R ditted 03-'26-2007. (2 Sheets). IS. 06-10332, W/D-G-IV SIN 1085 Jump Seat Lihgts,Rev.11R dated 03-26-2007. (2 Sheets). 16.06-10333, W/D-G-IV S/N 1085 Cabin Window Shades, Rev. UR dated 03-26-2007. (4 Sheets). 17.06-10334, W/D-G-IV S/N 1085 Cabin/Lav Call Systems, Rev.1/R dated 03-26-2007. (2 Sheets). 18.06-10335, W/D-G-IV S/N 1085 Crew Lavatory System, Rev.1/R dated 03-26-2007. (2 Sheets). 19.06-10336, W/D-G-IV S/N 1085 Cabin Audio Mods., Rev.1/R dated 03-26-2007. (2 Sheets). 20.06-10337, W/D-C-IV S/N 1085 Entertainment Systems. Rev.1/R dated 03-26-2007. (8 Sheets). 21.06-10338, W/D-G-IV S/N 1085 Assess Phone System, Rev. I/R dated 03-26-2007. (2 Sheets). 22.06-10339, NOT USED. 23. 06-10340, W/D-G-IV S/N 1085 Cabin I I VAC Outlet Mods., Rev.1/R dated 03-26-2007. (4 Sheets). 24.06-10341, W/D-O-IIV SIN 1085 CMK-1100 Electronic Flight Big Sys., Rev. I/R dated 03-26-2007. (3 Sheets). . . 25.06-10342, W/D-G-IV S/N 1085 Cabin Temp Control Mods, Rev. UR dated 03-26-2007. (2 Sheets). 26.06-10343, W/D-G-IV S/N 1085 XM Weather Receiver, Rev.1/R dated 03-26-2007. (2 Sheets): Data approved by Systems & Equipment DERT-710196-SW on FAA Form 8110-3 NJEN-07- 027dated April 04,2007. A EMI Test performed in accordance with Capital Aviation. Inc. EMI. Ground Test Procedures, Document No. 04-EMI-10000, Rev. I/R dated 11-22-2004. Document No. 04-EMI-10000 approved by Systems & Equipment - Avionics & Electrical DERT-710796-SW on FAA Form 8110-3, SLIFN-06- 074, dated September 26,2006. • • X 1 Matti:nal Shears Aso anacnoo SONY_GM_02753817 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240739 EFTA01326332 Walt Completed for (N677RPI on a Description or work Arrornossreci NOTE: I. All NON-ESSENTIAL systems and equipment installed on existing Non-Essential Busses. Load Sheding covered in Aircraft Flight Manual. 2. See Capital Aviation, Inc. FAA Form 337 entitled "Interior Cabin Mods" for mounting of Electrical Equipment. Log Book Entry made. Weighed Aircraft, computed new C.G. and entered in aircraft records. CONTINUED AIRWORTHINESS - Monitor item(s) for condition. If item(s) become damaged, replace with same make and model. If make / model is not available, notify the local FSDO of part replacement. Refer item(s) to installer or any qualified service center for repair or replacement. Items to be inspected in conjunction with operators approved inspection program to insure secutity, overall condition and proper operation as is required. CULFSTREAM G-11/ N677RP SIN 1085 W/O 1658 )(Additional Sneers Are Attached SDNY_GM_02753818 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240740 EFTA01326333 SDNY_GM_02753819 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240741 EFTA01326334 U.S. DEPARTMENT OF TRANSPORTATION. FEDERAL AVIATOR ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE April 4, 2007 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE GULFSTREAM MODEL NO. G-IV TYPE (Aiplans. Reda bisticoeter. Ott) Airplane NUM OF APPLICANT Capital Aviation Inc LIST OF DATA IDFNTIFICATION TITLE DRAWINGS See sheet 2 of 2 SEE SHEET 2 OF 2 NOTES: ' 1.The Electrical Design Data Aspects Only of these data are approved herein. Approval is In support of a 337 Interior installation modification in a Gulfstream , Model G-IV, SIN 1085 only. 2. EMI test required prior to returning aircraft to service. PURPOSE OF DATA Approve the Electrical Design Data Aspects Only in support of a 337 installation (Major Alteration ) APPUCABLE REOUIREAIENTS (LW sPiscMe sections) FAR 25.1301(aXbXcXd), FAR 25.1309(a)(b), FAR 25. 1351(a), FAR 25.1357(a)(c)(d), FAR 25.1359(a)(b) ma • C:i".3LTIt CERTIFICATION - Under authority vested by drecbon of the Administrator and In accordance with conditions under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered accordance with established procedures and found to comply with applicable requirements of the Federal 0 Recommend approval of those data Wore la Approve those data and Flattens of appointment 2 of 2 have been examined in , Aviation Regulatlens SIGNATU (S) OF 06.7) FIAT EERING REPRESENTATIVES) DESIGNATION NUMBERS(S) CLASSIFCATION(S) Joluaik et,_ a • DERT-710196-SW Systems & Equipment Avionics & Electrical 8110-3 JFN-07-027 FAA Form 8110.3 (11.70) SUPERSEDES PREVIOUS ELATION ELECTRONIC FORMAT (740) SDNYGM 02753820 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240742 EFTA01326335 SDNY_GM_02753821 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240743 EFTA01326336 FEDERAL AVIATION ADMINISTRATION FORM 8110-3 FOR GULFSTREAM, MODEL GIV, S/N 1085 NUMBER: JFN-07-027A DATED 4-4-2007 SHEET 2 OF 2 DRAWING NOMENCLATURE REVJDATE EFFECTIVITY REPORT￾ELA-10318 ELECTRICAL LOAD ADDENDUM GULFSTREAM GIV-S/N1085 IR- Dtd. 03-2407 S/N 1085 ONLY 06-10319 LAY-OUT-GIV S/N 1085 CABIN MODIFICATIONS I/R- Dtd. 03.26.07 " " 06-10320 W/D-G-IV S/N 1085 MASTER DRAWING NOTES 1/R- Ott 03-26-07 " a - 06-10321 W/D-G-IV S/N 1085 VENDER INFORMATION UR- Dtd. 03-26-07 " " 06-10322 W/D-G-IV S/N 1085 CABIN • EQUIPMENT/WIRING REMOVALS UR-Dtd. 03-26-07 " " 06-10323 W/D-G-IV S/N 108.5 CIRCUIT BREAKER PANEL MODS UR- Dud. 03.26.07 a " 06-10324 W/D-G-IV WI 1015 TERMINAL BLOCK LAYOUT 1/R- Ott 03-26-07 a " 06-10325 W/D-G-IV S/N 1085 GALLEY SYSTEMS I/R- Dtd. 03-26-07. " " 06-10326 W/D-G-IV S/N 1085 AFT LAVATORY SYSTEMS I/R- Did. 03-26-07 " 06-10327 W/D-G-IV S/N 1085 UPWA$11/DOW14WASH LIGHTING UR- Did. 03-26-07 - _ " 06-10328 W/D-G-IV S/N 1085 CABIN READING AND TABLE LIGHTS I/R- Dtd. 03-26-07 " a 06-10329 W/D-G-IV S/N 1085 CABIN AISLE LIGHTING I/R- Dtd. 03-26-07 " 06-10330 W/D-G-IV SIN 1085 ORDINANCE SIGNS I/R- Dtd. 03-26-07 " " 06-10332 06-10331 W/D-G-IV W/D-G-IV S/N 1085 ENTRY LIGHTS UR-Dtd. 03-26-07 " " S/N 1085 JUMPSEAT LIGHTS I/R-Dtd. 03-26-07 " 06-10333 W/D-G-IV S/N 1085 CABIN WINDOW SHADES 1/R Dtd. 03-26-07 " " 06-10334 W/D-C-IV S/N 1085 CABIN/LAV CALL SYSTEM 1/R Did. 03-26-07 " 06-10335 W/D-G-IV S/N 1085 CREW LAVATORY SYSTEMS I/R Dtd. 03-26-07 " " 06-10337 06-10336 W/D-G-IV W/D-G-1V S/N 1085 CABIN AUDIO MODS I/R Dtd. 03-26-07 " " S/N 1085 CABIN ENTERTAINMENT SYSTEMS 1/R Dtd. 03-26-07 " " 06-10338 W/D-G-IV S/N 1085 AIRCELL AXXESS PHONE SYSTEM UR Dtd. 03-26-07 " " 06-10340 W/D-C-1V S/N 1085 CABIN I1OVAC OUTLET MODS 1/R Dtd. 03-26-07 " 06-10341 W/D-G-IV S/N 10135 CMA-1100 ELECTRONIC FLIGHT BAG SYSTEM UR Dtd. 03-26-07 a 06-10342 W/D-G-IV S/N 1085 CABIN TEMP CONTROL MODS 1/R Ott 03-26-07 a 06-10343 GIV S/N 1085 XM WEATHER SYSTEM I/R-Dtd. 03-26-07 " " SDNY_GM_02 753822 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240744 EFTA01326337 SDNY_GM_027.823 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240745 EFTA01326338 U.S. DEPART/ea OF TRANSPORTATION FEDERAL AVIATION N4SCTRAT1ON STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE SEPTEMBER 26 2006 AIRCRAFT OR AIRCRAFT COMPONENT IDEMTTFC.ATON MAKE GulfstrearnAerospace Corporation t&COEL NO. G-iv TYPE (Urprane. Radio. MIlkoplel. etc) Airplane NAME OF APPLICANT Capital Aviation Inc LIST OF DATA IDENTIFICATION Ina DOCUMENT 04-EMI-10000 REVISION 1/R DATED 11-22-2004 EMI GROUND TEST PROCEDURE NOTES: 1.The Electrical Design Data Aspects Only of these data are approved herein. Approval is for the Gulfstream Aerospace Corp. Aircraft listed in TCDS Al2EA. Rev 29. PURPOSE CF DATA Approve the Electrical Design Data Aspects Only in support of a EMI Ground Test Procedure. APPLICABLE REQUIREMENTS (UN Nadia roan) FAR 25.1301(a)(bXc) - FAA 02:C;IVI. CERTIFICATION - undue =Ahern under Part 183 of the Federal accordance PUT estabfishod procedures vested by derecton 04 In Aeroflot:2kt Aeration Reptaattorts data listed above and found to comp/yeah appicalab approval or these data those data and In aoardanc0 volt and on attached fl ats reambeasel nequIromenta of Om Federal cannons and Inialions of aPPIATININI have bean rnalnaleal In Aseadon RoISITIona. is Recotrunond -- I Tln 0 Approve SIGNATU OF DESIGN*, REPRESENTATIVE(S) DE IS/ATM NIAABERSTSI cussincsnotem John F DERT-710198-SW Systems 8 Equipment Avionics 8 EJectical 8110-3 JFN-06-074 Si (1140) SUPERSEDES PREVIOUS ECtnow ILICTROICITORISTT(7441 SDNY_GM_02753824 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240746 EFTA01326339 SDNY_GM_02753825 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240747 EFTA01326340 0 MAJOR REPAIR AND ALTERATION us Oemarvera Twice:In (Airframe, Powerplant, Propeller, or Appliance) Wet 'Waren Mbredetrelee Form Approved CM No 21204320 For FAA Use Only Office Idenbfication talRUCTIONS. Rh Or type al entries See FAR 43.9. FAR 43 Appendix B. and AC 43 9.1 (or subsequent revelon thereof) for instrucoons and deposition of this form. The report is required by law (49 U.S C. 1421). Facture to report can result a girl penalty not to exceed 51.000 for *Eh such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make . i • MOON GV Sere) No. 1085 NabOnalty. and Revocation Mark N677RP ' t. Owner Name (As shown on registration caratiCete) TRT LEASING INC Address (As shawl on regisfralion car-tektite) 515 N FLAGLER DR STE P400 NEST PALM BEACH FL 33401-4320 3. For FAA Use 0* The alteration alterations) authorized David Kelm identified herin has been reviewed and found to be complete are compatible and eligible for use on the above described aircraft, in FAR 43.7. . . . r4C=E , \le..1—.. ti nt. —WOOL go—, with apPropriate DER approvals All aspects of the subiect to conformity inspection by a person • Li^ '7.s'7 i . •4. Unit Identification s. Type Ui'S SAM. Moist Sena! No. Repair flotation AIRFRAME (As dasenterf in Ilsm 1 above) X POWERFLANT PROPELLEFt APPLWCE Type Manufacturer • • : a. Conformity Statement 1 A Agency's Nays and AddretS B. Kind of Agency C Certrficale No. CAPITAL AVIATION, INC. ! 5500 PHILLIP J. RHOADES FIGR 2, WILEY POST AIRPORT BETHANY OK 73008 us. Commend methane • sconigin Genital*. ma. so X9114092), X can/kited Repair Staten Marulacturer D. 'Wei trial the Wet anew amnion nude to the men *Wee n diem 4 reeve ace deicnbed en the reverse or attachment; hereto have bee made in at coleance well the reouiemerts of Pane of ma us Fears Avia6On Rociations end that We Syron aanutio0 ham, and canal to Ma OW Of nag linOwaidd0 Dale d -009- 2a97 Signature of Authorized MICHAEL S. ROPER ' 7. Approval for Return To Service P rsuant to the authority given persons spoofed below. the raid Identified in lair 4 was i Administrator of the Federal Aviation Administration and et El APFROW-0 O n the manner preSCribed by the BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transpart Canada Airworthiness Group, Date of Approval or %alba • - DV-DI-2.407 Certificate or . DengristIon No. X91R0112Y --Spam of Authorizes - ftW MIGHAELS. ROPER . FAA Fenn 337 ilzse earinnevensie (Mee SDNYGA402753826 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240748 EFTA01326341 Week completed for IN677RPI on • !MICE Weight and balance or operating imitabon changes shag be elected Ingle aPliaoPtige morn Mad. An annum must be compatible wan an previous a/wagons to assure comMued conlormity went* appicalste d..wrdwress requirements 8. Descnpuon ot Work Accomplished GULFSTREAM G-IV N6'77FtP S/N 1085 W/O 1658 ANTENNA I. Removed existing Antenna and installed COMANT Antenna CI 420-I , s/n 162608 using existing doubler at F.S.I93C.00+9 as per Strong Aero Engineering drawing N677RP-011107- I, Rev. N/C dated 01 -1 I-2007. 2. Installed Sensor Systems, Inc. Iridium/GPS Antenna 567-1575-165, s/n 1333 F.S.193C.00+9 as per Strong Aero Engineering drawing N677RP-011107-2, Rev. N/C dated 01-11-2007. Data approved by Structures (A I, A4, PI, P4) DERT60581 8NM on FAA Form 8110-3 dated 02.19-2007. Weighed aircraft, computed new C.G. and entered in aircraft records. Log Book Entry made. CONTINUED AIRWORTHINESS - Monitor item(s) for condition. If item(s) become damaged, replace with same make and model. If make / model is not available, notify the local FSDO of pan replacement. Refer item(s) to installer or any qualified service center for repair or replacement. Items to be inspected in conjunction with operators approved inspection program to insure secutity, overall condition and proper operation as is required. CND W Additional sheets /me Attached SDNY_GM_02753827 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240749 EFTA01326342 V.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION AtmivIsTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 02/19/07 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE GULFSTREAM MODEL NO. G - IV TYPE cairpiene,4.410. AIRPL Hellorpter.etc.) ANE NAME OF APPLICANT CAPTIAL AVIONICS, INC. LIST or DATA IDENTIFICATION TITLE DRAWING REFS: "ANTENNA REPLACEMENT" "S67-1575-165 DOUBLER Notes: REMOVAL AND COMANT CI 420 - 1 ANTENNA IRIDIUM/DATA DUAL CHANNEL ANTENNA DESIGN & INSTALLATION" APPROVAL IS FOR ONE AIRCRAFT; S/N 1085, T/N N677RP N677RP -011107 - 1 REV N/C 01/11/07 N677RP -011107 -2 REV N/C 01/11/07 • . engineering design data only and is not an It indicates the data listed above only with the regulations specified by listed below as 'APPLICABLE with additional regulations not listed This approval'is for installation approval. demonstrates compliance paragraph and subparagraph REQUIREMENTS'. (Compliance here may be required). PURPOSE OF DATA IN SUPPORT OF A MAJOR ALTERATION TO SHOW COMPLIANCE WITH THE FOLLOWING REGULATIONS APPLICABLE REQUIREMENTS (List specific sections) CFR 14 FAR Part 25.301(a), Amdt 25-23; .303, Amdt 25- 23; .305(a), Amdt 25 - 86; .307(a), Amdt 25- 72; .365(a) (b)(c), Amdt 25-87; .601, Amdt 25-0; .603(a), Amdt 25-46; .605(a), Amdt 25-46; .607(a), Amdt 25-23; .609(a), Amdt 25-0; .611, Amdt 25- 23; .613(a) -(d), Amdt 25-72; .625(a), Amdt 25-72 CERTIFICATION - Under authority vested by direction of the limitations of appointment under Part 181 of the Federal sheets numbered N/A have been examined Administrator and in accordance with conditions and Aviation Regulations, data listed above and on attached in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. El Recommend approval of these data I oditi Therefore Pg Approve these data SIGNATVREISIOF DESIGNATED ENGINEERING RE RESENTATIVE(S) DESIGNATION NOKBERSIS) CLASSIFICATION(SI TREVOR J. STRONQ--- --\ DERT605818NM STRUCTURES(A1,A4,P1,P4) VVVicjkTAA I ( /U\ _ ... ...... Clt - - EDITION GPO 901-41 SDNY_GM_02753828 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (X)240750 EFTA01326343 SDNY_GM_02753829 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240751 EFTA01326344 0 MAJOR REPAIR AND ALTERATION US Overt* Crimea , (Airframe, Powerplant, Propeller, or Appliance) rens Ann Adriteiblike Fern Approved 0M3 No. 2120-0020 For FAA Use Only Office Identification INSTRUCTIONS: Print or type as entries. See FAR 43.9, FAR 43 Appends B. arid AC 43.9,1 (or subsequent revision thereof) for instructions and deposition of this lone. Ties report is required by law (49 US.C. 1421). Failure to report can resul ti civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM Model G-IM Sew No. 1085 Nellonality and Registration Mark MSTIRP 2. Owner /tare (As shown on registrabon carioca) TRT LEASING INC , Address //As shown al registration certificate) S15 N FLAMER DR STE P400 WEST PALM BEACHFL 33401-4320 . 3. For FAA Use Only The alteration alteration(S) authorized David Kelroc. are in identified henn has compatible and FAR 43.7. been reviewed and found to be complete eligible for use on tie above described aircraft. °Art "II tool <ma with appropriate DER approvals. All aspects of the autism to conformity inspection by a person L ...... _.-41./-...- LI - I. 0C) 4. Unit Identification S. Type UM Male • Model Sorel No Repar Artef Mien AIRFRWE (As descntial in Muir 1 above) -: X POAERRANT FRCPEMBI APPUNCE Type i Manufaciunsi ALConferseft7 Statement A. Agency's Name and Address ' B. land of Agency C. Certificate No. CAPITAL AVIATION, INC. 5500 PHIUJR J. RHOADES MGR. 2, ViALEY POST AIRPORT BETHANY. OK 73008 U.S. Conine:awe nine Forpn CeillfiCalled Marthiak X91R0921. X Ce(VIICat•O Repair Staten lannewer Ct I reaW Nai no ran ana anon nen be wtissi dented n ilet 4 roam ens decreed on te reverse a allaclinerds lent llosedance wale rte neurone 08 Pen 43 of to U.S. Fein ANSI*" Repeat» end swab mlorrreeco tinned en Sid and Nee been made in b as bit or rrir Wainge. Date 63 / a 2a 7 7 Signature of Authorized I g MICHAEL S ROPER 7. Approval for Return To Service Pursuant to the authority given persons specified below, the and identified in ism 4 was i it manner by the Administrator of the Federal Aviation Admeetration acid's El APPROVED O BY FAA Rt. S1Hi0art1a Inspector Manufacturer Inspection Authorization, Oiler (SPecify) • FAA Designee X Repair Station Person Approved by Transom Canada Airworthiness Group Dale of Approval or Reterzlon A l le4, - Cerlecate or 1 Designation No. X91R092Y -Span of Authorized MICHAEL S. ROPER . FAA Form 337nuo Elseetnevessewesee SDNYGlvi 02753830 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240752 EFTA01326345 .• Walt completed Ice IN677NPI on NOTICE Weill and balance or operating lordaton changes shell be ertered In the appoprerce aircraft record. An Aeration must be ccenpeatile *eh al premotrs Maria.* to assire continued eat/amity vah an *pebble anat*iessimitarements. & Desolation cr Work AocomPashed GIJLFSTREAM G-IV N677RP S/N 1085 W/O 1658 INTERIOR / CABIN MODS, I. Original Interior Configuration and New Interior Configuration are as shown on Capital Aviation, Inc. drawing 07-10018, Rev. URI dated,03-05-2007. (1 Sheet) 2. Modified existing L/H Fwd.Closet as per Capital Aviation, Inc. drawing 07-10019 Rev. 1/R dated 03-05.2007. (2 Sheets) 3. Installed R../14 Fwd. Crew Lay as per Capital Aviation, Inc. drawing 07-10020 Rev. I/R dated 03- 05-2007. (7 Sheets) 4. Installed Windowline as per Capital Aviation, Inc. drawing 07-10021 Rev: I/R dated 03-05-2007. (2 sheets) 5. Installed Credenza as per Capital Aviation, Inc. drawing 07-10023 Rev: I/R dated 03-05-2007. (10 Sheets). 6. Installed SubWoofer Cable( to existing Ft/H AFT Bulkhead as per Capital Aviation, Inc.drawing 07-10024 Rev: I/R dated 03-05-2007. (I Sheet) 7. Modified L/H and R/H Galley as per Capital Aviation Inc. drawing 07-10025 Rev: I/R dated 03-05- 2007. (5 Sheets) • 8. Modified existig Vanity as per Capital Aviation Inc, drawing 07.10026 Rev: I/R dated 03.05-2007. (3 Sheets). 9. Installed 17" Monitor at F.S. 297.0 as per Capital Aviation Inc, drawing 07-10027 Rev: I/R dated 03-05.2007. ( 4 Sheets ). 10. Installed Aircell FUH at FS. 232.5 as per Capitall Aviation Inc, drawing 07-10028 Rev. I/R dated 03-05-2007. ( 4 Sheets ). II. Installed Misc. Equipment as per Capital Aviation Inc, drawing 07-10029 Rev: I/R dated 03-05- 2007. ( 4 Sheets ). Data approved by Structural DERT-710098-SW, on FAA Form 8110-3, NSE-07-004 dated 04-02- 2007. CONTINUED AIRWORTHINESS - Monitor item(s) for condition. If ken(s) becinneydamagel, • replace with same make and model. If make / model is not available, notify the local FSDO of part replacement. Refer item(s) to installer or any qualified service center for repair or replacement. Items to be inspected in conjunction with operators approved inspection program to insure secutity, overall condition and proper operation as is required. Weighed Aircraft computed new C.G. and entered in Aircraft records. Log Book Entry made. ()Ciao:Nome Sheets Aro Attached SDNY_GM_02753831 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240753 EFTA01326346 04/02/2007 ION 1:18 FAA %003/004 US. OELIMMENT OF TRANSPORTATION FEDERAL AVIATIONADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 4-2-07 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARE Gulfstream Aerospace Corporation MOM Na GIV TYPE (Mast Rad H•OcrS etc) Airplane MALE OF APPLICANT Capital Aviation Inc. LIST OF DATA IDENIVICATON 771E Dwg. No 07-10018 Rev. VR. dtd 3-6-07 Sheet 1 Dwg. No. 07-10019 Rev. UR, dtd 3-5-07 Sheets 1 & 2 Dwg. No. 07-10020 Rev. UR, dtd 3-5-07 Sheets 1 Vim 7 Dwg. Na 07-10021 Rev. UR, dtd 3-5-07 Sheets 18 2 Dwg. No. 07-10023 Rev. UR. dtd 3-6-07 Sheets 1 thrU 10 Dwg. No. 07-10024 Rev. l/R. Md 3-5-07 Sheet 1 INTERIOR INSTALLATION LH FWD CLOSET MOD RH FWD CREW LAV INSTALL WINDOWLINE INSTALL CREDENZA INSTALL SURWOOFER CABINET INSTALL NOTES: 1. This FAA approval is for structural aspects of the data only. Additional approvals may be required for other aspects of the data. 2. The inspection of the installation is not being approved 3. The approval Is in support of the noted modet. S/N 1085 only. SE-07-004 Sheet 1 of 2 PURPOSE OF DATA To provide FAA Approved data in support of a Form 337 approval APDIkum F REQUIREMENTS as ip allow) FAR 25.301, 25.303, 25.305, 25.307, 25.603, 25.605, 25.607, 25.813, 25.789(a) at Amendment 25-56 CEP:MACAU:IN . under sumo* vetted by deeded *lima Ammeurator and Ln =meant* wan ~worn WIC1 bIlibitiOrit of appointment urger Pmt 183 of to Fedora anew: Ra- et ans, data Wed above and on aliened crmot nvenearm )0C4 have been manned in =Wan= Ni estiahAled pi IXtd4), C'S 411C found to wmpty vall appleatie nattdementa of Ite Federal AvishOn ~In , 0 Recommend approval of them data 4iNekTromeiore 2 Approve thaw data 51 ATI NA 0j tet'SF ' Thee , D S NATO USEFLS(S) CLASSIFiCAT/ON(S) Richard W. Southard PERT-710241-SW Structures FAA Fonm MIMS (I JO) SUPERSEDES PREVIOUS EPROM ELECTRONIC FM:m*3 (790, SDNYGlvl02753832 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O240754 EFTA01326347 SDNY_GM_02753833 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240755 EFTA01326348 04/02/2007 MON 1;19 FAA ?004/004 OE DEPARTMENT OF IPANSPORTA11014 FEDERAL AVIATION ACGINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 4-2-07 AIRCRAFT QR AIRCRAFT COMPONENT IDENTFIC•TION NAPE Gulfstream Aerospace CorPOretite la0DEL NO. GIV TYPE plep/ony Airplane RM. Nymootte. NAME OF APPLICANT Capdal Aviation Inc. No UST Or DATA IDENTIRCANON 1TRE Dwg. No 07-10025 Rev. UR. dtd 3-6-07 Sheets 1 thy 5 Dwg. No. 07-10026 Rev. UR, dtd 3-5-07 Sheets 1 dint 3 Dwg. No. 07-10027 Rev. UR, dtd 34-07 Sheets 1 Wm 4 Dwg. No. 07-10028 Rev. UR, did 3447 Sheets 1 that 4 Dwg. No. 07-10029 Rev. UR, dtd 3-5-07 Sheets 1 thru 4 Lti AND RH GALLEY MOD VANITY MOD MONITOR INSTALL MRCS LL INSTALL MSC EQUIPMENT INSTALL NOTES: 1. This FAA approval is for structural aspects of the data only Additional approvals may be required for other aspects of the data. 2 The inspection of the installation is not being approved 3. The approval's in support of the noted model, SIN 1085 only. SE-W-004 Sheet 2 of 2 PURPOIE OF DATA To provide FAA Approved data in support d a Form 337 approval APPUCARE REEMMEMENTS DM weft media* FAR 25.301, 25.303, 25.305, 25.307, 25.603, 25.605, 25.607, 25.613, 25.789(a) at Amendment 25-56 CERTIFICATION - Vnde, mulhonly veered by ciontron of the Adrnitingefter and in •Coonlenon sal andRiCe% Under PM 163 of !In rt...ten, AvtabOn Regt10130r4, Outs rn.ted *Love and On lanChed nen numbered accordance w0 MtabezIllee procedures end found to cotnuty DAM meta* Itiqukeelenb of the Federal 0Recomenand approval of ThOs. data I ?hat) Throb, MAMMA. Mara dab awl Imitaffn of appointment vex hive boon Wit s:4 in MAST Repulterte. IA TWatEMIORlar artFASENTNINE161 OESIGNATMet NIPMERNS) I CIASWICATIONM1 Richard W. Southard .. DERT-710241-SW Structures ... FM Foam 111104 (ii -TO) SUPERSEDES PREMOUS EOMON ELECTROMC FORMAT (7-00) SDNY_GM_02 753834 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240756 EFTA01326349 SDNY GM 02753835 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240757 EFTA01326350 MAJOR REPAIR AND ALTERATION ,.......... Nyed •Aae. (Airframe, Powerplant, Propeller, or Appliance) ........ Oram NO POPrOse M) 21204030 U let FAA se ORM CfAce kftradien ,NSTRUCTIONS Prot et hoeel Pena. See FAR 43 E. MR 43 APP•Ma B. end AC 43 91 crehteepant mimeo teed) S3r Mare Ma eispommm cf um In yhe mon A repuppy oy /•• l49 U SC 1421) Felon anon cm rowan 4 ow yemMY AM to Ammo, SICCO re, Yeti AAA Valallon (Seam or Irvin Paint Am mom 1. Aircraft Make Gultstream atom GIV Sem, No 1085 144nonaly end Rapflebon Mot N423TT 2 Owe Nwrm (Al Mean OfrAYAStraVari ON/Ecole) TRT Leasing Address (As Moen oa mplifilibbn CMIFCMO) 515 N Flag*/ Or STE P400 West Palm Beach, FL 334014320 3. For FAA Um Mk 4. UM 109neficeeon 4 Type UM MOP Mcdel 34041 He Rea Miriam AIRFRAME X (As described In Hem 1 above) PCP, t RP. ANT PROPELLER lice APPLIANCE lAndscosee 4 ConfomMy Meepre4 A Apncys NY* and MOAN B Kid .: iAgar/ C. Cenficee. No. CE Avionics, Inc. 2789 Fightllne Avenue Sanford, FL 32773 us. CeAlPedNecrenK 0E4R411M Famign Called Mithant. X CP1E•A Roper Saban Monawaset 0 I owe I y tat OM Wee Reba MielefaCa made to to unAls)MInflocl hells atom end lerscrtal onV* mem et enschmens MMO hen been cede in eeeerdame del Me repatments of PM 43 44 the U.9. F eat& Avalon Regalscrs rats IPA • lortsebOi twililhed Bain le sme and coma to Iheeeel el Pm WeeMelie Ca May 22, 2007 &Oran cfluilwreed tilmduel . doe ./: Michael E. Hughes • 7. approval for Rohn to Swam MW MM •..fley ran pram spew beCre Si. MM IderMsd Si am • pas mewled n we warner welarblatfl e• ACINNIVOlot of me Few,. Anew Armen.= et le El APPROVED 0 REJECTED FAA Ft StanPirdt Minaarer inspomanhartamen salw Mayan aapaca. BY FM Dowee X Reeler NOM Pence 90,0•4 TV TremPM Cana Anyonlemis OM. OOP a I Appian' or RESPIOn May 22, 2007 Cat mem ot EsPranon He st We 4 / Iatreasecilnilatilw)us ict a / s ir d $i 0.i ...... 0E4R411M tio . Michael E. NuoMs am Fenn MY mat) SONY GM_02753838 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240758 EFTA01326351 NOTICE Weight and balance or operating limitation changes shall be entered in the apProOnate aircraft record. An alteration must be compatible with all previous itterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished Of more space Is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) Removed Collins Part Number 822.9210-008 TDR-94D Mode S Diversity Transponders Serial Numbers 2221 and 3672 and Installed factory modified per Service Bulletin 504 to Part Number 822-9210-308 (Enhanced Surveillance) Serial Numbers ICBM and 4J2W. Interfaced the TDR.940 to the Number 1 and Number 2 Honeywell HGT1075AE03 Inertial Reference Systems and made additional voting changes per CE Avionics, Inc. Drawing Number 5893B-t. Revision UR dated March 22, 2007 (Approved on FAA Form 8110-3 dated May 21, 2007 by Leslie S Roblin. DERT-510335-CE - Systems & Equ talent). The installation was made In ccapitance with Gulfstream IV Arming Diagram Manual Revision 52, dated December 31. 2008, Chapter 20. Sections 20-24-00.20.25-07, 20-28-00 and 20-28-09; Chapter 34, Section 34.02-04; and in compliance with FAR 25.1301, 25.1309 and 25.1431. END￾El Mani S , l InAllatred (1 Page) US.OPD:1989-0653.171 SDNY_GM_02 753837 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240759 EFTA01326352 Armament. FAA Fr 337 Dated May 22, 2007, N4237T.Gulfstream 04V, Mu 1085. Sheet I of DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 21, 2007 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstrcam Aerospace Corp. MODEL NO G-IV TYPE (Airplane. Rano. Helicopes. sac) . Airplane NAME OF APPLICANT CE Avionics, Inc. Sanford, Fl. LIST OF DATA IDENTIFICATION TITLE 5893B-1, Rev IR, dated 5.21.07 Additional Wiring for Transponder Mode S Surveillance END Notes: I) The electrical gyms only of the above listed dm at approved Main Thissprat is for ensineerns design data only. It ndicaes die dna liseclabove romances retie= only Min the regulations specified by wrap* std subparagraph tided tebw as- Applicable Requirements". 2) Cornplimce vrith addi ionalreaula ins Inc listed my to required This trot does not confide FAA approvalorall the coalman's dm nccessry be subset in bn of =Siam to necessary requirements br Meat Se Mention. The a iia unit area s are esst Related in this 'preys]. 3) After the Akar an, thesimnel must be let urned to service by FAAmawcod pained PURPOSE OF DATA: Design approval in support of major attention, installation of Elementary & Advanced ATC Surveillance (Flight ID) Transponder System on Gulfstrearn 0-I VSerics aircraft, serial number 1085, registration no. N42317: Systems & Equipment Design Approval Only. APPLICABLE REQUIREMENTS of Title 14 CFR (List specific sections) FAR 25.869 (aX4) FAR 25.1357 (aXc) FAR 25.1301 (aXbXe)(d) FAR 25.1381 (exb) FAR 25.1353 (bXd) CERTIFICATION - u........ ....t. Sc.. Son inl In .ult. that auiribet•J MOM 'Wigton awash. a (................ ,we wawa ass amass Sapp:non aim Psn in sr au F.S.. Amara RAMakm. Pm has iit•Odain sub enialAwd pectin end kmad is WW1 with illpialis 'Kris.. MMNana A"... P.O.W. O Recommend eppoval of Mn data I (We) llecrefore eil Amore these data SIGNATUREM OF DESIGNAT ENG ERI RE E REM DESIGNATION NUMBER(S) CLASSIFICATIONIS) Leslie S. Roblin • DERT-510335-CE Systems & Equipment FAA Form 8110-3 (I140)SUPERSEDES PREVIOUS EDITION (0 V Rob alt3 doe) 010509 GPO 901113 SDNY_GM_02753838 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240760 EFTA01326353 SDNY_GM_027.839 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240761 EFTA01326354 0 MAJOR REPAIR AND ALTERATION tilift...... 0 T wear las mum. (Airframe, Powerplant, Propeller, or Appliance) sans. OMBFOrm *Waved MO 21204020 For FM 13•4 Over Mob lanfloatien INSTRUCTIONS Rt4 a tope d eines See FAR 419. FAR434cent O. W AC 419.1 a eteeepril melon Owed) Kw ingevakee and dfloslion et en Van Pio neon i~e3 le lea (H1.1C 021) Fein ea repon one* m 4 del penile nab ease III.0)D low each es. *Ake (Seaers901 F40401 Aeelen Ao 1959) s. myna PAW, GULFSTREAM Model G-N, sols Ma 1085 Petbraff W Rama,Mot N42317 1 Omer Nun fAr row on,.walla, colikeel TRT LEASING INC Amer (A, shown eNoever. oNellceON 515N RACIER DR SUITE P400 WEST PALM BEACH. FL 334014320 3. Fee DA Use Only 4. UM kkalikallen L TIT.* UM IIIS Rea Solid No Ream Metsbat AIRFRANE 0 9 As dissafInd In awn 1 above PONERKANT El 0 INIDPELLER 0 0 OPPLINCE Type 0 0 M 0 blenulwitror S. Coreenrely Sleernerd A Preis Nee in4Addreee S. Fib d AireY C. Carthal• ft ALAN D. REDMON 200 REDMON RIDGE DAWSONVILLE, GA 30534 u S Cedes! Mocha 3107552 MP Fasin Ceded Moen tame two. Han wassAist D I <fly It WO ewe flee eleraeco ale 43 we eat) Itilelled Mabee tore ere Suited onIre nem a ellienneeT hereto hen been as n ecoortlence Ise re • ellterthiels ol Pe 43 cf a U S Flideil Meson Repealer* eel era seconelon WOW ninon a no incl one le Se bog deny Ircaleapi 0414 4 APRIL 2007 Syrian of ()drs. / ..---...-'•-----."' 7. for ex Antal to to alliOnty Oven moons aged billo,the int Adetrailnkt 011/10 rowel MA200)Admedereen Ind a MM., in is 4 wee areplosci in toe worm preacited by IN el APPROVED 0 REJECTED BY ri '—' FM FS StenderdS Inspecior O lAwascluw Irabun AW:notion (Spay) O ;SA 000trose O Repsep Slam New .440fteed IN Treaty Cale Nreetileito Creep \ 1 Dal* *I Approve/ or Reran 4 APRIL 2007 .. _ °Macs* Oelepriece NO 3107562 a Snows MAN D. /,4_,.-- /) \ %--....." s:zr SDNY_GM_02753840 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240762 EFTA01326355 NOTICE Weight and belance oroperating limitation changes shall be entered in the apProPrIste astiallredard An einem^ must be compabble with all previous alterations to assure continued conlommy with the applicable airworthiness requirements 8. Description of Work Accomplished (0N more Spies is required, at additional sheets. Identify with onsralt nabonakty and registration mark and date work completed) AIRCRAFT MODIFIED: N42377 G-IV SS 1055 4 APRIL 2007 1. THE FOLLOWING WORK WAS ACCOMPLISHED BY CAPITOL AVIATION SERVICES: REMOVED DUAL TRANSPONDERS AND UPGRADED WITH NEW FUGHT ID UNITS. 2. REMOVED DUAL COLONS TOR-94 TRANSPONDERS AM) RTU-4210 CONTROL HEADS AND INSTALLED DUAL TDR940 TRANSPONDERS P/N 622-9210-005 SI 2221 8. S8 3872 WITH CONTROL HEADS RTU-4210 P/N 822-0838-015 SA 267 8 Se 1176 PER ROCKWELL COLLINS STC 01142W-0 AND IS SUPPLEMENTED WITH ENHANCED SURVEILLANCE USING ROCKWELL COLLINS CMM P/N 523-0778502 REV 3 DATED 10 NOV 2008 AND SERVICE INFOR1MT1ON LETTER SIL-1.04 ALONG WITH DRAWINGS NO CC-040407 REV IR APPROVED BY DER ANDREW K. ANDERSON ON FM FORM 8110-3 DATED 4 APRIL 07. THE INSTALLED MODES SYSTEM SATISFIES THE DATA REQUIREMENTS OF ICAO DOC 7030/4. REGIONAL SUPPLEMENTARY PROCEDURES FOR SSR MODES ENHANCED SURVEILLANCE IN DESIGNATED EUROPEAN AIRSPACE. 3. CONTROL OPERATION INFO.: REFER TO ROCKWELL COLLINS PROUNE II PILOTS GUIDE DOCUMENT NUMBER 523-0773070- 004117, DATED JULY 14, 1993, OR LATER APPROVED REVISION. 4. SERVICE INFORMATION: REFER TO COLUNS CMM REFERENCED ABOVE. 5. MAINTENANCE INSTRUCTIONS: REFER TO COLLINS CANA REFERENCED ABOVE. 6. TROUBLESHOOT INFORMATION: REFER TO COLUNS CMM REFERENCED ABOVE. 7. REMOVAL ANO REPLACEMENT: REFER TO COLLINS CMOS REFERENCED ABOVE. 8. DIAGRAMS: N/A 9. SPECIAL INSPECTION REQUIREMENTS: NONE 10. APPLICATION OF PROTECTIVE COATINGS: WA 11. DATA NO HARDWARE WAS REQUIRED. 12. UST OF SPECIAL TOOLS: NONE 13. FOR COMMUTER CATEGORY AIRCRAFT: N/A 14. RECOMMENDED OVERHAUL PERIODS: NO ADDITIONAL LIMITATIONS. 15. AIRWORTHINESS UMITATIONS: NONE AT THIS TIME. 16. REVISIONS: A LETTER WILL BE SUBMITTED TO THE LOCAL FSDO WITH A COPY OF THE REVISED FM FORM 337 -END_ A} 0 AddilcrelfropS An Allmo's, U.S.OP0:1989-0463-171 SDNY_GM_02753841 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240763 EFTA01326356 Apr 04 07 09:32a Andrew Anderson 770-387-0701 P • 1 U S. OEPARASENT OF TRANSPONTAIION FEDERAL AvallON Aramosnunon STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Apn1-04-2007 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MANE Gulfstream MODEL NO. G-IV 'TYPE tithatm Radm fralitaba et) Airplane MANE Of APPUCAXT Private Consultant to ATS INC LIST OF DATA MENDFICATION 'RAE CC-040407 Flight VD Installation (Dated 04-04-2007 Rev VR) PURPOSE OF DATA In support of major modification for SIN 1085 ONLY. APPUCABLE RECIUREMEXTS dal mice smut 25.1309 (a)(b)(c)(dXeXg) 25.1351 (a) 25.1357 (aXt4(6)(6)(e)(9) CERTIFICATION - under authal(y el by dlitarti of the AcInnatrafor and In womb= NM oamtdions end lialittorm et OppoirdrUtif Latta Part 103 of N. Ficleral Mallon ReOutrons. au Wed alien and on attached staters numbered r arta hare been auatted In accordance's* astabGalyarl doceduras NM found to =oh Idth alIoNable nutternets of Me Foetal Aviatch Repubsbars. 0 Recommits:1 approval amen data I Thetein (83 Approve Sew data S pil e s) OF TED EWXNEEFUN(3 RF_PRESERTATNE(5) IDESIGNIIIM7 FliFISERAS) CLASSFrATONA 4n t. DE RT-510004-CE System & Equipment FliaM Analyst Andrew7 Anderson FM Form 11104 (t1.70) SUPERSEDES PREVIOUS ECITION ELECTRONIC FORMAT (7.03) SDNY_GM_02753842 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240764 EFTA01326357 SDNY GM 02753843 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240765 EFTA01326358 fr 0 , L. : esenrani • MAJOR REPAIR AND ALTERATION • ' af tillrannislai . (AI:frame. posemplvd, Propeller. or Appliance) Fowl Appeased Elicirmt robesMats CSOM.2111)403) 11/30107? Mc FAA um den ... .. Alniblillelfaa i -. .‘ INSTRUCTIONS: Print a type all greet Sao Me 14 CFR 4µa. Part 43 Appendix B. and At 43.94 (or etiongse mann thereon for irenctorts end Minabon of It form. Thee report le wined by km (49 U.B.C. .44701) Fans to report cannot. hada prey to tech much Nolen. (49 U S.C. §48301(a)) . ' I. Aircraft ova "le-tYand jigiets161:111-441 N677RP i scrim No. . 1085 make Gulfsueam ilothi G-IV sea 2. Owner Nana (Ai Man cerillon) Arkbers (/4 Moan on regkorattn oartlAcate) raini,15 N Eisele: Dr. Suite P400 r • • . cn reglanden TRT Leasing Inc. ay • .West Palm Beach are as 33410-4320 ea r USA • • S. PerliAlle Um Only . . 4. r/Ps 6. Unit Identification . Repot Mallon UM Araks Model Sinai No. 0 IN AIRFRAME . - - (A it assambe I Magi I above) O • ... - . O PONSMUJIT • ' .. . _. ... . RECEIVED . .. . . . - . ... : pRpp,....,t .... . . . . • ---• • • •••- . • - - . - El - APPLIANCE 'type ASW - FSDO OK : Lardocaser 4 Conformity Ittornort A. Agency's Name and Address B. Ktnd a Agency id. Associated Acro.Senn ice u. a. unkaaid Mechanic 1 tranuracon nom PO Box 1310 rarely Carercateci Mechanic C. Certdkate No. ow Oklahoma City an OK ..x Gellman Rena Eamon D, 73008 o w., USA SSWR I 86K caiiii Enno,.. . —es Orartaten D. I astly !het the repair anon alteration made to the unit e) kientleed in Item 6 above aid deacrIbed on the reverse or attachrrants Anti Sive boon nude in amo-danco rah the requirements of Part 43 of the US. Fenn Aviation Regulations and that the inbrmaton fantod hareln le Ina and carob to the tint of my Imosiedge. Extended range hal per 14CFR Pert 43 E App. El Sisnahreibets of Authated Incilvklual d i e Awce/A-re.,7> 4. a 4, - _COL V 'c, ( 7.-...g12.- Y. Et/eA r )ty - 1,--- 71,--;717 .77 7. Ape rand for Ran to Site Pursuant to the *Wintry given persona snarled baba. the unk identified in /tern 5 was Impeded h the manner proscribed by the Adenbiletretor of the Federal Antal Adman:atm midis 0 Approved 0 Reflected FAA FitStendards - .- Ilanufachrer Mentenance Organization Panora ACORMS MiCillibtien -. . . illipeCitt Ommilmeni a/ Imielpiel • FAA Dilignse ._ . . .. _ . ._ . _ . Repea le r y irssectial Autortzslon Other (Specify) - - Certinte a . Otaignatkin M.. liA2- 2 3 14‘iel 901inglikillafAtentledtralniduel ,.. , 7.; ., ;;Z:‘,.. . . I/. .. . tr i; di4 - . " " . --retN aidte.AOX -' ( o3/e37260-7) SDNYGM02753844 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240766 EFTA01326359 NOTICE • • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be Compatible with all previous alterations to assure continued confonnitysvith the applicable airworthiness requirements. 8. Description of Work Accomplished alman space fa reyndral. mach additional sheets. identify with aircraft nationality and registration Mark and date work coatpkier 1 Aircraft Make GulfAreom.. . Model GIV . Serial Pluinber1085 Reiiiiradoe Nia7RP Date03/00007 . , . . Installed Gulfitream'ingineefecfrepairs at fiVe lOattiOns on ilie upper akin of the floor panels in the cabin area. Reference.thecntlfatteant $E05005902 Rev. IR drawing: : All doubler material is 2024-T3 0.050 thick. All replacement core material is 5.7-3/16-20N 5052. All bonds were made using EA9309.3NA adhesive. Drawing INSTL No. Doubler Diameter F.S. R.B.L. L.B.L.. -1 5.60 489.43 28.22 -3 6.40 476.45 28.57 -5 5.90 . 475.66 16.75 -7 6.70 482.41 28.78 -9 6.90 481.19 16.32 This repair was done in accordance with the GulfstreamSE05005902 Rev. IR drawing and the Gulfstream engineering 8110-3 form, Identification SE40001085 Rev. B, dated 03/07/2007. There is no change to the aircraft Weight and Balance or Equipment List. . For Continued Airworthiness reference the aircraft manufacturer's applicable data. With respect to the work referenced in the Associated Aero Service work order number 4635, this aircraft has been found safe for return to service. END El Additional Sheets Arc Attached S 0 P01990.761.751 SDNY_GM_02 753845 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240767 EFTA01326360 03/12/2007 69:22 25519 TECHOP S T RUC T LIRE '3 PAGE NS 0 AG' US. DEPARTMENT OP TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 03 / 1916-Ce / .3--- ' 'AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION - . MAKE .. i - Gulfstieam MODEL NO. 0-tV S/N LOSS TYPE: tabus. rues aseresec at . -Airplane .. -NAME OF APPLICANT . . ., • - - . • .. . . .. .. . — - . • . . . . .. . Culfetreani Agit:aspect Conioration • LIST OF DATA IDENTIFICATION TITLE SE40001085 REV B --______ .., • : TOP DRAWING - REPAIR/MODIFICATION, G-IV S/N 1085 END OF DATA ------- only of the above listed data are approved herein. This design data and is not installation data. ' ' • --- NOTE: The structural aspects approval is only for the Engineering PURPOSE OF DATA • Support major repair for G-IV sin 1085. APPLICABLE REQUIREMENTS (Lin specific sections) FAR 25.601 CERTITICATION - Under authority appointment under Pan I ID of the have been vested by direction of the Administrator and in accordance with condition and limitations of Federal Aviation Regulations, data listed above and on ached sheets numbered examined in accordance with enablishol procedure. and found to comply with applicable Regulations. Recontnattxl approval of these data ve these data requitements oft's< Federal Aviation O OWe) Therefore SIGNATURE(S) OF DESIONA ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) • 146 1'44 12 .;-- it. Robert H. Drinnon, Jr. DER Y-51117S-CE Structures FAA Form 8110-3 mane SDNY_GM_02753846 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240768 EFTA01326361 SDNY_GM_02753847 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240769 EFTA01326362 Form Approved OMB No 21210020 MAJOR REPAIR AND ALTERATION us. owenweili For FAA Use *ray at Tranwartrtol (Airframe, Powerplant, Propeller, or Appliance) FecWsl AA•0on Ades least-40.n Office Idertiticaton VINN X00 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appal& B, and AC 439-1 (or stbsequerd revision thereof) for inn ions and deposition of this lone. This reports required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty rot to exceed 51.000 for each such violation (Section 931 Federal Aviation Act 1958) 1. Aircraft mon Gil/stream *al GIV Sew tee. 1085 Swear and Rildenten Wen/ N677RP 2. Owner Nwns (As ilwaN on rophbvtlx. Estate) Petersen Aviation &knee (Ae Moan 0e leeettebee CeteGk) 7155 Vatican Ave Van Nuys CA 91406-3917 3. For FM Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As descnbed in item 1 above) X POWERPLANT PROPELLER APPLIANCE NM MAMAPCILMIt 6. CoolomitlyStatement A Agency's Name and Address 9. 10nd dAgratcy C. Cerblicale No. X U.S CsencaltOeortere Damon Midgette ASP565174728 4828 Adele Court Woodland Hills. CA 91384 FralenCereforged mega Cerleostes hew satin Menaces D. /certify that the repar and/or alteration made to the urk(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accorda roe with the requirements of Part 43c4 the U.S. Federal Aviation Regulaticns and that the information furnished herein is true and correct to the best of my knowledge. Date 919 Irina ter' /0/23/93 7. Approval for Retum To Service Ptrauard to the a /holey given persons specified below, the wit iderefied in item 4 was inspected in the manner prescribed by the Adminstrator of the Federal Aviation Administration and s a APPROVED RE.ECTED sr FAA Flt St a rstirds aspect*, Manufacturer X Inspedion Adhestration Other (Specify) FM Designee Repair Station caoesion est uiseeron r Dale clApprowl a Rojection 1O/1 3/ 0 3 CenkRIA OP Ceelgeollon EA I/Mr /Mr ir SignAlralp FAA Form 337 (12 SDNYGM02753848 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240770 EFTA01326363 SDNY_GM_02753849 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240771 EFTA01326364 NO110E Weight and balance or operating limitation changes shed; be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued =O:porgy with the applicable airworthiness requirements. 8. Description of Work Accomplished 01 more space is required, each addrtional sheets. (den* vett aircraft nationality end registration mark and date work completed) Reconfigtred cabin interior per STC STO1sssl A See Master Drawing List report SAM -1-02 approved by the FAA on 1021/03. see letter of approval dated 10r20/03 signed by Alan T. Shinseki. Manager, Systems and Equipment Branch. Los Angeles Aircraft Certification Office. ❑ AMIloral moans Attached FAA Fon 337 MN) . US. OP0.1989-0-663-17I SONY_GM_02753850 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240772 EFTA01326365 SDNY_GM_02753851 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240773 EFTA01326366 10/21/2003 02:37 FAX 562 827 5210 FAA LAACO 1ST FLA FAX Q1001 • 3gratebliteeta poreeetta papa:tent of gransportation - eater 4,1kEriactires Sthnsististcalier; $uppfnuental Zue dertifirate Afeendes ST01555LA .574.c a4ta.dle Syncro Aircraft Interiors, Inc. 7701 Woodley /Avenue Van Nays, Ca 91406 .--1/1, axe der agerape d• 4540 04 *4A. zdtemearantaaamara, Astizetst.t end co-2 ‘44ro t atray-e$ yrevanionseses emaienyrdeerdirs npierieurearhe 19d 25* 166 Federal Aviation ...98esagsreavo, *Catification basis is set tenth in Type Certificate Data Sheet Al2EA araiTegkacOe .SS.• i f f••••, * Sonde.: Angg Sae: Gulfstream ...a0edet G-1V S/14 1085 ..§flosvivas, te..fess Siscja &Cyr Cabin interior re-configuration in accordance with Syncro Master Drawing List SA11-1-02 Rev, NC, dated October 12, 2003, or later FAA approved revision. Salnetaaas cadraidaevair Data pertaining to this modification is considered inadequate for duplication oa other aircraft This approval is limited to the installation made mthilfstream Cr1V Serial Number 1085. A copy of this STC must be included in the permanent records of the modified aircraft. tage4e4ak Rea 44440arialf delta 41.4,4 14 444 4.444A. entitlerataWi•dtl:, OiD ea, egaisearammenee Jotassicee 0 Ce Od• a isornistrays ria.4 a odano4s a+ 44 agessimarnerc744 .rts...c at/Sara'''. Asinsaa(gr.14.v. 0.4 August 12, 2003 Arlo• .1.4.iesscace .• October 21, 2003 MTh, isluasse: arale .t.paseace.• .53). eravaiw Vo4 -44 • Wittaccs) Alan Sbinseki Manager, SYsteass and Equipment, Los Angeles Aircraft Certification Office (rdk) -e ma i••••14rmnartil not MCCAW 3 yea; " SDNY_GM_02753852 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240774 EFTA01326367 SDNY_GM_027.8. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240775 EFTA01326368 tit doormen olomnionan MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Um Only Office Identification NIN`C F‘. Do reetermarnmen steam INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix (3; and AC 43.9-1 (or subsequent revision thereof) for inStruct inn and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Aci of 1950). 1 .Aircraft Make GULFSTREAM AEROSPACE CORP. Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA a. Owner Name (As shown on registration certificate) BA LEASING & CAPITAL CORP. Address (As shown on registration certificate) TWO EMBARCADERO CENTER SAN FRANCISCO CA. 94111 3. For FAA Use Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ' (As described in Item I above) xx POWERPLANT PROPELLER APPLIANCE Type Manulacturer 6 Conformity Statement A Agency's Name and Address B. Kind of Agency C. Certificate No. It LANCE A. MATTESON 2407 EAST SHEA BLVD. PHOENIX, ARIZONA 85028 U.S. Certificated lawNnic AP 1864049 Forerun Corldicated Mechanic 04eldicated hew Station Manulacturer 0. I Gerrity that the Waif and/or &Cormier) mad to the un Ifs) identified in item 4 above and described on lhe reverse or attachments hereto have been mule in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date i .— / s 7- ?a Signature of or d Ir‘vid K. 7. Approval for Return To Sonic upt. of Maintenance Pursuant Administrator BY to the authority given persons specified below. the unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is qii APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer XXvInspection Authorization Other [Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection /11-re Certificate or Designation No. 5267054_94 Signature of Authori is fliduai SDNY_GM_02753854 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240776 EFTA01326369 NOTICE Weight and balance or operating limitation changes shall be entered ,n the appropriareaircralt record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description ol Wont Accomplished (it more space is required. attach additions, sheets ldenldy with aircraft nationality and repostiarion mark and date work completed.) JANUARY 15, 1990, GULFSTREAM AEROSPACE CORPORATION MODEL G-IV, SiN 1085, N88GA, FAA Type Certificate Data Sheet Al2EA. REFER TO: GAC Maintenance Manual, Illustrated Parts Catalog, and Wiring DIAGRAM MANUAL ATA Chapter(s), 22 AUTOPILOT, 24 Electrical Power, 32 LANDING GEAR; HONEYWELL CORP. Maintenance Manual for the SPZ-8000 INTEGRATED FLIGHT MANAGEMENT SYSTEM; GREYHOUND CORP. NUTCRACKER RIGHT MAIN DC AND/OR ESSENTIAL DC MODIFICATION, ELECTRICAL DhU. No. 32122589, dated 12-25-89. see DER APPROVED FAA Form 8110-3 dated January 10, 1990. The purpose of this alteration is to eliminate the failure of Flight Guidance Computer (FIGC] number 2 whenever power is momentarily lost on the 28 Volt DC Essential Bus because of automatic bus switching. Performed all of the "MODIFICATION INSTRUCTIONS" contained on Greyhound Corp. Electrical Dwg. No. 32122589, referred to above, in compliance with FAR 43.13 Performance rules (general) (a)(b). All parts that were installed were new at the time of installation and comply with FAR 21.303 (b)(1)(2)(4). Tested the modification in accordance with all steps titled '"TESTING THE MODIFICATION" contained on Greyhound Corp. Electrical Dwg. No. 32122589, referred to above, and noted no abnormal or unusual results before, during, or after the testing sequence. Recorded compliance with this FAA form 337 in the aircraft's maintenance records, in accordance with FAR 43.9(a)(1)(2)(3)(4) and complied with the requirements of FAR 43 Appendix B (a)(1)(2)(3). It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination included, but was not limited to, consideration that this modification provides power to the nut￾cracker relay circuits in a similar manner that the Gulfstream Model G1159 and G1159A non-VSCF aircraft utilize, as a result of this modification the installed FGC equipment can function safely and properly as it was intended, and the following specific sections of the applicable requirements of the Federal Aviation Regulations have been complied with: 25.1301(a)(b)(c)(d), 25.1309(a), 25.1353(a), 25.1357(a)(c), and 25.1359(d). There were no changes to the aircraft's electrical load analysis and the effect upon the aircraft's weight and balance report is negligible. ****END OF THIS SHEET****Greyhound Corp. Dwg. 32122589 is attached ❑ Additional Sheets Are Attached SDNY_GM_02753855 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240777 EFTA01326370 • .., • . 0 MAJOR REPAIR AND ALTERATION US Ocorrnee. aeon osmon (Airframe, Powerplant, Propeller, or Appliance) Weenellivicifien AdOeradreelen Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification Jr PC ParIZ)O INSTRUCTIONS: Print or type all entries. Sea FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) ) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to repon can result i acivil penalty nol to exceed $1.000 for each such violation (Section 901 Federal Aviation Act 011956). I. .Aircraft Make GULFSTREAM AEROSPACE CORP. Model G —IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) BA LEASING & CAPITAL CORP. Address (As shown On registration certificate) TWO EMBARCADERO CENTER SAN FRANCISCO CA. 94111 3. For FAA Use Only 4. Unlit IdentlfIcalion 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) XX POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. LANCE A. MATTESON 2407 EAST SHEA BLVD. PHOENIX, ARIZONA 85028 x US Certificated Mecham< AP 1864049 Foreign Ceeld 'Med liAeCheniC manufanifICAIMS CO %VIC StillI011 cturer D s certify that the repair and/or alteration made to the un f(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 430f the U.S. Federal Aviation Regulations and that the information furnished herein is true and Correct to the best of my knowledge. Coate Signature of A ed Indwidus T. Approval for Return To Sr*? upt. Ot matntenance Pursuant Administrator BY to the authority given persons specified below. We unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is .4) APPROVED O REJECTED t Standards FAA Fi M WMOr Manufacturer XX IrtepectiOn AuthOreratiOn Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Refection /—/e -90 t Certificate or Designation No. 26705494 Signature 01 Authorized idual Orr SDNY_GM_02753856 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240778 EFTA01326371 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description col Work Accomplished (U more space is required. attach additional sheets Identity With 811Cfel nationality and registration mark and date work compleunt1 JANUARY 15, 1990, GULFSTREAM AEROSPACE CORPORATION MODEL G -IV, S/N 1085, • N88GA, FAA Type Certificate Data Sheet Al2EA. REFER TO: GULFSTREAM AEROSPACE CORP. (GAC] MAINTENANCE MANUAL, ILLUSTRATED PARTS LIST, AND WIRING DIAGRAM MADATAL - ATA CHAPTER 49; GARRETT AIRESEARCH AUXILIARY POWER UNIT MAINTENANCE MANUAL 49-21-89 FOR MODEL GTCP36-1CCG; GREYHOUND CORP. API SURGE VALVE CONTROL MODIFICATION ELECTRICAL CHG. No. 49122489, dated 12-24-89, see D€ APPROVED FAA Form 8110-3 dated January 10, 1990. The purpose of this alteration is to eliminate a nuisance operation of the PPUes surge control valve whenever power is momentarily lost on the 28 Volt Essential Bus because of automatic bus switching. Performed all of the modification instructions contained on Greyhound Corp. Electrical Dwg. No. 49122489, referred to above, in compliance with FAR 43.13 Performance rules (general) (a)(b). All parts that were installed were new at the time of installation and comply with FAR 21.303 (b)(1)(2)(4). Tested the modification in accordance with all steps titled "TESTING THE MODIFICATION" contained on Greyhound Corp. Electrical Dwg. No. 49122489, referred to above, and noted no abnormal or unusual results before, during, or after the testing sequences. Recorded compliance with this FAA form 337 in the aircraft's maintenance records in accordance with FAR 43.9 (a)(1)(2(2)(4) and complied with the requirements of FAR 43 Appendix B (a)(1)(2(3). It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination included, but was not limited to, consideration that this modification provides power from the same power source that the Gulfstream Aerospace Model G1159A (VSCF) (GIII) aircraft uses to control the APU's surge control valve, the installed equipment will function safely and properly as it was intended and the following specific sections of the applicable requirements of the Federal Aviation Regulations have been complied with: 25.1301(a)(b)(c)(d), 25.1309(a), 25.1353(a), 25.1357(a)(c), and 25.1359(d). There were no changes to the aircraft's electrical load analysis and the effect upon the aircraft's weight and balance report is negligible. ****END OF THIS SHEET""Greyhound Corp Dwg. 49122489 is attached ❑ Additional Sheets Are Attached SDNY_GNL02753857 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240779 EFTA01326372 US DEPARTMENT OF TRANSPORTATION . , FEDERAL AVIATION ADMINISTRATION MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) Fen. Apron', Sweet Berne No. as-Ro60.r FOR FAA USE ONLY DE \ OFFICE N J NTWICATION I CSQD INSTRUCTIONS: Print or type all entries. Ste FAR 43.9. F 1R 43 Appendix B. and AC 43.9-I (or subsequent revision chereoll for instructions end disposition of this form. 1. AIRCRAFT mAnGulfstream Aerospace MOOEL G-IV SERIµ NO. .NATIONALITY AND REGISTRATION MARK 1085 , N88GA NAME (Ai 'Soon on registration nortincoro) i ADDRESS fro shown on registration tertikahlt 2. OWNER I BA Leasing and Capital Corp. ITwo Embarcadero Ctr, 10th Floor San Francisco, CA 94111 3. FOR FAA USE ONLY 4. UNIT IDENTIFICATION 5. TYPE UM? MALI NOM I Mem. NO. Wail wee. MVP. AIRFRAME de ;bed tern I x (A obo 0••••••••••••••••••••••• PoWettlANT PROPELLER APPLIANCE TVPI mthytACTUtal 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS R. KIND Of AGENCY C. CERTIFICATE NO. Western Commander, Inc. 16300 Daily Drive Van Nuys, CA 91406 U.S. ClititiCal0 mux.•.I6 REPAIR STATION #4221 —11- Ail A 4, R-I,2, Al Lila AAP FOittiON CtaloriCATI0 MCKANIC COITitiCATI0 suits STATION iiiANUIACTUala D. 1 musclemen's cenify that the repair and/or alteration made to the unit's) identified in item 4 above and described on the reverse or hereto have been made in accordance with he requirements of Pan 43 of the U.S. Federal Aviation Regulation! ead that the information furnished herein is true and correct to the ben of my knowledge. DATE September 7, 1989 SIGNA I OF AUTHORIUD - INDIVIDUAL e . 7. APPROVAL FOR ROM T SERVILE pen uan to the authority given persons specified below the unit identified in item 4 was inspected in the manner prescribed by - the Administrator of the Federal Aviation Adtnini ttanion and is 0 APPROVED 0 REJECTM BY P44 TIT. IITANOA191 nelfger011 IMMIPACIIMI INSPOCISON AUTICIUSATION OMR 4.00,) FAA Cillgatell x WWI STATION CANADIAN DEPARTMENT OP TM/MOW 'Mallet°. Or [ DATE OP APPROVAL OR REJKTION CERTIFICATE OR DESIGNATION NO. SIGN E OF AUTHOR?) II:rUartt ocy 9-7-89 #4221 D ny C. rnham, Chief Inspector . (7-en ($320) SDNY_GM_02753858 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240780 EFTA01326373 V.L.A3 - 8LetZ00 I O1103f8fS 3/W331O8d H3CI8O SHdV89V8Vd 'L '8 '6 '01 'ST PUB LT 629ESLZCINOANEIS NOTICE aircraft appropriate the in entered be shall changes limitation operating or balance and Weight An record. with conformity continued assure to alterations previous all with compatible be must alteration the requirements. airworthiness applicable sheets. additional attach required, is space more (If ACCOMPLISHED WORK OF DESCRIPTION 8. completed.) work date and mark registration and nationality aircraft with Identify on listed drawings per installed modifications Electrical and Avionic approved and 8-8-88 dated N/C #08000012 Drawing Top Commander Western -476. #NM DER by data per System Warning Proximity Ground V Mark Sundstrand Installed Western per performed deviations Minor SA218850. STC by approved -476. #NM DER by approved 2-8-88 dated N/C #08069091 drawing Commander accordance in System Sensor Lightning LSZ-850 Honeywell Installed Drawing Commadner Western and SA2388S0 STC by approved data with -476. #NM DER by approved 11-14-88, dated N/C 08069157 No. SA4749SW STC by approved data per Lights Logo Vore De Installed 1-21-88. dated #3 Rev. third a , (IRS) System Reference Inertial Honeywell third a Installed (3), Computers Navigation NZ910 System, Management Flight Honeywell data with accordance in Sensor VLF/OMEGA Honeywell Single a and SA3774NM. STC by approved revised. List Equipment and provided supplements Manual Flight revised. report balance and weight Aircraft END ATTACHED ARE SHEETS ADDITIONAL 6 AC/2490A FAA C /40260 I966-559.I2I TICE OF PRINTING GOVERNMENT U.S. 0 EFTA01326374 I LIS DEPARTMENT OF TRANSPORTATION FEDERAL AWATION•ADMINISTRADON 1 MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) Fenn A pproi _ . B.4410 8 eau.Vet.04 ROO I FOR FAA USE ONLY IDENTIFICATION 7 N‘( INSTRUCTIONS' Pnnt or type ell entries See FAR 4)9. F X R a) Appendix R. and AC 43.9-I lot subsequent revision thereon for instructions and disposition of this form. I. AIRCRAFT MAKE I MODEL Gulfstream Aerospace I G-IV . Mal NO. NATIONALITY AND REGISTRATION MARK 1085 i N88GA NAME (Ai shot', on registration cerrtigrott) ADDRESS (As show" on repoleolion erfiPcoTS) 2. On " 1 BA Leasing and Capital Corp. I Two Embarcadero Ctr, 10th Floor I San Francisco. LA 94111 3. FOR FAA USE ONLY 4. UNIT IDENTIFICATION S. TYPE UNIT MASS /*CPU I Stew. NO. WAN M111 •110N AIRFRAME ••••••••••••••••••••••••• (A de Med I ob two) •••••••••••••••••••••• X POWERKANT PROPELLER APPLIANCE POI ssaminemuest 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS I. KIND Of AGENCY C. CERTIFICATE NO. Western Commander, Inc. 16300 Daily Drive Van Nuys, CA 91406 V.S. CIITOKATID islettANIC REPAIR STATION #422I A-3 84, R1,2,87 Lit, A & p POTION CiatinCATIO AtICitANIC Y wall STATION atAstuFACTuate D. I certify that the repair and/or e 'on made to the 'mitts) identified in hens 4 above and described on the reverse or enechments hereto have been made in accordance with he requirements of Pan 45 of the U.S. Federal Aviation Regulation, sad that the information furnished herein is inn and correct to the best of my knowledge. DATE September 8, 1989 GNATURE OF i D INDIVIDU 7. APPROVAL FOR RETURN TO SERVICE Put uen to the euthoriey given persons specified below the unit identified in item 4 was inspected in the manner prescribed by the Adminietntor of the Federal Aviation Administration and is UAPPROVED OREJEL M./ SY FAA In STANDARDS petrol MANVFACTMORS lesSeKTION AUTHORIZATION 000 agyroW SA IMMOtell XX "PAM STATION CANN:MAN DEPAIITAMNT OF INSAKTOt OM Ala 2 DATE OP APPROVAI OR ON 9-8-1989 CERTIFICATE OR DESIGNATION NO #4221 SIGMA T E OP AUTHORIZED I DIVIDU LI- . nnv C Farnham. Chief Inspector AA Ponn 337 17-on 013201 SDNY_GM_02753860 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240782 EFTA01326375 £8LIWZ00ViSa 01_031$:ins 3AI1D3108d 2130180 SHdtql9V8Vd 'L '8 '6 '01 'ST Pim LT ANDS NO L99ESLZ0 NOTICE aircraft appropriate the in entered be shall changes limitation operating or balance and Weight An record. with conformity continued assure to alterations previous all with compatible be must alteration the requirements. airworthiness applicable sheets. additional attach required, is space more (If ACCOMPLISHED WORK OF DESCRIPTION 8. completed.) work date and mark registration and nationality aircraft with Identify with accordance in installed interior Custom Aerospace Gulfstream November dated 02 Revision #1159C-GER-023, Report the and 1988 14, Consulting in listed as reports following Inc. Engineers, Aerospace Interiors, Aero and -442 #NM DER by approved reports Drawing Inc., 1989. 28, August dated RAI-G-1085 per installed components major following The and reports the listed: as specifications Installation Bar L/H 1. AIN-52-2 CAE Installation Galley R/H 2. AIN-52-3 CAE Galley Crew Fed R/H 3. AIN-18-3 CAE Installation Entertainment T.V. 4. AIN-38-8 CAE Installation Cabinet Vanity 5. AIN-41-4 CAE Installation Cabinet Storage Stereo/ R/H & L/H 6. AIN-41-8 CAE Installation Bulkhead 7. AIN-38-26 CAE Net & Reinforcement Bulkhead 539.75 8. AIN-GIV-I CAE Inst. Installation Panel Service Toilet Aft 9. AIN-GIV-2 CAE Replacement Floorboard 10. AIN-GIV-4 CAE Installation Pedistal & containers Water 11. AIN-GIV-6 CAE Installation Net and Shelves Baggage Aft 12. AIN-GIV-8 CAE Installation Mast Drain 13. AIN-GIV-9 CAE Instalation Ladder Service 14. AIN-GIV-10 CAE Installation Toilet Aft 15. AIN-GIV-12 CAE Installation Box Tool Service 16. AIN-GIV-13 CAE Installation Track Seat 17. AIN-GIV-14 CAE meet materials covering and Insullation FAR of requirements the (a) paragraph 1 part F Appendix 25.853 in stated as (d) through -FR -1085 #AI Report Inc. Interiors, Aero 1989 7, September dated -45 Inc. Caleo, John by substantiated and -682. #NM DER FAA completion upon jacks on weighed Aircraft outfitting. of balance and weight and list Equipment revised. reports according accomplished workmanship All 5, Chapters 43-13-1A A.C. to 9, 1, Chapters 43-13-2A A.C. and 7 & 6, 13. & 12 END ATTACHED ARE SHEETS ADDITIONAL O AC724904 FAA C 1916-659.12O40260 FICE OF TING PRiN GOVERNMENT *U.S. EFTA01326376 ;eat of_ 27 4* • MAJOR REPAIR AND ALTERATION Form Approved OMR No. 21200020 OS Datong-mai celtarsortaion For FM Use Only liationi Aviation (Airframe, Powerplant, Propeller, or Appliance) Atrnintar • tiOn Office IdeabfiCagen„ „ tje‘rk air )Jae INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendtx B. and AC43.9-1 (or subsequent revision theme° for instruct/cos and disposition of this fon. This is required by law (49 U.S.C. 1421). Failure o report can result in a civil penalty not lo exceed S 1000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. make GOLFSTREAM model CIV Aircraft Sabi No 1085 Nalianaky end Ropisoraien Mark N677RP 2. Owner Name (As sites on registraton eerbfkale) PETERSEN AVIATION Address (As shone on registration comitano 7155 VALJEAN AVE. VAN NUYS, CA 91406 3. For FAA Use Only The data identified herein only for above describe aircraf 43.7. FAA INSPECTOR WP-FSDO-1 compli with a plicable al rthin 5 requirements and is approved •ubject con i;y fie on by a person authorized in FAR y DATE: dad .15 ..#1;21r e 4. Unit Identification 5. Typo Unit • Serial No. Repair Anenwon AIRFRAME (As described In Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8. Conformity Statement A. Agency's Name and Address B. /0nd of Agency C. Certificate No. Ire AVIONICS INC. U. S. Certified Mechanic AQ4ROS9N RADIO CI. 2, 3 7035 SOPHIA AVE. Foreign Certified Mechanic LTD INSTR VAN NUYS, CA 91406 X Certified Repair Station LTD AIRPRAHS AQ4R059N Manutachrer D. I certify that the repair and/or alteration made to the can t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance w tit the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my knowledge. Date //aS/20cs￾Signature of Authorized Individual etaa17-‘ 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is g APPROVED O REJECTED FAA Ft Standards Impeder Manufacturer in Auttniurition Other (Specify) BY FM Desiree X Repair Station Person Approved by Transport Canada Anvortrinees Grew Dale of Approval a Rejection Certlficate or Designation No. or / AQ4R059till Signature of Authorized Individual ........-^c z eta/ FM Form 337 (1241) SDNY_GM_02 753862 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240784 EFTA01326377 1 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N677RP Installed an Artex C-406-1 ELT P/N 453-5002. Antenna P/N 110-340. and Remote Switch P/N 345-6196-04. The installaben was done Ni accordance with AETEX document number: 570-5001 REV A. Reference 8110-3 Signed by Trevor Strong DER No. DERT60581NM for mounting approval of the antenna. The ELT was mounted at STA. 753.50. the antenna was mounted at STA. 633.00. The ELT Switch was mounted in the cockpit on the copilot's dzus rail at STA. 54.00. A 1 amp circuit breaker labeled 'ELT' was Installed on the copilots circuit breaker panel. Existing spare wires were used for the ELT system. Reference IFR Avkmics document no. ICAW AXE% 406 for Instruction for Continued Airworthiness. Mounting for el 03MpOnents and installation details are in compliance with applicable portions of AC.13-1I3 Chapters 11 and 12; AC 43.13-2A Chapters 2 and 3. The mountings are made on existing previously approved equipment shelves or location in the aircraft and meet strength requirements of AC 43.13-2A Chapter 1. ARTEX Description and operation manual document number 570-5001 was installed in the aircraft The ELT. Antenna. and the NAV interface unit meets TSO requirements C126. A logbook entry has been made. Wiring diagrams. Revised Weight 6 Balance and Equipment list Amendment have been provided as necessary. Work Order 39886 on Neat this agency covers the work describe above. ND El...ADDITIONAL SHEETS ARE ATTACHED • laGe03:1101.0.C46012/40036 SDNY_GIA_02 753863 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240785 EFTA01326378 IFR Avionics, Inc. • : 7035 Sophia Ave. Van Nuys CA. 91406 Instructions For Continued Airworthiness For a Artex ELT Document No. ICAW ARTEX 406 This alteration to this aircraft obligates the aircraft operator to include the following maintenance information provided by this document in the owner/operator's Aircraft Maintenance Manual and the ownedoperator's Aircraft Scheduled Maintenance Program. The Artex 406 ELT Line Replaceable Units' (LRU) maintenance is on condition and there is no periodic, preventative or scheduled maintenance required for the continued operation of this unit. Should any failure of the Artex 406 ELT System occur, it should be properly noted, and the unit should be removed from the aircraft. Once a failure has occurred, it is advisable to do a visual inspection of the Artex 406 ELT system. This inspection should include, but is not limited to the Artex 406 ELT mounting, the antenna, the NAV Interface Unit, associated wiring. and any related hardware. This inspection should be performed through elementary means. 1. Maintenance, repair. reinstallation and testing information for the Mex 406 ELT system in this aircraft are contained in the Artex Description, Operation, Installation, and Maintenance Manual document number 570- 5001 REV A. 2. The Line Replaceable Unit (LRU) part numbers and other necessary part numbers contained in the installation data documentation for this modification should be placed into the aircraft's owner/operators appropriate Illustrated Parts Catalog (IPC). 3. Wiring diagram information contained in the installation data documentation for this modification should be placed into the aircraft owner/operators appropriate airplane Wiring Diagram Manual. 4. The scheduled Maintenance tasks required by this modification are to added to the aircraft owner/operators appropriate airplane maintenance program are as follows: a. Perform on at least an annual basis a periodic inspection of the equipment rack, equipment mountings, associated wiring, cables, connectors, hardware, antenna and related aircraft structure for integrity, security, wear. chaffing, and etc. Special attention should be given to the aircraft primary structure with regards to fatigue and stress cracking, corrosion, and etc. NOTE: These inspections may appear as part of opportunity inspections or recommended Zonal inspection tasks. 5. Should it become necessary to remove a component of the Artex 406 ELT system, secure the associated cables and wiring, collar the applicable circuit breakers, placard the aircraft that the unit has been removed. Revise the weight & balance and the equipment list arid make a logbook entry stating the unit has been removed for service (refer to section 91.213 of Title 14 of the Code of Federal Regulations and/or the aircraft's MEL) 6. The Artex 406 ELT System and its related primary components can only be repaired at a factory authorized repair center or an appropriately rated FAA Part 145-repair station. NOTE: Should structural repairs be necessary to the airframe they should be performed in accordance with FAA approved data, the Structural Repair Manual from the Airframe manufacturer (SRM) or guidance contained in Advisory Circular (AC) 43.13-18, if applicable. 7. For additional information regarding this modification and the related equipment refer to the following documents: a. The Artex Description, Operation, Installation, and Maintenance Manual document number 570-5001 REV A. Page 1 of 1 SDNY GM 02753864 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240786 EFTA01326379 V SDNY GM 02753865 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240787 EFTA01326380 _ 0 MAJOR REPAIR AND ALTERATION arm (Airframe, Powerplant, Propeller, or Appliance) reatnal on ettentureatan Form Approved OMB No. 2120-0020 For FAA Use Only Office identification W/4 0 1— gOri CCA 0 INSTRUCTIONS:Print or typo all entries. SeeFAR43.9. FAR43Appendix B. and AC43.9-1 (or subsequent rewisionthereol) I or instructions and disposition of thislorm.Thisreport is required by law (49 U.S.C. 1421). Failure to report can result ina civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). • 1. Aircraft Make GULFSTREAM Model G-IV Serial No. 1085 Nationality and Registration Mark N677RP 2. Owner Name (As shown on registration certificate) PETERSEN AVIATION ROOMS (As shown on registration certificate) 7155 VALJEAN AVE VAN NUYS CA 914064917 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make . Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer • 8 Conformity Statement A. Aunty's Name and Address B. Kind of Agency C. Certificate No. IFR Avionics Inc. US. Certificated Mechanic AQ4R059M Radio Cl 1.2,3 LTD Instr. LTD Airframe. LTD Spec Service. 7035 Sophia Ave. Foreign Cettincatne Mechanic Van Nuys CA 91406 x Certificated Repair Station Manufacturer D. I certify thattherepairand/or alteration madelotheun have been made in accordance with the requirements furnished herein is true and correct to the best of my t(s)identifiedin itern4aboveanddescribedonthereverseorattachments hereto 01 Part 43 of the U.S. Federal Aviation Regulations and that the information knowledge. Date q-k-1, - Loot Signature of Authorized Individual 7. Approval for Return To j Se tt Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is xi APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) By FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval orRejection Certificate or 2040esignation No. q-(---4, -,, ANR05914 Signature of Autttrize dividual 6 FAA Fenn 337 0243a) SDNY_GM_02753866 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240788 EFTA01326381 • .6 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished Of more spaces required, attach adchtlonal sheets. Identify with as:craft nahonalify and reparrafron mark and date work completed.) N677RP Upgraded existing Honeywell TCAS II Traffic Collision Avoidance System (TCAS) to be Minimum Operating Performance Standards (MOPS) 7 version compliant (Change 7), in accordance with Gulfstream STC ST00711AT. Removed existing Honeywell TCAS II Traffic Collision Avoidance System Processor Part Number 4066010-904, SIN 93121994. Sent unit to manufacturer for Change 7 Mod, to be Minimum Operating Performance Standards (MOPS) 7 version compliant (Change 7). Received modified TCAS Processor, new Part Number 4066010-910, unit keeps same Serial Number . Reinstalled modified TCAS Processor in aircraft. Performed ground check of TCAS system. TCAS system passed ground check. Gulfstream Aerospace FM Approved Airplane Flight Manual Supplement Document No. SC41129M04, Rev. A. dated Jan 5, 2001 or later FAA Approved revision, is required with this installation. Instructions for Continued Airworthiness are part of STC contained in Report No. CE41 129A003, Rev. A. dated Jan 5, 2001 This modification does not effect the aircraft's existing Weight & Balance. Log Book entry has been made. Equipment List Amendment has been provided. Work Order 37783 on file at this agency covers the work described above. END 0 Additional Sheets Are Attached OMR. GOVERNMENT ►RINTING OF FICE: 1922-711-012/60157 SONY_GM_02753867 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240789 EFTA01326382 . ... ad- .. - I - MAJOR REPAIR AND ALTERATION US 0•0Celmerd a terecoreere (Airframe, Powerplant, Propeller, or Appliance) ows marten mMaminblrellen Form APPrOved OMB No. 21200020 For FAA Use Only Office Identification S/P1/- YNY -"AN INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) lot Instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 31.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM Model G4V Serial No. 1085 Nationality end Registration Mark N677RP 2 . Owner Name (As shown on registration certificate) PETERSEN AVIATION Address (As shown on registration certificate) 7156 VAI-JEAN AVE VAN NUYS CA 914064917 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described In Item 7 above) X POWERPLANT PROPELLER APPLIANCE Type ' Manufacturer 8. Conformity Statement A. Arilincy's IFR Avionics 7035 Sophia Van Nuys Name and Address B. Kind of Agency C. Corti icate No. Inc. Ave. CA 91406 . u.s. catenated Mechanic AtI4R059M Radio C1 1,2,3 LTD Instr. LTD Airframe. LTD Spec Service. Foreign Certificated Mechanic x Cerlificated Rena Station Manufacturer D. I certify thai the repair and/or alteration made to the un t(s) identified In item 4 above and describedon the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Data Signature Authorized Individual 7. Approval /— er lot u To Service Pu Administrator EST suanl to the of authority given persons specified below. the unit identified in item 4 was inspected in the manner prescribed by the the Federal Aviation Administration and is gl APPROVED 0 REJECTED FAA Flt. Standards Inspector - , Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval Or RejeCtion / 12512,90 I Certificate or Designation No. AO4R059/.1 Sign e of Authorized Individual l.., 8- FAA Form 337 met SDNY_GM_02753868 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240790 EFTA01326383 NOTICE Weight and balance or operating limitation changes shalt be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. a. Description of Work Accomplished (it more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) N677RP Removed eisting NZ-2000 Flight Management System (FMS) Navigational Computer Units (NCU), Part Number (7018879-01002), Serial Numbers (95120678, 95120716, & 95120669) from the aircraft. Sent NCU's to manufacturer for software upgrade from software 4.1 to software 5.2. In accordance with Gulfstream Aerospace Corporation (GAC), Aircraft Service Change (ASC) No. 349AM6. Received modified NCU's from the manufacturer new NCU Part Number is 7018879-03014. NCU's keep their original Serial Numbers. Reinstalled NCU's into the aircraft. Gulfstream Aerospace Corporation FAA Approved Airplane Flight Manual Supplement Number GIV-2000-03, dated July 25, 2000, in accordance with Gulfstream Aerospace Corporation ASC No. 349AM7, is required with this modification. The NZ-2000 system was operationally ground checked in accordance with ASC No. 349AM6. NZ-2000 system passed ground check. The Honeywell FMZ-2000 Pilot's Guide is Installed in the aircraft This modification does not effect the aircraft's eAsting Weight & Balance. No wiring changes were made to the aircraft. A log book entry has been made. An Equipment List Amendment has been provided. Work Order 37626 on file at this agency covers the work described above. END O Additional Sheets Are Attached *U.S. GOVIIRNMENT PRINTING OFFICE: 19112-761-012/50157 SDNY_GM_02753869 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240791 EFTA01326384 - 00 MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 tin Orporiment cr TramontalOn (envoi Aviation AdninistratiOn For FAA Use Only Office Idenfificat WP-23 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Gulfstream Aerospace Model G-IV Serial No. 1085 Nationality and Registration Mark N677RP 2. Owner Name (As shown on registration certificate) Petersen Aviation Address (As shown on registration certificate) 7155 Valjean Ave. Van Nuys, Ca. 91406-3917 3. For FAA Use Only The data identified herein complies with applicable airworthiness requirements and is approved only for the above described aircraft subject to a conformity Inspection by a person authorized In FAR 43.7 IBIC: 40-imiv- —20C4 -4 1".c.s. LAXIFSDO Dated 3-9-0/ 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in hem 1 above) XX POWERPLANT PROPELLER APPLIANCE Type Manufacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Garrett Aviation Services 6201 W Imperial Highway Los Angeles, Ca. 90045 U.S. Certificated Mechanic Foreign Certificated Mechanic AN3R377L X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and cored to the best of my knowledge. Date 03 -0 4 -0) Signst74,liveri er ourchro‘ e dist,h4e-- 7. Approval for Return to Service Pursuant Administrator BY to the authority given persons specified below, the unit ides Med In item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is X APPROVED 0 REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (S peci fV) FAA Designee X Repair Station Person Approved by Transport Canada Ainvorthiness Group Date of Approval or Rejection OZ — O4 -di Certificate or Designation No. AN3R377L Signatrely,erso, Aficatimi 4 it/Art.1,a", Form 337 (1243) SDNY_Gtv1_02753870 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00240792 EFTA01326385 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished Of more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished. Accomplished an upgrade to the previously installed #1 and #2 transponder systems. The #1 and #2 P/N 622-9210-003 transponders were removed and (2each) transponders that were modified by the equipment manufacture Rockwell/Collins to P/N 622-9210-006 status, in accordance with their service bulletins #13, #17 and #20 were installed. Accomplished an electrical wiring change to the #1 and #2 systems, in accordance with the equipment manufacture Rockwell/Collins Service Information Letter 1-96 dated 10-20-97. The electrical wiring changes mentioned above enables systems to have part number status interchangeability. Accomplished a complete ground operational check of systems and a electromagnetic interference verification with satisfactory results. Tested the #1 and #2 transponder systems for altitude integration, in accordance with FAR Part 43 appendix "E" para. ( c ). No change to weight and balance. END X Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769.012160157 SDNY_Glvl_02753871 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00240793 EFTA01326386 kg,' A7PrOvtd a COO Ito. 2120l0t0 Fee FAA Use a MAJOR Only mei REPAIR AND ALTERATION u S DcywUncal (Airframe, Powerplant, Propeller, or Appliance) of Tevoce.wica learnt Arbeee Admit:atriums Office Identifkadon VitI%-i ••"' 1C K 00 INSTRUCTIONS Print a type al entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision the rWt for instrucdons and disposition of thi form. This report is required by taw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such Notation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Model GULFSTREAM G-P/ Serial No. Nationality and Registration Mark 1085 N677RP 2. Owner Name (As shown on registration certificate) PETERSEN AVIATION Address (As shown on registration certificate) 7155 VALJEAN AVE VAN NUYS, CA 91406 - 3917 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above) • ********* •*****••• X Powerplant Propeller st m ei. tat 'MED fir / V ... i g .. Ill Appliance Tie Fitborhaz nos 6 FEB 0 9 V 2001 1 Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of YS FSDO C. Certificate No. WESTERN JET AVIATION,INC. 1750 HAYVENHURST AVE. VAN NUYS, CA 91406 U.S. trot echamc W1JR483Y Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowled e Date JANUARY 31, 2001 Signature Authorized Individual . 7. royal for Return to Service Pursuant to he authority given persons specified b low, uni ide tilled in item 4 was inspected in the rnanne prescribed by the Administrator of the Federal Aviation Administration and is la APPROVED O REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection JANUARY 31, 2001 Certificate or Designation No. W1JR483Y Signature of Authorized Individnal C D —O41 FAA Form 337 0 1-95) SDNYGlvl02753872 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240794 EFTA01326387 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) PERFORMED THE FOLLOWING CUSTOMER BULLETINS AND AIRCRAFT SERVICE CHANGES: C/B 107 - FLAP "D" TRACT DOWN LOAD HOOKS - INSPECTION. C/B 108 - ACM BYPASS SHUTOFF VALVE - ACTIVATION WIRING - CHAFE PROTECTION. C/B 114 - NOSE LANDING GEAR ACTUATOR ROD END - LIFE LIMIT. C/B 116 - ELEVATOR BALLAST WEIGHT HELICOIL - INSTALLATION. CM 121 - AILERON BOOST BELLCRANK LUG THICKNESS TO LUG RADIUS RATIO - INSPECTION. CB 127 - HE ANTENNA ADAPTER - INSPECTION. C/B 128 - WIRE HARNESS AT F.S. 603 - INSPECTION. ASC 198 A1111 - ACM BYPASS SHUTOFF VALVE ACTIVATION WIRING CHAFE PROTECTION. ASC 403 - WINGLET ATTACHMENT HARDWARE REMOVAL / REPLACEMENT. ASC 414 - NOSE LANDING GEAR ACTUATOR ROD END SERIAL NUMBER. Changes to the Aircraft Weight and Balance has been Determined to be Negligible and Continues to Meet the Airworthiness Criteria Under Which it was Originally Certificated. END • :4r MI\ e I, • I. ' lit %:c!) O Additional Sheets Are Attached SDNY_GIvl_02753873 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240795 EFTA01326388 of 0 MAJOR REPAIR AND ALTERATION us cowmen, a Loatecornon (Airframe, Powerplant, Propeller, or Appliance) fe olAvicitlen Aorilni er sffetion Form Approved OMB NO. 2120-0020 For FAA Use Only Office Identification alfie - - /0/ - - --, ed>7 a INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequ nt revision thereof), or instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not toexceed51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM Model G4V Serial No. 1085 Nationality and Registration Mark N677RP 2. Owner Name (As shown on registration certificate) PETERSEN AVIATION Address (As shown on registration certificate) 7165 VALJEAN AVE VAN NUYS CA 914064917 3. For FAA Use Only The data identified herein described aircraft subject INSPECTOR WP-FSDO-1 complies with a li able al rthiness uirem and is to conformity' s ction n z FAR 43.7. Date:......7 approved only for above FAA Ofe2-li 4. Unit Wan IL Typo Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWER PLANT PROPELLER APPLIANCE Type Manufacturer • II Conformity Statement A. Agency's IFR Avionics 7035 Sophia Van Nuys Name and Address B. Kind of Agency C. Ceni icate No. Inc. Ave. CA 91406 • u.s. Certificated Mechanic AQ4Ft059M Radio Cl 1.2 3. LTD Instr. LTD Airframe. LTD Spec Service. Foreign Certificated Mechanic x Certificated Repair Station mannoovref D. I certify that the repair and/or alteration made to (neuritis) 'dentified In item4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date SI tura of Authorized ndlvid I ;--- 2 lf --- ?tat) 7. vat for Rate To Service Pu Administrator BY suant to the authority given persons specified . the unit identified in item 4 was inspected In the manner prescribed by the of the Federal Aviation Administration and is xl APPROVED 0 REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Parson Approved by Transport Canada Airworthiness Group Dale of Approval or Rejection ._... --- 2 4 - .),,,,,,o Certificate or Designation No. AO4ROSSM Sigi lure of Authorized individu FAA Form 337 02 eel SDNY_GIvl_02753874 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240796 EFTA01326389 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. IL Description of Work Accomplished of more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) N677RP Removed existing lea. Panasonic PV-4662 VCR, and 2ea. Baker Electronics SB1410AAB 14-LCD Monitors. Installed two each Samsung Electronics Co. 170MP, 1T' LCD Monitor In accordance with manufacturers Owner's Instructions P/N BN68-00108E-01 dated 1999. Installed a RCA Corp. PROSCAN Model PS8680Z Digital Video Disk Player in accordance with manufacturers Users Manual Manual No. TOCOM 15346010 dated 1998. The LCD monitors are located at arm 151.0, & 443.0, and the DVD is located at arm 145.0. Installation details are in compliance with AC 43.13-1B chapters 11, and 12, AC 43.13-2A Chapter 2, and AC 25-10. Post installation ground test were performed in accordance with Manufacturer's installation manual's, and AC 25-10. All systems operated normally. The above equipment was mounted by Synchro Aircraft Interiors. Van Nuys, Ca. and was structurally approved under FM Form 337, dated May 24, 2000. The above equipment is interfaced to the aircraft's existing cabin entertainment, audio/video switching system. For Continued Airworthiness Instructions for the LCD Monitor see IFR Avionics Inc. Document No. ICAW-170MP, REV. N/C, dated May 23, 2000, for the DVD see IFR Avionics Inc. Document No. ICAW-PS8680Z, REV. N/C, dated March 16, 1999. Revised Weight & Balance performed by Synchro Aircraft Interiors. Van Nuys, Ca. A log book entry has been made. Wiring Diagrams, and Equipment List Amendment have been provided. Work Order 37230 on file at this agency covers the work described above. END ill Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: I102-765-012/601$7 SDNY_GM_02753875 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240797 EFTA01326390 Wt. IFR Avionics, Inc. 1035 Sophia Ave. Van Nuys Ca. 91406 Document No. ICAW-170MP Dated: May 23, 2000 REV. N/C Instructions For Continued Airworthiness For a Samsung Electronics Co. 170MP 17" LCD Monitor This alteration to this aircraft obligates the aircraft operator to include the following maintenance information provided by this document in the owner/operator's Aircraft Maintenance Manual and the owner/operator's Aircraft Scheduled Maintenance Program. The Samsung Electronics Co. Line Replaceable Unit (LRU) maintenance is on condition and there Is no periodic, preventative or scheduled maintenance required for the continued operation of this unit. Should any failure of the Samsung Electronics Co. 17' LCD Monitor system occur, it should be properly noted, and the unit should be removed from the aircraft. Once a failure has occurred, it is advisable to do a visual inspection of the 17" LCD Monitor system. This inspection should include, but is not limited to the 17' LCD Monitor mounting, associated wiring, and any related hardware. This inspection should be performed through elementary means. 1. Maintenance, repaired, reinstall, and testing information for the 17' LCD Monitor system in this aircraft are contained in the Samsung Electronics Co. Owners Instructions (P/N EIN68-00108E-01 dated 1999, or later). 2. The Line Replaceable Unit (LRU) part numbers and other necessary part numbers contained in the installation data documentation for this modification should be placed into the aircraft's owner/operators appropriate Illustrated Parts Catalog (IPC). 3. Wiring diagram information contained in the installation data documentation for this modification should be placed into the aircraft owner/operators appropriate airplane Wiring Diagram Manual. 4. The scheduled Maintenance tasks required by this modification are to added to the aircraft owner/operators appropriate airplane maintenance program are as follows: Perform on at least an annual basis a periodic inspection of the equipment rack, equipment mountings, associated wiring, cables, connectors, hardware, and related aircraft structure for integrity, security, wear, chaffing, and etc. Special attention should be given to the aircraft primary structure with regards to fatigue and stress cracking, corrosion, and etc. NOTE: These inspections may appear as part of opportunity inspections or recommended Zonal inspection tasks. 5. Should it become necessary to remove the 17" LCD Monitor, secure the associated cables and wiring, collar the applicable circuit breakers, placard the aircraft that the unit has been removed, revise the weight & balance and the equipment list and make a logbook entry the unit has been removed for service refer to section 91.213 of Title 14 of the Code of Federal Regulations and/or the aircraft's MEL). 6. The 20" LCD Monitor and its related primary components can only be repaired at a factory authorized repair center or an appropriately rated F.AA. Part 145 repair station. NOTE: Should structural repairs be necessary to the airframe they should be performed in accordance with F.A.A. approved data, the Structural Repair Manual from the Airframe manufacturer (SRM) or guidance contained In Advisory Circular (AC) 43.13-1A, if applicable. 7. For additional Information regarding this modification and the related equipment refer to the following documents: a. Samsung Electronics Co. 17* LCD Owner's Instructions (P/N BN68:00108E-01 dated 1999, or later). Page 1 of 1 SDNY_GM_02753876 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 r EFTA_00240798 EFTA01326391 SDNY_GM_02753877 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240799 EFTA01326392 IFR Avionics, Inc. 7035 Sophia Ave. Van Nuys Ca. 91406 Document No. ICAW-PS8680Z Dated: March 16, 1999 REV N/C Instructions For Continued Airworthiness For a ProScan PS8680Z Digital Video Disk (DVD) Player This alteration to this aircraft obligates the aircraft operator to include the following maintenance information provided by this document in the owner/operators Aircraft Maintenance Manual and the owner/operators Aircraft Scheduled Maintenance Program. The ProScan Line Replaceable Unit (LRU) maintenance is on condition and there is no periodic, preventative or scheduled maintenance required for the continued operation of this unit. Should any failure of the ProScan PS8680Z DVD, it should be properly noted, and the unit should be removed from the aircraft. Once a failure has occurred, it is advisable to do a visual inspection of the DVD system. This inspection should include, but is not limited to the DVD mounting, associated wiring, and any related hardware. This inspection should be performed through elementary means. 1. Maintenance, repaired, reinstall, and testing information for the DVD system in this aircraft are contained in the ProScan User's Manual (Manual No. TOCOM 15346010). 2. The Line Replaceable Unit (LRU) part numbers and other necessary part numbers contained in the installation data documentation for this modification should be placed into the aircraft's owner/operators appropriate Illustrated Parts Catalog (IPC). 3. Wiring diagram information contained in the installation data documentation for this modification should be placed into the aircraft owner/operators appropriate airplane Wiring Diagram Manual. The scheduled Maintenance tasks required by this modification are to added to the aircraft owner/operators appropriate airplane maintenance program are as follows: Perform on at least an annual basis a periodic inspection of the equipment mountings, associated wiring, cables, connectors, hardware, and related aircraft structure for integrity, security, wear, chaffing, and etc. Special attention should be given to the aircraft primary structure with regards to fatigue and stress cracking, corrosion, and etc. NOTE: These inspections may appear as part of opportunity inspections or recommended Zonal inspection tasks. 5. Should it become necessary to remove the DVD secure the associated cables and wiring, collar the applicable circuit breakers, placard the aircraft that the unit has been removed, revise the weight & balance and the equipment list and make a logbook entry the unit has been removed for service refer to section 91.213 of Title 14 of the Code of Federal Regulations and/or the aircraft's MEL). 6. The DVD and its related primary components can only be repaired at a factory authorized repair center or an appropriately rated F.A.A. Part 145 repair station. NOTE: Should structural repairs be necessary to the airframe they should be performed in accordance with F.A.A. approved data, the Structural Repair Manual from the Airframe manufacturer (SRM) or guidance contained in Advisory Circular (AC) 43.13-1A, if applicable. 7. For additional information regarding this modification and the related equipment refer to the following documents: a. ProScan Users Manual (Manual No. TOCOM 15346010). Page 1 of 1 SDNY_GM_02753878 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240800 EFTA01326393 SDNY_GM_02753879 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240801 EFTA01326394 G-1-00 Mt 14.8.240ma--- f i 4 /R. di MAJOR REPAIR AND ALTERATION U.S. Depeetneet plTheuppeteme (Airframe, Powerplant, Propeller, or Appliance) ham Awaon AdmInIstrollea / 517 --/Z 5 ?OO 0 a( 557 Form Approved OMB No.2120-0020 For FAA Use Only Office Identification Go Po I INSTRUCTIONS: Print or type al entries. See FAR 43.9, FAR 43 Append( B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Aircraft Stelae GULFSTREAM motet GIV Sens] It 1085 NolimarY end Rightists, Mork N677RP 2 Owner Marne (As shoat ea segIstntlan anthem.* PETERSEN AVIATION Address (As shawl on registration certificate) 7155 VAUEAN AVE. VAN NUYS. CA. 91406-3917 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Mention AIRFRAME described In Item I above) X (As POWERPLANT PROPELLER APPLIANCE Type Manteactser 6. Co formity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. RICHARD P. JOSEPH JR. 3456 GARNET ST. APT. 0338 TORRANCE. CA. 90503 0 U.S. CerlAcated MochaPp MP 245198915 0 Foreign Oct-Seated iischaric 0 CestAxalecl Repair Swan 0 manuracturer D. I certify that the repair and/or alteration made to the unifts Identified in kern 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is bye and correct to the best of my knowledge. Date 6.2q . co Signature of Authorized Indvidted--- n -----' 2 7. Approval for Return To Service `------t----- Pursuant to the authcrey given persons specified below, the u rt identified In kem 4 was inspected in the manner presented by the Administrator of the Federal Aviation Administration and is ] APPROVED 12I REJECTED BY 0 FAAFtaavixds 0 Manufacturer 0 Inspection Authorization Other (S y) 0 FAA Designee 0 Repair Station n LI PersonaPaca:ObiTfbraPad Canada Alnvorthiress Group Date of oprwal or Rejection b M oo Certificate 6 356 or Designation No. 14 .225" of Inefrvidual IC(ALacrIA,N FAA Form 337 (12.88) SDNYGlvl_02753880 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240802 EFTA01326395 NOTICE Weight end balance or operating limitation changes shall bo entered in the appropriate eitcraftnscord. An alteration muslin) " compatible with all previous operations to assure continued conformity with the applicable einvorthiness requirements. 8. Description of Work Accomplished (II more space is required, attach additional shoe& Identifywith aircraft naffonatily and togistration mark and data work completed.) 1.) FIREBLOCKING: REMOVED ALL SINGLE SEATS, DOUBLE SEATS, ATHREE PLACE DIVAN, AND JUMPSEAT. ALL SEATS WERE REUPHOLSTERED AS FOLLOWS: SKANDIA, INC. DAX GRAPHITE/POLY 2611.0 FOR ALL SEATS MENTIONED EDELMAN LEATHER -ROYAL HIDE P/N RH323 CUSTOM LT GRAY DYE LOT AFLOO FOR (6) SINGLE SEATS GARRETT LEATHER C-616 CHATHAM SEAFOG DYELOT 67296 FOR RI EACH DOUBLE SEATS ICF/UNIKAVAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY TREATED AT SYNCRO REF. JOB 034)32FOR THREE PLACE DIVAN VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCX TREATED AT SYNCRO REF. LB 00032 SKANDIA INC. NOMEX BATTING USED ON ALL ABOVE SEATS MENTIONED. ALL MATERIALS MENTIONED ABOVE MEET FLAMMABIUTY &FIREBLOCKING REQUIREMENTS PER FAR 25.853 (CI APPENDIX F PART II AMENDMENT 2583. REFERENCE SKANDIA, INC. TEST PLAN 15823 REV. IR. APPROVED BY JUDY BOGGS DERV-406020CE ON 5/19/00. 2.1 FLAMMABILITY: REMOVED DECOR PANELS AND STRIPPED OFF EXISITNG FABRIC. RECOVERED WITH A BER GAM° FABRIC P/N 1797/1 LAV1NA. LAV AFT BULKHEAD AND DOOR WERE REMOVED AND STRIPPED OF EXISITNG COVERING. RECOVERED WITH A KNOLL TEXTILES FABRIC P/N K183-1 BUM! PEARL. ALL MATERIALS MENTIONED ABOVE MEET FLAMMABILITY REQUIREMENTS PER FAR 25.853 (o) APPENDIX F PART I (el (1) G). REFERENCE SKANDIA, INC. TESTPLAN 85902 &81103 APPROVED BY JUDY BOGGS DERV-4050204CE ON 4/25/00. INSTALLED NEW 10016WOOL CARPET THROUGHOUT AIRCRAFT, CARPET MATERIAL MEETS FLAMMABILITY REQUIREMENTS PER FAR 25.853(A). REFERENCE 81103 PROVIDED BY SCOTT GROUP. 3.1 THE EXISTING THREE PLACE DIVAN IS MODIFIED BY MOVING THE EXISTING CENTER TRUSS STRUCTURE AFT BY 4.75 INCHES AND THE FWD TRUSS STRUCTURE FWD BY 4 INCHES FOR THE PURPOSE OF FITTING UFE RAFTS UNDERNEATH. WORK WAS PERFORMED BY DYNAMO AVIATION PER SYNCRO WORK OR DE R .THE ABOVE MENTIONED MODIFICATION IS APPROVED BY HOWARD L PATTERSON DERT405434MM, PER AN 8110-3 DATED 5/8/00. REFERENCE STRUCTURAL SUBSTANTIATION REPORT DA41085 REV. "NC* DATED 5/8/03 PREPARED BY SHANAZ GALANTE. 4J ONE PANASONIC VCR MODEL PV4682 WAS EXCHANGED WITH DVO PLAYER MODEL PS88802. REMOVED E)GSITNG RACK FROM L/H FWD COMPARTMENT. MODIFIED TO INCORPORATE NEW DVD PLAYER. REMOVED TWO 14' LCD MONITORS FROM STA 193B &STA441 INSTALLED TWO 17" LCD MONITORS MODEL 8170MP. ONE IS MOUNTED ONTO THE AFT BULKHEAD ON THE FWD R/H EXISITNG STORAGE CABINET LOCATED AT STA 193 AND THE SECOND ONE IS MOUNTED ONTO THE FWD SIDE OF THE AFT L/H BULKHEAD LOCATED AT STA 442. • ALL THE ABOVE MODIFICATIONS ARE APPROVED BY HOWARD L. PATTERSON DERT-535434-NM. REFERENCE 81103 APPROVED ON 5/15/00. REPORT DOCUMENT SY.GLIOSSR EV. PREPARED BY SHANAZ GALANTE. THE ABOVE EQUIPMENT WAS ELECTRICALLY INSTALLED BY IFR AVIONICS, VAN NUYS, CA. SEE FAA FORM 337, DATED ON MAY 242000 FOR DETAILS. 5.) WEIGHT &BALANCE WAS RECALULATED. REFERENCE WEIGHT &BALANCE REPORT DATED 5/23/01 El Add Tonal Sheets Are Attached FAA Form 337 (1248) U.S. GPO:19893-663-171 SDNY_GIvI_02753881 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240803 EFTA01326396 r • Interior Alteration Report Gulfstream GIV N677RP S/N 1085 Syncro Aircraft Interiors, Inc. Van Nuys, Ca. 91406 May 24,2000 Table Of Contents 4— Opposite Page - FAA form 337 1. Compliance with FAR 25.853 (c) for fireblocking of all passenger seats. Skandia, Inc. Test plan #5823 2. Proof of compliance per FAR 25.853 (a) for materials used on: a.) Decor Panel Fabric b.) Lay aft bulkhead c.) Carpet 3. Divan modification 8110-3 and report 4. Structural Substantiation 8110-3 and report 5. Weight & balance report (original inserted into weight & balance book) SDNY_GIvl02753882 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240804 EFTA01326397 SDNYGM02753883 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240805 EFTA01326398 • - U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION - STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DAM 05/19/00 AIK4K/U-I UK AIMUKAI-I IVJPIIMINtN I IULN I I FICA I IUN MAKE OULFSTPEAM SIN 1085 MODEL NO. ON TYPE (Airplane. Ratio. Helicopter Me.) Aiwhat NAME OF APPLICANT Stadia, Ine. SYNCEDAIRCRAFT INTERIORS WI VI- UA IA IDENTIFICAI ION NILE Work Order 0 45812-00 Test ID 23626 ' FIREBLOCKING FLAMMABILITY TEST RESULTS REF: Skandia, Inc. Test Plan # 5823 Rev IR Dated: 05/12/00 For PN's 5823-1, 5823-2, 5823-3, 58234 5823-5 & 58234 SKANDIA, INC. DAX GRAPHITE/POLY 26 MD EDELISI LEATHER ROYAL HIDE RH323 CUSTOM LT. GRAY DYE LOT AFI.00 . GARP,EIT LEATHER C-616 CHATHAM SEAFOG DYE LOT 67296 ICF/UNIICA VAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY ' TREATED AT SYNCRO REF. JOB 00-032 VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 SKANDIA, INC. NOMEX BATTING • ......-- PURPOSE OF DMA DEMONSTRATION OF COMPLIANCE WITH MATERIAL FLAMMABILITY REQUIREMENTS APPLICABLE REQUIREMENTS (list specific sections) FAR 25.853 (c) Appendix F Part)] Amendment 25-83 FAR 25.853 (a) Appendix F Part I (a) (1) (ii) CERTIFICATION -Under authority of appointment under Part 183 of have vested by direction of the Administrator and in accordance with conditions the Federal Aviation Regulations, data listed above and on attached shorts been examined in accordance with established procedures and found to comply Regulations. approval of these data these data and limitations numbered with applicable requirements of the Federal Aviation ecommend I (We) Therefore Approve ,. TURE(S) _ OF D NATED ENGINEERING REPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) A-El 1 DERY-405020-CE Structural Special Judy oggs FAA Form 81104 (11-70) SUPERSEDES PREVIOUS EDITION SDNYGIvl_02753884 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240806 EFTA01326399 SDNY_GM_02753885 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240807 EFTA01326400 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 SYNCRO AIRCRAFT INTERIORS, INC. TEST PLAN #5823 REV IR SKANDIA WO #45812-00 GULFSTREAM GIV S/N 1085 DEMONSTRATION OF COMPLIANCE OF AIRCRAFT SEAT CUSHION ASSEMBLIES TO THE FIREBLOCKING REQUIREMENTS OF FAR 25.853 (C) AMENDMENT 25-83 DATE: REVISION NO. EFFECTIVE PAGE DESCRIPTION 5-12-00 IR PREPARED BY: DATE: S - 7- 7-CD° CHECKED BY: DICK DATE: 570 8/0 LAUGHLIN APPROVED DATE: 5 --i -OD PAGE: 1 SDNYGlvl02753886 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240808 EFTA01326401 • 0 SDNY_GM_02753887 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240809 EFTA01326402 • SKAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN 5823 REV IR INDEX OF PAGES REVISION PAGE 1 INDEX OF PAGES 2 MATERIAL LIST 3 TEST SPECIMEN PROCEDURES 4 PRODUCTION PROCEDURES 5 TEST DRAWING (P/N 5823-1 & 5823-2) 6 TEST DRAWING (P/N 5823-3 & 5823-4) 7 TEST DRAWING (P/N 5823-5 & 5823-6) 8 PRODUCTION DRAWINGS 9-11 FIREBLOCKING FLAMMABILITY TEST RESULTS 12-14 WEIGHT LOSS STRIP CHART 15-17 DAILY CALIBRATION CHART 18 VERTICAL FLAMMABILITY TEST RESULTS 19-27 TRACEABILITY DOCUMENTS 28-40 PAGE: 2 SDNYG1.1_0275388.13 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002408 10 EFTA01326403 SDNYGM02753889 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240811 EFTA01326404 • SKANDIA, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN 5823 REV IR MATERIAL LIST DRESS COVER: EDELMAN LEATHER ROYAL HIDE RH323 CUSTOM LT. GRAY DYE LOT AFL00 DRESS COVER: GARRETT LEATHER C-616 CHATHAM SEAFOG DYE LOT 67296 DRESS COVER: ICF/UNIKA VAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY TREATED AT SYNCRO REF. JOB 00-032 BATTING: SKANDIA, INC. NOMEX BATTING CANVAS: VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 ADHESIVE: CORAL ADHESIVES CC1025 ADHESIVE FOAM: SKANDIA, INC. DAX GRAPHITE/POLY 26 ILD, 47 ILD & 55 ILD VELCRO: SKANDIA, INC. PBLK1.00L & PBLK1.00H 1' LOOP AND HOOK BLACK PAGE: 3 SDNYGlvl_02753890 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240812 EFTA01326405 SDNY_GM_02753891 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002408 I 3 EFTA01326406 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN #5823 REV IR TEST CUSHIONS: TEST NO. 1 P/N 5823-1 & 5823-2 Test cushion dress covers are fabricated using 50% Edelman Leather Royal Hide RH323 Custom Lt. Gray Dye Lot AFL00 and 50% Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032. Test cushions are fabricated with Skandia, Inc. DAX Graphite/Poly 26 ILD which qualifies the same foam of a higher density. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, test cushions have a layer of Skandia Nomex Batting placed between the dress cover and the foam on the seating surfaces only. Test cushion dresscovers wrap over and around foam with the leather velcroing to leather and canvas velcroing to canvas in a window pane fashion. TEST NO. 2 P/N 5823-3 & 5823-4 Test cushion dress covers are fabricated using 50% Garrett Leather C-616 Chatham Seafog Dye Lot 67296 and 50% Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00- 032. Test cushions are fabricated with Skandia, Inc. DAX Graphite/Poly 26 ILD which qualities the same foam of a higher density. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, test cushions have a layer of Skandia Nomex Batting placed between the dress cover and the foam on the seating surfaces only. Test cushion dresscovers wrap over and around foam with the leather velcroing to leather and canvas velcroing to canvas in a window pane fashion. TEST NO. 3 P/N 5823-5 & 5823-6 Test cushion dress covers are fabricated using 50% ICF/Unika Vaev Fabric 917 Color 81 Cranbrook Cranbrook Grey treated at Syncro ref. job 00-032 and 50% Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032. Test cushions are fabricated with Skandia, Inc. DAX Graphite/Poly 26 ILD which qualifies the same foam of a higher density. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, test cushions have a layer of Skandia Nomex Batting placed between the dress cover and the foam on the seating surfaces only. Test cushion dresscovers wrap over and around foam with the fabric velcroing to fabric and canvas velcroing to canvas in a window pane fashion. PAGE 4 SDNYGlvl_02753892 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240314 EFTA01326407 • • SDNY_GM_02753893 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002408 15 EFTA01326408 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN #5823 REV IR PRODUCTION CUSHIONS 6 PAX SEATS Production cushion dress covers-are fabricated using Edelman Leather Royal Hide RH323 Custom Lt. Gray Dye Lot AFL00. Production cushions are fabricated using a combination of different densities of Skandia, Inc. DAX Graphite/Poly with 26 ILD being the lowest density used. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, production cushions have a layer of Skandia Nomex Batting placed between the dress cover and foam on seating surfaces only. There is a layer of Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032 bonded to the back side of the back and bottom side of the bottom utilized as a close out fabric. Production cushion dresscovers wrap over and around foam with the dresscover velcroing to the canvas in a window pane fashion. 2 DOUBLE PAX SEATS AND JUMPSEAT Production cushion dress covers are fabricated using Garrett Leather C-616 Chatham Seafog Dye Lot 67296. Production cushions are fabricated using a combination of different densities of Skandia, Inc. DAX GraphiteJPoly with 26 ILD being the lowest density used. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, production cushions have a layer of Skandia Nomex Batting placed between the dress cover and foam on seating surfaces only. There is a layer of Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032 bonded to the back side of the back and bottom side of the bottom utilized as a close out fabric. Production cushion dresscovers wrap over and around foam with the dresscover velcroing to the canvas in a window pane fashion. DIVAN Production cushion dress covers are fabricated using ICF/Unika Vaev Fabric 917 Color 81 Cranbrook Cranbrook Grey treated at Syncro ref. job 00-032. Production cushions are fabricated using a combination of different densities of Skandia, Inc. DAX Graphite/Poly with 26 ILD being the lowest density used. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, production cushions have a layer of Skandia Nomex Batting placed between the dress cover and foam on seating surfaces only. There is a layer of Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032 bonded to the back side of the back and bottom side of the bottom utilized as a close out fabric. Production cushion dresscovers wrap over and around foam with the dresscover velcroing to the canvas in a window pane fashion. PAGE 5 SDNYGIvl_02753894 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002408 16 EFTA01326409 • SDNY_GM_02753895 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240817 EFTA01326410 • *SIGN APPROVAL REQUESS FAR 25.853 (c) APPENDIX F PART II TEST SPECIMEN DRAWING NO: 5823 WO# 45812-00 REV IR DATED: 05-12-0Q MAKE: GULFSTREAM MODEL: G1V SIN: 1085 SEAT DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION F CONFORMITY INSP APPROVED TEST PROCEDURES END VIEW BACK CUSHION WITHOUT' DRESS COVER c END VIEW BOTTOM CUSHION WITHOUT DRESS COVER FOR TESTING IN ACCOR AU. TOLERANCES ! .125 SEAT BACK PIN 5823-1 SEAT BOTTOM P/N 5823-2 COMPOSITOR MANUFACTURER PART NUMBER . -. . COLOR DYE LOT FLAME TREATMENT A DRESS COVER LEATHER 50% EDELMAN LEATHER ROYAL HIDE RH223 CUSTOM LT GRAY AFUO B DRESS COVER CANVAS 50% VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK GREY • TREATED AT SYNCRO REF. JOB C0032 C BATTING SKANDIA, INC. NOMEX BATTING WHITE PLACED BETWEEN DRESS COVER AND FOAM ON SEATING SURFACES CI FOAM .75 ' SKANDIA, INC. DAX GRAPIETEROLY 26 MD MAUVE ' E FOAM I.75 SKANDIA, INC. DAX GRAPHITE/POLY 26 ILD MAUVE F VELCRO V SKANDIA, INC. ' PBLKI.ODL LOOP PBLKI.OOH HOOK BLACK ALL CUSHION ASSEMBLY COMPONENTS ARE BONDED WITH CORAL ADHESIVES CCI025 ADHESIVE eather ve woes to leather and canvas ve croes to canvas. Materials on backs and bottoms are identical PAGE 6 SDNYGIvl_02753896 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024081S EFTA01326411 SDNYGM02753897 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240819 EFTA01326412 *SIGN APPROVAL REQUEST. FAR 25.853 (c) APPENDIX F PART II TEST SPECIMEN DRAWING NO: 5823 WO# 45812-00 REV IR DATED: 05-12-00 MAKE: GULFSTREAM MODEL: GIV SRN:: 1085 SEAT DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION OF CONFORMITY INSPECTOR TEST SPECIMENS TO BE SUBMITTED FOR TESTING IN ACCORDANCE WITH FAA APPROVED TEST PROCEDURES ALL TOLERANCES • .12T END VIEW BACK CUSHION SEAT BACK P/N 5823-3 WITH0UT' DRESS COVER D E F END VIEW BOTTOM CUSHION WITHOUT DRESS COVER SEAT BOTTOM P/N 5823-4 COMPOSITOR MANUFACTURER PART NUMBER COLOR DYE LOT FLAME TREATMENT A DRESS COVER LEATHER 50% GARRETT LEATHER CHATHAM . C-61 ft SEAFOG 57996 B DRESS COVER CANVAS 50% VAN NUYS AWNING CO. • ARABIAN COTTON ARMY DUCK GREY TREATED AT SYNCRO REF. JOB CO.= C BATTING SKANDIA, INC. NOMEX BATTING WHITE ' PLACED BETWEEN DRESS COVER AND FOAM ON SEATING SURFACES 0 FOAM .75 SKANDIA, INC. DAX GRAPHITEIPOLY 2BILD MAUVE E FOAM 1.75 SICANDIA, INC. DAX GRAPHITEJPOLY 2BILD MAUVE F VELCRO 1' SKANDIA, INC. PBLKI.CCL LOOP PBLK1.COH HOOK BLACK ALL CUSHION ASSEMBLY COMPONENTS ARE BONDED WITH CORAL ADHESIVES CC1025 ADHESIVE Leather velcroes to leather and canvas velcroes to canvas. Materials on backs and bottoms are identical. PAGE 7 SDNYGlvl_02753898 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240820 EFTA01326413 • SDNYGM02753899 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240821 EFTA01326414 •SIGN APPROVAL REQUES. FAR 25.853 (c) APPENDIX F PART II TEST SPECIMEN DRAWING NO: 5823 WO# 45012-00 REV IR DATED: 05.12-00 MAKE: GULFSTREAM MODEL: GIV Sift. 1085 SEAT DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION OF CONFORMITY INSPFCTIOWTEST SPECIMENS TO FORIESTING2LACCORDANCE WITH FM APPROVED TEST PROCEDURES ALL TOLERANCES ± .1r END VIEW BACK CUSHION WITHOUT DRESS COVER g- E ENO VIEW BOTTOM CUSHION WITHOUT DRESS COVER SEAT BACK P/N 5823-5 SEAT BOTTOM P/N 5823-8 COMPOSITOR MANUFACTURER • PART NUMBER COLOR DYE LOT FLAME TREATMENT A DRESS COVER FABRIC 9:396 ICPUNIKA VAEV 917 CRANBROOK CRANBROOK GREY 81 TREATED AT SYNCRO REF. JOB COCG2 B DRESS COVER CANVAS 50% VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK GREY TREATED AT SYNCRO REF. JOB CO032 C BATTING SKANDIA, INC. NOMEX BATTING WHITE PLACED BETWEEN DRESS COVER AND FOAM ON SEATING SURFACES D FOAM .75 SKANDIA, INC. DAX GRAPHITFJPOLY 2811.0 MAUVE E FOAM 1.75 SKANDIA, INC. DAX GRAPHITEIPOLY 28 ILD MAUVE F VELCRO 1' SKANDIA, INC. PBUL1.01 LOOP P8Ua.COH HOOK BLACK ALL CUSHION ASSEMBLY COMPONENTS ARE BONDED WITH CORAL. ADHESIVES CC1025 ADHESIVE Leather velcroes to leather and canvas velcroes to canvas. Materials on backs and ottoms are Identical. PAGE SDNYGI.1_02753900 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240822 EFTA01326415 • SDNYGM02753901 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240823 EFTA01326416 8 A r ' 0 ENO VIEW BA CK:AND BOTTOM CLISH/ON A. DRESS COVER: EDELMAN LEATHER ROYAL HIDE RH323 CUSTOM LT. GRAY DYE LOT AFLOO B. BATTING: A LAYER OF SKANDIA, INC. NOMEX BATTING PLACED BETWEEN DRESSCOVER AND FOAM ON SEATING SURFACES ONLY C. FOAM CONSTRUCTION: A COMBINATION OF DIFFERENT DENSITIES OF SKANDIA DAX GRAPHITE/POLY WITH 26 ILO BEING THE LOWEST DENSITY USED D. CLOSE OUT FABRIC: VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 BONDED TO THE BACK SIDE OF THE BACK AND BOTTOM SIDE OF THE BOTTOM CUSHION E. VELCRO: SKANDIA, INC. PBLK1.00L & PBLK1.00H 1- LOOP AND HOOK PRODUCTION CUSHIONS TYPICAL 6 PAX SEATS TEST PLAN 5823 WO# 45812-00 REV IR DATE: 05-12-00 GULFSTREAM GIV S/N 1085 ALL COMPONENTS BONDED WITH CORAL ADHESIVES CC1025 ADHESIVE THE BURN TEST REQUIREMENT FOR THIS PRODUCTION ARTICLE IS MET BY TEST SPECIMENS 5823-1 & 5823-2 ' PAGE 9 SDNYGIvl02753902 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240824 EFTA01326417 • r = lk. SDNY_GM_02753903 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240825 EFTA01326418 • e A r D I BOT TO ENO VIEW BACK:AND M CUSHION A. DRESS COVER: GARRETT LEATHER C-616 CHATHAM SEAFOG DYE LOT 67296 B. BATTING: A LAYER OF SKANDIA, INC. NOMEX BATTING PLACED BETWEEN DRESSCOVER AND FOAM ON SEATING SURFACES ONLY C. FOAM CONSTRUCTION: A COMBINATION OF DIFFERENT DENSITIES OF SKANDIA DAX GRAPHITE/POLY WITH 26 ILD BEING THE LOWEST DENSITY USED D. CLOSE OUT FABRIC: VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 BONDED TO THE BACK SIDE OF THE BACK AND BOTTOM SIDE OF THE BOTTOM CUSHION E. VELCRO: SKANDIA, INC. PBLK1.00L & PBLK1.00H 1' LOOP AND HOOK ALL COMPONENTS BONDED WITH CORAL ADHESIVES CC1025 ADHESIVE PRODUCTION CUSHIONS TYPICAL 2 DOUBLE PAX SEATS & JUMPSEAT TEST PLAN 5823 WO# 45812-00 REV IR DATE: 05-12-00 GULFSTREAM GIV S/N 1085 THE BURN TEST REQUIREMENT FOR THIS PRODUCTION ARTICLE IS MET BY TEST SPECIMENS 5823-3 & 5823-2 PAGE 10 SDNYGIv1_02753904 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240826 EFTA01326419 SDNY_GM_02753905 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240827 EFTA01326420 SOTTEO/4 ND VIEW BACA-- CUSH' -.AND A. DRESS COVER: ICF/UNIKA VAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY TREATED AT SYNCRO REF. JOB 00-032 B. BATTING: A LAYER OF SKANDIA, INC. NOMEX BATTING PLACED BETWEEN DRESSCOVER AND FOAM ON SEATING SURFACES ONLY C. FOAM CONSTRUCTION: A COMBINATION OF DIFFERENT DENSITIES OF SKANDIA DAX GRAPHITE/POLY WITH 26 ILD BEING THE LOWEST DENSITY USED D. CLOSE OUT FABRIC: VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 BONDED TO THE BACK SIDE OF THE BACK AND BOTTOM SIDE OF THE BOTTOM CUSHION E. VELCRO: SKANDIA, INC. PBLK1.00L & PBLKI.00H V LOOP AND HOOK PRODUCTION CUSHIONS TYPICAL DIVAN TEST PLAN 5823 WO# 45812-00 DATE: 05-12-00 REV IR ' GULFSTREAM GIV S/N 1085 ALL COMPONENTS BONDED WITH CORAL ADHESIVES CC1025 ADHESIVE THE BURN TEST REQUIREMENT FOR THIS PRODUCTION ARTICLE SPECIMENS 5823-5 & 5823-6 IS MET BY TEST PAGE II SDNYGlvl_02753906 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240828 EFTA01326421 SDNYGM02753907 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240829 EFTA01326422 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client : SYNCRO AIRCRAFT INTERIORS Date : 05/19/00 Client P.O. Aircraft: GULFSTREAM GIV Test Plan 11: 5823 Skandia WON: 45812-00 Rev: IR S/N: 1085 FIREBLOCKING FLAMMABILITY TEST RESULTS FAR 25.853 (c) Appendix F Part U Amendment 25-83 Conditioning Room: Time In :05/J7/00 Time Out: 05/19/00 Part Number Specimen Bum Length (Inches) VERT HORIZ-T HORIZ-B Weigh Loss (LBS.) cm Al 5823-1 LEATHER/CANVAS 9.0 5823-2 LEATHER/CANVAS 7.5 3.6 0.25 3.9 #2 5823-1 LEATHER/CANVAS 9.2 5823-2 LEATHER/CANVAS 7.7 4.2 0.26 4.2 #3 5823-1 LEATHER/CANVAS 9.2 5823-2 UMBER/CANVAS 7.2 3.8 0.25 3.9 AVERAGE: 9.1 7.5 3.9 0.25 4.0 Materials: Dress Cover 50% EDELMAN LEATHER ROYAL HIDE RII323 CUSTOM LT. GRAY DYE LOT AFL00 50% VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 Foam: SICANDIA, INC. DAX GRAPHITE/POLY 261W Other SICANDIA, INC. NOMEX BATTING Comments: FIREBLK3-6499 PAGE: 12 SDNYGIvl_02753908 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240830 EFTA01326423 • SDNY_GM_02753909 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024083 I EFTA01326424 • SKANDIA, Inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client : SYNCRO AIRCRAFT INTERIORS Date : 05/19/00 Client P.O. #: Aircraft: GULFSIREAM GIV Test Plan #: 5823 Skandia WO #: 45812-00 Rev: IR S/N: 1085 FIREBLOCKING FLAMMABILITY TEST RESULTS FAR 25.853 (c) Appirlix F Part II Amendment 25-83 Conditioning Room: Time In:05/17/00 Time Out: 05/19/00 Part Number Specimen Burn Length Race VERT HORIZ-T HORIZ-B Weigh Loss (LBS.) (%) in 5823-3 LEATHER/CANVAS 8.0 5823-4 LEATHER/CANVAS 7.4 2.6 0.26 4.4 #2 5823-3 LEATHER/CANVAS 8.2 58234 LEATHER/CANVAS 7.0 3.4 0.26 4.4 #3 5823-3 LEATHER/CANVAS 8.4 5823.4 LEATHER/CANVAS 7.5 3.7 0.28 4.7 AVERAGE: 8.2 7.3 3.2 0.27 4.5 Materials: Dress Cover 50% GARRETT LEATHER C-6I6 CHATHAM SEAFOG DYE LOT 67296 50% VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 SKANDIA, INC. DAX GRAPHtTE/POLY 26 ED SKANDIA, INC. NOMEX BATTING Foam: Other. Comments: FIREBLK3.6501 PAGE: 13 SDNYGIv102753910 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240832 EFTA01326425 • • SDNYGM02753911 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240833 EFTA01326426 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 Client : SYNCRO AIRCRAFT INTERIORS Date : 05/19/00 Client P.O. #: Aircraft: GULFSIREAM GIV Test Plan ft 5823 Slcandia WO #: 45812-00 Rev: IR S/N: 1085 FIBEILOCKING FLAMMABILITY TEST RESULTS FAR 25.853 (c) Appendix F Part II Amendment 25-83 Conditioning Room: Time In:05/9/00 Time Out: 05/19/00 Part Number Specimen Burn Length (Inches) VERT HORIZ-T HORIZ-B Weigh Loss (LBS.) (%) #1 5823-5 FABRIC/CANVAS 8.0 5823-6 FABRIC/CANVAS 7.8 3.4 0.26 4.1 #2 5823.5 FABRIC/CANVAS 7.7 5823-6 FABRIC/CANVAS 7.3 3.3 025 3.9 #3 5823-5 FABRIC/CANVAS 8.4 5823-6 FABRIC/CANVAS 8.0 3.7 0.28 4.3 AVERAGE: 8.0 7.7 3.5 0.26 4.1 Materials: Dress Cover: 50% ICF/UNIKA VAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY TREATED AT SYNCRO REF. JOB 00-032 50% VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 Foam: SICANDIA, INC. DAX GRAPIWIFJPOLY 26 ILD Other: SICANDIA, INC. NOMEX BATTING Comments: FIREBLIC3-6502 PAGE: 14 SDNYGIvl_02753912 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240834 EFTA01326427 • • SDNY_GM_02753913 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240835 EFTA01326428 *O.5 6.33 LB 6. 33 LB 6. 33 L 6. 22 LB 6. 11 LB 6. 10 LB 6.09 LB 6.09 LB 6.08 LB 6.08 LB￾MAY 19 2000 7 p - cif? .3 ..57? 3 - - BURN LENGTH VERT HORZ-T 7 T￾HORZ-B - Nit 1.60., • gialmemiggin • 6. 19 LB CURN LENGTH 6. 20 LB VERT 9. 6. 20 LB---HORZ-T 6. 06 LB HORZ B 5.98 LB WT.L0SS LBS. awe 5.96 LB WV % !omegas 5.95 LB 5.94 LB 5.94 LB , 5.94 6. 40 LB 6. 40 LB 6. 40 L 6. 25 LB 6. 18 LB 6. 17 LB' 6. 16 LB 6. 16 LB 6. 15 LB 6. 15 LB--- BURN LENGTh ERT -9 A HORZ-T HORZ B PAGE: 15 SDNY GM 02753914 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240536 EFTA01326429 • • SDNY_GM_02753915 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240837 EFTA01326430 6PA-401 MAY 19 2000 t p (.5--wp 3 Ay 5ra-3- 3 5. 95 LB 5.95 LB 5.95 LB 5.83 LB 5. 74 LB 5. 71 LB 5. 70 LB 5. 70 LB 5. 70 LB 5. 69 LB BURN LENGTH ERT HORZ-T HORZ-B WrLQ$$ LOS. WTian %nal iEro 5. 92 LB BURN LENGTH 5. 92 LB VERT - 55 55. 9078 2 LB LLF WTHu°1410SRZRZ:TBS 5- 68 LB Valigi--i6er"'"" 5.67 LB 5.67 LB 5.66 LB 5.66 LB---- 5. 92 LB BURN LENGTH 5.92 LB VERT = 5: .9782 = 5.69 LB nuns Las, = 5.67 LB ma 9601 se,sers. 5.66 LB 5.65 LB 5. 64 LB 5. 64 LB PAGE: 16 SDNYGIv1_02753916 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 1O, 15, and 17 EFTA 00240838 EFTA01326431 • • SDNYGM02753917 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240839 EFTA01326432 ri4 6 yer fp 6. 34 LB 6. 34 LB 6.34 L. 6.21 LB 6. 12 LB 6. 10 LB 6. 09 LB 6. 09 LB 6. 09 LB 6. 08 LBO MAY 19 2000 t)° ,5-ga 3 3-Se ,, CU RN LENGTH ERT HORZ-T 7 -cr HORZ B WT.Lpgg LBO.® IMT4wq ienws 6 47 LB CORN LENGTH 6.48 LB __VERT = . 6. 48 LB.' HORZT 6.. 236 LB wrJER1 HO - t88. 6. 25 LB wT lismsaimmes 6.24 LB 6.23 LB 6.. 23 LB---" 6. 47 LB r URN LENGTH 6. 47 LB VERT = Q ie 6. 47 HORZ-T V/7 6. 35 LB MORZ-B = 6.24 LB WT.LOSS LBO. 6. 21 LB Yin WM) cep 6. 20 LB 6. 20 LB 6. 19 LB 6. 19 LB, " PAGE: 17 SDNYGlvl02753918 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40840 EFTA01326433 SDNY_GM_02753919 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240841 EFTA01326434 SDNY_GI,1_02753920 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240842 EFTA01326435 SDNY_GM_02753921 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240843 EFTA01326436 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client WO #: 45812-00 SYNCRO AIRCRAFT INTERIORS Date: 04/24/00 7701 WOODLEY AVENUE Test Plan #: 5823 Rev:IR VAN N(JYS CA 91406 PO #: Aircraft: GULFSTREAM OW S/N: 1085 VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 04/21/09 Time Out: 04/24/00 Specimen EDELMAN LEATHER ROYAL HIDE RH323 CUSTOM LT. GRAY DYE LOT AFL00 Desc.: Flame Application (seconds) Flame Time (seconds) Burn Length (inches) Drippings (seconds) 12 0.0 0.3 0.0 12 9.2 0.3 0.0 12 10.3 0.3 0.0 Average: 6.5 0.3 0.0 Comments: Vertical (12 sec.) Bum Test: Average Self-Extinguish time may not exceed 15 sec. Average Bum Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Signed: /ERTI2NW-25381 Failed : PAGE: 19 SDNYGlvl02753922 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40844 EFTA01326437 • SDNYGM02753923 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240845 EFTA01326438 • SKAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: WO ft 45812-00 SYNCRO AIRCRAFT INTERIORS Date: 05/04/00 7701 WOODLEY AVENUE Test Plan #: 5823 VAN NUYS CA 91406 PO #: Aircraft: GULFSTREAM OW S/N: 1085 VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 05/02J$1 Time Out: 05/04/00 Specimen Dese.: GARRETT LEATHER C-616 CHATHAM SEAFOG DYE LOT 67296 Flame Application (seconds) Flame Time (seconds) Burn Length (melts) Drippings (seconds) 12 0.0 0.5 0.0 12 0.0 0.5 0.0 12 0.0 0.6 0.0 Average: 0.0 0.5 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. • Passed: Failed : Signed: PAGE: 20 ✓ERTI2NW-25382 SDNYGlvl_02753924 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240846 EFTA01326439 SDNY_GM_02753925 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240847 EFTA01326440 • SliAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: WO #: 45812-00 SYNCRO AIRCRAFT INTERIORS Date: 04/24/00 7701 WOODLEY AVENUE Test Plan #: 5823 Rev: IR VAN NUYS CA 91406 PO #: Aircraft: GULFSTREAM GIV S/N: 1085 VERTICAL FLAMMABif T triPcT RESULTS FAR 35.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Tithe In: 04/21/00 Time Out: 04/24/00 Specimen VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. Des° JOB 00-032 Flame Application (seconds) Flame Time (seconds) Bum Length (inches) Drippings (seconds) 12 Warp 0.0 Fill 0.0 Warp 2.7 Fill 2.0 Warp 0.0 Fill 0.0 12 0.0 4.7 2.4 4.5 0.0 0.0 12 0.0 13.2 2.6 7.1 0.0 0.0 Average: 0.0 6.0 2.6 4.5 0.0 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed:❑ Failed : Signed: ✓ERTI2-6308 PAGE: 21 SDNYGlvl_02753926 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240848 EFTA01326441 • • SDNYGM02753927 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240849 EFTA01326442 • SKAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: SYNCRO AIRCRAFT INTERIORS 7701 WOODLEY AVENUE VAN NUYS CA 91406 Aircraft: GULFSTREAM GIV WO #: 45812-00 Date: 03/23/00 Test Plan if: 5823 Rev: IR PO it: S/N: 1085 VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 03/22/00 1:30PM Time Out: 03/23/00 1:35PM Specimen ICF/UNIKA VAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY TREATED AT Desc.: SYNCRO REF. JOB 00-032 Flame Application (seconds) Flame Time (seconds) Burn Length (inches) Drippings (seconds) 12 Warp 0.0 Fill 0.0 Warp 1.3 Fill 2.6 Warp 0.0 Fill 0.0 12 0.0 0.0 2.0 1.4 0.0 0.0 12 0.0 0.0 1.9 1.6 0.0 0.0 Average: 0.0 0.0 1.7 1.9 0.0 0.0 Comments: Vertical (12 sec.) Burn Test Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: I ^j Failed : PAGE: 22 tERT12-6306 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SDNY15, 02753928 and 17 EFTA_00240850 EFTA01326443 • SDNY_GM_02753929 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024085 I EFTA01326444 • SKANDIA, inc. 5181 Falcon Road • Rockford. Illinois 61109 • Phone 815/227.1611 • Fax 815/227.1920 Client: WO #: 47120-00 SKANDIA (PRODUCTS) Date: 04/25/00 Test Plan #: PO #: Aircraft: STOCK Conditioning Room: Time In: Specimen SKANDIA, INC.: DAX GRAPHITE/POLY FOAM, 1/2", 26 ILD, LOT #03290 Desc.: S/N: NA VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) 04/24/00 11:50AM Time Out: 04/25/00 1:00 PM Flame Application (seconds) Flame Time (seconds) Bum Length (inches) Drippings (seconds) 12 0.0 2.8 0.0 12 0.0 2.9 0.0 12 0.0 2.8 0.0 Average: 0.0 2.8 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Signed: Litz L. Carin Demus VERTI2NW-24914 Failed : PAGE: 23 SDNYGlvl_02753930 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240852 EFTA01326445 SDNYGM02753931 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240853 EFTA01326446 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 Client: SKANDIA (PRODUCTS) Aircraft: STOCK WO #: 47120-00 Date: 04/25/00 Test Plan #: PO14: S/N: NA VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 04/24/00 II:50AM Time Out: 04/25/00 1:05PM Specimen Desc : SKANDIA, INC.: DAX GRAPHITE/POLY FOAM, UT, 26 MD, LOT #03310 Flame Application (seconds) Flame Time (seconds) Burn Length (inches) Drippings (seconds) 12 0.0 2.0 0.0 12 0.0 2.3 0.0 12 0.0 2.4 0.0 Average: 0.0 2.2 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Signed: E 7G• Carin Demus ERT12NW-24915 Failed : PAGE: 24 SDNY_Glvl_02753932 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240854 EFTA01326447 SDNY_GM_02753933 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240855 EFTA01326448 • SKAND1A, inc. 5181 Falcon Road • Rockford. 111inois 61109 • Phone 815/227-1611 Client: • Fax BIS/227-1920 WO #: SKANDIA (PRODUCTS) 44446-00 Date: 02/16/00 Test Plan #: PO #: Aircraft: STOCK S/N: NA VERTICAL_FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 02/15/00 3:15PM Time Out: 02/16/00 4:23PM Specimen SKANDIA, Desc.: INC.: NOMEX THERMAL BATTING, PART 135, LOT #02140 Flame Application (seconds) Flame Time (seconds) Bum Length (inches) Drippings (seconds) 12 12.0 2.3 0.0 12 5.3 1.4 0.0 12 0.0 0.9 Average: 0.0 . 5.8 1.5 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish Burn Length may not exceed 8". Average time may not exceed IS sec. Average Dripping may not exceed 5 sec. after falling. Passed: in Signed: A:t " / 4 9-nte•o-, Carin Demus zNW-23221 Failed : PAGE: 25 SDNYGlvi_02753934 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240856 EFTA01326449 SDNY_GM_02753935 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240857 EFTA01326450 Client: SKANDIA (PRODUCTS) Aircraft: STOCK • SKANDIA, Inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227.1920 WO 41724-99 Date: 12/02/99 Test Plan #: PO #: S/N: NA VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 12/01/99 9:30AM Time Out: 12/02/99 10:00 AM Specimen Desc.: SKANDIA, INC.: 1" BEIGE SEW HOOK FASTENER, SBGEI.00H, LOT #11299-lit Flame Application (seconds) Flame Time (seconds) Burn Length (inches) Drippings (seconds) 12 0.0 3.6 0.0 12 0.0 3.4 0.0 12 ' 0.0 3.2 0.0 Average: 0.0 3.4 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Signed: e.i Carin Demus VERT12N'W-21424 Failed : PAGE: 26 SDNY_Glvl_02753936 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240858 EFTA01326451 • w SDNYGM02753937 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240859 EFTA01326452 Client: SKANDIA (PRODUCTS) Aircraft: STOCK r SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 WO #: 40478-99 Date: 10/27/99 Test Plan #: PO #: S/N: NA VVERTICAL FLAMMABILITY TEST RESUt TS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 10/26/99 2:30 PM Time Out: 10/27/99 2:55PM Specimen Desc.: SKANDIA INC.: LOOP FASTENER, SBGEI.00L, SEW BEIGE I", RUN # 42112- Flame Application (seconds) Flame Time (seconds) Burn Length (inches) Drippings (seconds) 12 0.0 2.4 0.0 12 0.0 2.6 0.0 12 0.0 2.6 0.0 Average: 0.0 2.5 0.0 Comments: Burn Vertical Length (12 sec.) may Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: ri RT I 2NW -20642 Failed : ri PAGE: 27 SDNYGkl_02753938 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240860 EFTA01326453 r SDNY_GM_02753939 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240%61 EFTA01326454 0W02/280.ps-Cbcp:?.0 flncVclrPNL2V 8189885 • Teddy & Arthur Edelman, Limited EDELMAN 2:334263840;9/NCR° , 28 HawleyvIlle Road. P. O. Pox 110. Hawlei/villa, CT 06440-0110 Tel: (203) 426-3611. Fax: (203) 426-3840 Sold To: Cust No: 003549 SYNCRO AIRCRAFT INTERIORS VERONICA ALZAREZ 818 901-9828 7701 .WOODLEV AVENUE VAN NUYS, CA 91406 USA PAGE 84 PAGE:01 Order Nos 615346 Pick Date: 04/76/2000 Snipped To; ----- WINCRO AIRCRAFT INTERIORS 7701 WOODLEY AVENUE VAN NUYS, CA 91406 USA Cust. PO No. Order Date Shyer:. & SIsmn Delivery Terms itttrifireTter — oil/26/2000' — GPS7r KIET—":0 - —DAYS￾OtY-Ord OtY.Shp Item No. Description 606.25 Color Lot 0.00 RH323 ROYAL HIDE. Special instructions: JOB noo-b32-4.01 - 600 5/F 4.09 - 55 S/F RESHIPMENT TIE TO RMA 615344 CUSTOM LT GRAY AFLOO NO CLAIMS FOR NATURAL OR VISIBLE DEFECTS ARE TO BE ALLOWED UNLESS MADE WITHIN 5 DAYS AFTER RECEIPT OF GOODS BY SUTER. RESPONSIKLITY OF THE SELLER FOR (NATURAL DEFECTS WHICH MAY BE VISIBLE IN LEATHER OR FABRICS AS ORIGINALLY SHIPPED. CEASES AFTER SUCH LEATHER DR FABRIC HAS SEEN CUT OR FABRICATED PICKING TICKET - PAGE 1 COPT I PAGE: 28 SDNYGIvl_02753940 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240862 EFTA01326455 i SDNY_GM_02753941 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240863 EFTA01326456 05/09/2000 88:28 8189885251 GARRETT. L EAT H E R 1 Natural Selection. SYNCRO Garen locrhoc Cap:ma:en 1360 MOM Shoot DvDo13, NY 14213.1305 Toknonco.3 500442.7735 716.862.9301 Far 7164824358 Woo Site yomtgarettlealher.com PAGE 67 ACKNOWLEDGMENT (THIS IS NOT A BILL) 5 O SYNCRO AIRCRAFT INTERIORS H SYNCRO AIRCRAFT INTERIORS 0 ACCOUNTS PAYABLE P RECEIVING 7701 WOODLEY AVENUE 7701 WOODLEY AVENUE 0 VAN ,NUTS, CA 914.06 0 VAN NUYS, CA 91406 EDER DATE .)3/30/00 CUSTOMER P.O. 09691 SEP VIA PDX.,21 OVERNITE FOB. BUFFALO NY TERMS NET 15 DAYS MM VERONICA DUE DATE 04/03/00 LOCATION KENM SALES PERSON A T INTRS - TONI THOMAS <CA) currincanoN FAR 25.553 a/b tJANTITY ORDERED DESCRIPTOR Ea QUANTITY SHIPPED 490 I • FOR WAREHOUSE *EKED BY: C-618 Chatham ** CFA CERT .8110-3 GUI.FSTBAM SN 1085 N884CE ONLY Seafog APPROVED 3-30-00 Certificate: - G IV 67296 . • 9. I . 4/9(0, tio Cert - St , DATE 3bl/ 0D NECKED BY: I FOR SELECTING JARRETT LEATHER ORUENNO. !!! I 37210 on MARKED HIDES ARE NOT RETURNABLE PLEASE INSPECT CAREFULLY. SDNY_GM_02 753942 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240864 EFTA01326457 SDNY_GM_02753943 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240865 EFTA01326458 V.L43 - 9980tZ00 cn C co rn H 77 0 H rn < rn 0 0 rn JJ ,0 7D 0 77 .>"j CO c0 F" o2 Ic) W r (T, 0- F" ICE Ctevx:Ittlars4 W. Utio New lo( Comae Orrecond. VI! it Caine. NV tos64 re:14a 0 iCas :r:pee CPO Alt LS na Ens 006594 O SYNCRO AIRCRAFT INTERIORS INC. D 7701 WOODLEY AVE • VAN NUYS, CA 91406 0 L J PACKING LIST Locat S 0 01 ICE Taftville Warehouse ID REPRINT 1 018-901-9828 SYNCRO AIRCRAFT INTERIORS INC. 7701 WOODLEY AVENUE VAN NUYS, CA 91406 191902-00 OROER DATE "USTOMEsi PUN HASECK,ESNO. 3/09/00 ! 09567 PEDAL giSTRUCTIOVS ► BEND OT4ORDERED OTY.SAWED KMUSACKCJOBE0i UN BIN= I NEMNO. DESC.1e7MN 1 2 30.00 -0 J. j T 30.00 30.00 .00 YRD 11.78.7 ,220 , • GRANBROOlts CRANBROOZ JOB NO. ED0-032 V. 195 GREY 4.04 . DATE R*0 i PICKED DV PAM() CHECKED aY MAIRENOECTAD NO7E: 1HIS SHIPMEIC HAS BEEN CHECKED TWICE ANY DISCREPANCIES /MST BE REAMED IIAMEDLUELY. N0 CLAIM VALI/EA EMEDMIER5DAYS SHIP DATE 3/17/00 !UPS Second Day Air SHIPVA Y ea "0 3 in co tRIV7 GCE • —i tn) 3/10/00 5 8 EFTA01326459 SDNY_GM_02753945 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240867 EFTA01326460 PAGE 35 05/89/2000 10:33 8188885251 • SYNCRO • SDNYGlvl_02753946 This is to certify that the materials described below have been flame-retardant treated in order to meet the flammability requirements of FAR 25.853 (b) Amendment 25-32 by: The treatment process used is in accordance with Syncro Aircraft Interiors Process Specification PSOO1. THE FLAME RETARDANT PROCESS USED WILL BE REMOVED AFTER THREE WASHINGS. DRYCLEANING DOES NOT REMOVE RETARDANT. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240868 EFTA01326461 • • SDNY_GM_02753947 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240869 EFTA01326462 05/09/2000 10:33 , • • 818988525/ • SYNCRO • PAGE 05 ran Kilda AWNING CO, INC. SINCE 1ST B 5661 SEPULVEDA BLVD., VAN NUTS, CA. 91411 - PHONES: 752-5607 - FROM LA. 573-3331 COST. ORDER No. NAME tr • -7 • n--- DATE = r ADDRESS CA11,21O c •c, I C .-.14)4e4m, 5 SOW SY CAD( CAA. cuA dtmA moStAVD. pm cut. C0MINCTCA S CC • 2 7 7 0 0 2 QUANTITY • DESCRIPTION PRICE AMOUNT qiris • c,"O6.. AMOUNT '155. -c: TAX LABOR TOTAL 5 5'i DEPOSIT BALANCE DUE 555 77 AU. CLAIMS MID RETURNED GOODS MUST BE ACCOMPANIED BY THIS BILL 107290 RECD BY .1641C1C0.6••20.. 3I4 PAGE: 32 SDNYGlvl02753948 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40570 EFTA01326463 SDNY_GM_02753949 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024087 I EFTA01326464 PAGE 07 85/89/2000 10:33 8189885251 • SYNCRO • This is to certify that the materials described below have been flame-retardant treated in order to meet the flammability requirements of FAR 25.853 (b) Amendment 25-32 by: The treatment process used is in accordance with Syncro Aircraft Interiors Process Specification PS001. THE FLAME RETARDANT PROCESS USED WILL BE REMOVED AFTER THREE WASHINGS. DRYCLEANING DOES NOT REMOVE RETARDANT: SDNY_GM_02753950 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240572 EFTA01326465 SDNYGM02753951 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240873 EFTA01326466 05/09/2000 18:33 / / ..r" • N?. 1 9 6 1 8 Sold To Shipped To 8199885251 SYNCRO CORAL INDUSTRIES, INC. SYNCRO AIRCRAFT 10109 SO. SHOEMAKER AVE. SANTA FE SPRINGS, CA 90670-3495 (562) 944-9971 7701 WOODLEY AV. VAN NUYS, CA 91406 PAGE 08 so' Jan. 28, 2000 CVSIODAEAS GROM 9390 .SAISPAAN TS.% Net 30 SFS SMAPCO VIA - Pratt' Trkg • • . . • per gal 2 5-gal. pails CC1025A adhesive, Lot #2521A0 20 90 209 00 ..-- .4ek Freight & handling charges, 25 88 FES 2 5 aCe £(0 W. 04 (5-C>- 6( ) 0 For resa e 51:1 i• c ‘i-ne TOTAL 234 88 LEGAL RATE OF INTEREST WILL BE CHARGED ON OVERDUE ACCOUNTS INVOICE PAGE: 34 SDNYGIvl _02753952 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40874 EFTA01326467 • • SDNY_GM_02753953 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240875 EFTA01326468 • SKAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 ****** ORDER NUMBER:0043599 ORDER DATE: 01/26/00 SOLD TO: SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE VAN NUYS CA 91406 INVOICE ****** INVOICE NUMBER: INVOICE DATE: CUSTOMER NO: PAGE: 1 0056911-IN 01/26/00 0001650 SHIP TO: SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE VAN NUYS CA 91406 CONFIRM TO: BRENDA CUSTOMER P.O. SHIP VIA 9388 FED SAVER F.0.8 TERMS DAVIS JUNCTION NET 30 1.5% LATE CHARGE ITEM NO. UNIT ORDERED SHIPPED BACK ORD PRICE AMOUNT SKAHC.25 EACH 1.000 .000 1.000 327.930 .000 .25"X56"X48' ENSOLITE AHC WHSE: 002 DAX26.5 EACH 15.000 15.000 .000 14.520 217.800 DAX 26 1/2"X24"X72" F/R FOAM LOT NUMBER: 11019-2 WHSE: 002 15.000 DAX261.0 EACH 15.000 15.000 .000 29.040 435.600 DAX 26 1"X24"X72" F/R FOAM LOT NUMBER: 01100-2 WHSE: 002 15.000 DAX262.0 EACH 20.000 20.000 .000 58.080 1,161.600 DAX 26 2"X24"X72" F/R FOAM LOT NUMBER: 11159-2 WHSE: 002 20.000 DAX471.0 EACH 15.000 .000 15.000 29.040 .000 DAX 47 1"X24"X72" F/R FOAM WHSE: 002 PAGE: 18 PAGE: 35 CONTINUED SDNYGIvl_02753954 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240876 EFTA01326469 SDNY_GM_02753955 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240877 EFTA01326470 • SKAND1A, 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 ****** ORDER NUMBER:0043599 ORDER DATE: 01/26/00 SOLD TO: SYNCRO'AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE VAN NUYS CA 91406 INVOICE ****** INVOICE NUMBER: INVOICE DATE: CUSTOMER NO: PAGE: 2 0056911-IN 01/26/00 0001650 SHIP TO: SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE VAN NUYS CA 91406 CONFIRM TO: BRENDA CUSTOMER P.O. SHIP VIA 9388 FED SAVER ITEM NO. UNIT ORDERED F.O.B TERMS DAVIS JUNCTION NET 30 SHIPPED BACK ORD 1.5% LATE CHARGE PRICE AMOUNT DAX472.0 EACH 10.000 .000 10.000 58.080 .000 DAX 47 2"X24"X72" F/R FOAM WHSE: 002 DAX55.5 EACH 25.000 25.000 .000 14.520 363.000 DAX 55 1/2"X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 10259-30 25.000 DAX551.0 EACH 15.000 15.000 .000 29.040 435.600 DAX 55 1°X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 12209-5 15.000 DAX552.0 EACH 20.000 20.000 .000 58.080 1,161.600 DAX 55 2"X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 01030-5 15.000 LOT NUMBER: 10259-5 5.000 FR CANVAS/NAT YARD 10.000 10.000 .000 10.000 100.000 FR CANVAS/NAT 64" X 1 YARD WHSE: 002 LOT NUMBER: 11249 10.000 1OMEX BATTING EACH 2.000 2.000 .000 375.000 750.000 PART 135 THERMAL BAT 40"X2OYDS WHSE: 002 LOT NUMBER: 01050 2.000 PAGE: 19 PAGE: 36 CONTINUED SDNYGlvl02753956 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA ()1240878 EFTA01326471 • SDNY_GM_02753957 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240879 EFTA01326472 V.L.43 - 0880K0O cn co rn H — I n -0 7a 0 rn n — I rn 0 70 C rn 7J -a 7a 7a to CO -P u, c, STIF-0 cu CI_ -sI iCl° 19618 Sold lo CORAL INDUSTRIES, INC. SYNCRO AIRCRAFT 10109 SO. SI•1OEMAKER AVE. SANTA FE SPRINGS, CA 90070-3495 (502) 944-9971 7701 WOOULEi AV. • VAN NUYS, CA 91406 Shippod to OAK Jan. 28 2000 (WO/4n ORDER 9390 SME5mAN IERAtS • Net 30 F.O.B. srs •• UWEDVIA Pratt Trkg... •• • • . . per gal 2 5-gal. pails CC102.5A adhesive, Lot 112521A0 20 90 209 00 Freight & handling charges 25 88 For resale w.6 4 (51 ) - 6 1 ' ) 507, 5b ' ). Sitlir TOTAL 234 88 : LEGAL RATE OF INTEREST WILL BE CHARGED ON OVERDUE ACCOUNTS t: II EFTA01326473 • • SDNY_GM_02753959 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240881 EFTA01326474 • SKAND1A, Inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 ****** ORDER NUMBER:0043599 ORDER DATE: 01/26/06 SOLD TO.: SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE VAN NUYS CA 91406 CONFIRM TO: BRENDA CUSTOMER P.O. SHIP VIA 9388 FED SAVER ITEM NO. UNIT ORDERED PBGE2.00L EACH 2.000 PSA BEIGE 2" LOOP 1.007 NUMBER: 11119-PHL PBGE1.OOH EACH 3.000 PSA BEIGE 1" HOOK LOT NUMBER: 11229-PHL PBGE1.00L EACH 3.000 PSA BEIGE 1" LOOP. LOT NUMBER: 01050-PHL SBGE2.00H EACH 2.000 SEW BEIGE 2" HOOK LOT NUMBER: 09298-HL PBLK2.00H EACH 3.000 PSA BLACK 2" HOOK LOT NUMBER: 01140-PHL PBLK2.OOL EACH 3.000 PSA BLACK 2" LOOP LOT NUMBER: 08309-PHL INVOICE ****** PAGE: 3 INVOICE NUMBER: 0056911-IN INVOICE DATE: 01/26/00 CUSTOMER NO: 0001650 SHIP TO: SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE VAN NUYS CA 91406 F.O.B TERMS DAVIS JUNCTION NET 30 SHIPPED BACK ORD 1.5% LATE CHARGE PRICE AMOUNT 2.000 .000 33.000 66.000 WHSE: 002 2.000 3.000 .000 19.750 59.250 WHSE: 002 3.000 3.000 .000 19.750 59.250 WHSE: 002 3.000 2.000 .000 15.750 31.500 WHSE: 002 2.000 3.000 .000 33.000 99.000 WHSE: 002 3.000 3.000 .000 33.000 99.000 WHSE: 002 3.000 PAGE: 21 PAGE: 38 CONTINUED SDNYGlvl_02753960 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240882 EFTA01326475 SDNY_GM_02753961 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240883 EFTA01326476 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax1515/227-192.0 ****** ORDER NUMBER:0043599• ORDER DATE: 01/26/06 SOLD TO: SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE VAN NUYS CA 91406 CONFIRM TO: BRENDA CUSTOMER P.O. 9388 SHIP VIA FED SAVER ITEM NO. UNIT ORDERED PBLK1.00H EACH 3.000 PSA BLACK 1" HOOK LOT NUMBER: 01050 -PHL PBLK1.OOL EACH 3.000 PSA BLACK 1" LOOP LOT NUMBER: 01050 -PHL SBLK2.00H EACH 3.000 SEW BLACK 2" HOOK LOT NUMBER: 11309 -HL SBLK2.00L EACH 2.000 SEW BLACK 2" LOOP SBLX1.00L EACH 2.000 SEW BLACK 1" LOOP LOT NUMBER: 09249-HL INVOICE ****** PAGE: 4 INVOICE NUMBER: 0056911-IN INVOICE DATE: CUSTOMER NO: 01/26/00 0001650 SHIP TO: SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE VAN NUYS CA 91406 F.O.B TERMS DAVIS JUNCTION NET 30 SHIPPED BACK ORD 3.000 .000 WHSE: 002 1.5% LATE CHARGE PRICE AMOUNT 19.750 59.250 3.000 3.000 .000 19.750 59.250 WHSE: 002 3.000 3.000 .000 15.750 47.250 WHSE: 002 3.000 .000 WHSE: 002 2.000 15.750 .000 2.000 WHSE: 002 .000 7.500 15.000 2.000 NET INVOICE: LESS pirWT: CRT: SALES TAX: 5,219.95 .00 PAGE: V60.85 .00 INVOICE TOTAL: 5,780.80 SDNYGlvl_02753962 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240884 EFTA01326477 SONYGAL02753963 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240885 EFTA01326478 SKANDIA FLAMMABILITY PICKING LIST FOR TEST CUSHION FABRICATION MATERIALS MATERIALS QTY. LOT# PICKED BY INSPECTED BY DAX GRAPHITE/POLY 26 ILD BURN BLOCK BACKS DAX.26.75X25 DAX .75" X 18' X 25* 6 a at￾033m. . 2Cn DAX GRAPHITE/POLY 26 ILD BURN BLOCK BOTTOMS DAX261.75X20 DAX261.75' X 18" X 20" 6 it ig,,,-.41- ,03n4 5--, ...• SKANDIA NOMEX BATTING ...- 2.5 YDS O7.1 yo Da￾THREAD 69 NYLON X 4 .- SKANDIA VELCRO 1' PBLK1.00L & PBLK1.001-I LOOP AND HOOK BLACK 09? 1- frt. 09119-NI￾0 3 ?go HC 4 CORAL ADHESIVES CC1025 ADHESIVE X TEST PLAN # 5823 WORK ORDER # 45812-00 PREPARED BY: JUDY BOGGS SweAO S-17-00 (7-e" 71g ft 30 it 30 31115 PAGE: 40 SDNYGlvl_02753964 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240866 EFTA01326479 SDNY_GM_02753965 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240887 EFTA01326480 ' • U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION •STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS UA It 04/25/00 AIWACA1-I UK AllitA<Ar I ILUNIVUtitti I IlltNIII-Ila I JUN MAKE GULFSTREAM SIN 1085 MODEL NO. OW TYPE (Altplene, Radio. Helicopter etc.) Anplane NAME OF APPLICANT Mandl; Inc SYNCRO AIRCRAFT INTERIORS Ub I UP VA IA IUnN i IFICANON NILE Work Order # 46501-00 Test ID 22923 . ... FLAMMABILITY TEST RESULTS REF: Skaudia, Inc. Test Plan #5902 Rev NEW Dated: 04/17/00 For PN's 5902-1 P/N 5902-1 Test pan* are r X 12' pieces of Knoll, Inc., Fabric 1(1831 Butai Pearl treated at Syncro Ref. Job #00-032. Both the warp and fill . of the fabric are tested . • Rev A Dated: 04/24/00 For PN's 5902-3 P/N 5902-3 Test panels are 3" X 12" piece's of Bergamo Fabrics., Fabric 1797-1 Lavin treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric arc tested. PURPOSE Or UM A DEMONSTRATION OF COMPLIANCE WITH MATERIAL FLAMMABILITY REQUIREMENTS APPUCABLE REQUIREMENTS 01st specific sections) FAR 25.853 (a) Appendix F Part I (a) (1) (h) CERTIFICATION -Under authority of appointment under Part 183 of have vested by direction of the Administrator and in accordance with conditions and limitations the Federal Aviation Regulations, data listed above and on attached sheets numbered been examined in accordance with established procedures and found to comply with applicable Regulations. approval of these data these data requirements of the Federal Aviation ecoromend I (We) Therefore Approve SIGNATURE(S) OF a. 0 TED ENGINEERING REPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) —A • \ ) DERY-405020-CE Structural Special Judy B ggs AA FOfi51 8110-3 (11.70) SUPERSEDES PREVIOUS EDITION SDNYGIvl_02753966 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240888 EFTA01326481 • • SDNY_GM_02753967 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240889 EFTA01326482 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 SYNCRO AIRCRAFT INTERIORS, INC. TEST PLAN #5902 REV A SKANDIA WO# 46501-00 GULFSTREAM GIV S/N 1085 DEMONSTRATION OF COMPLIANCE OF FAR 25.853 (a) APPENDIX F PART I (a)(1)(ii) DATE: REVISION NO. EFFECTIVE PAGE DESCRIPTION 04/24/00 A ALL ADDITIONAL TESTING CHANGED P/N 5902-2 TO 5902-3 04/17/00 NEW PREPARED BQA-i-a- Lei-) DATE: a4-00 JU CO ER CHECKED BY: A:a DICK LAUGHLIN DATE: le/2- s-70 APPROVED B DATE: c4-- D-5" 00 Page 1 SDNY GM 02753968 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002401390 EFTA01326483 SDNY_GM_02753969 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240891 EFTA01326484 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN 5902 REV A MATERIAL LIST: FABRIC: KNOLL, INC.: FABRIC K1.831 BUTAI PEARL TREATED ATZYNCRO REF. JOB #00-032 BERGAMO FABRICS: FABRIC 1797-1 LAVINA TREATED AT SYNCRO REF. JOB #00-032 TEST SPECIMENS TEST NO. 1 P/N 5902-1 Test panels are 3' X 17 pieces of Knoll, Inc., Fabric K1831 Butai Pearl treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric are tested. Test specimens are representative of fabric that will be used as lay aft bulkhead panel covering. TEST NO. 2 P/N 5902-3 Test panels are 3" X 17 pieces of Bergamo Fabrics., Fabric 1797-1 Lavina treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric are tested. Test specimens are representative of fabric that will be used as decor panel covering. Page 2 SDNYGlvl02753970 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240892 EFTA01326485 SDNY_GM_0275.71 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00240893 EFTA01326486 i tESIGN APPROVAL REQUEST • FAR 25.853 (a) APPENDIX F PART I (a)(I)(ii) TEST SPECIMEN DRAWING NO: 5902 WO #46501-00 REV A DATE: 04/24/00 MAKE: GULFSTREAM MODEL: GIV S/N: 1085 DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION OF CONFORMITY INSPECTION TEST SPECIMENS TO BE SUBMITTED FOR TESTING IN ACCORDANCE WITH FAA APPROVED TEST PROCEDURES ALL TOLERANCES +/- .030 INCH PANEL 5902-1 2' A 3' COMPOSITION MANUFACTURER PART NUMBER COLOR FLAME TREATMENT A FABRIC KNOLL, INC. K1831 BUTAI PEARL SYNCRO REF. JOB 00-032 ' Page 3 SDNYGIvl_02753972 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240894 EFTA01326487 SDNY_GM_02753973 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240895 EFTA01326488 • • DESIGN APPROVAL REQUEST FAR 25.853 (a) APPENDIX F PART I (a)(0(ii) TEST SPECIMEN DRAWING NO: 5902 WO #46501-00 REV A DATE: 04/24/00 MAKE: GULFSTREAM MODEL: GIV S/N: 1085 DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION OF CONFORMITY INSPECTION TEST SPECIMENS TO BE SUBMITTED FOR TESTING IN ACCORDANCE WITH FAA APPROVED TEST PROCEDURES • ALL TOLERANCES +1- .030 INCH PANEL 5902-3 12" 3" COMPOSITION MANUFACTURER PART NUMBER COLOR FLAME TREATMENT A FABRIC BERGAMO FABRICS 1797-1 LAVINA MULTI￾GREY SYNCRO REF. JOB 00-032 Page 4 SDNYGlvl02753974 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240896 EFTA01326489 r SDNY_GM_02753975 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240897 EFTA01326490 A A. KNOLL, INC. FABRIC K1831 BUTAI, PEARL TREATED AT SYNCRO REF. JOB 00-032 PRODUCTION DRAWING TYPICAL LAV AFT BULKHEAD COVERING TEST PLAN 5902 REV A DATE: 04/24/00 WO# 46501-00 GULFSTREAM GIV S/N 1085 BURR TEST REQUIRSHNT FOR THIS PRODUCTION AR77CLE IS ME7' BY ZEST SPECIME' 5902-I Page 5 SDNYGlvl_02753976 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240898 EFTA01326491 • SDNYGM02753977 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240899 EFTA01326492 A B. BERGAMO FABRICS: FABRIC 1797-1 LAVINA TREATED AT SYNCRO REF. JOB 00-032 PRODUCTION DRAWING TYPICAL DECOR PANEL COVERING TEST PLAN 5902 REV A DATE: 04/24/00 WO# 46501-00 GULFSTREAM GIV S/N 1085 BURN TES7'REQUTREVENT FOR THIS PRODUCTION ARTICLE 1S il&T BY SPECAIFJ 15902-3 Page 6 SDNY GM 02753978 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024090() EFTA01326493 • • SDNY_GM_02753979 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024[1901 EFTA01326494 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: WO #: 46501-00 SYNCRO AIRCRAFT INTERIORS Date: 04/18/00 7701 WOODLEY AVENUE Test Plan #: 5902 VAN NUYS CA 91406 PO ft: 09724 Aircraft: • GULFSTREAM GIV • S/N: 1085 VERTICAL FLAMMABILITY TEST RESULTS FAR 4853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 04/07/00 Time Out: 04/18/00 Specimen P/N 5902-1 Desc; • Test panels are 3" X 12" pieces of Knoll, Inc., Fabric K1831 Butai Pearl treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric are tested. Rev: A Flame Application (seconds) Flame Time (seconds) Bum Length (inches) Drippings (seconds) 12 Warp 0.0 Fill 0.0 Warp 2.3 Fill 2.6 Warp 0.0 Fill 0.0 12 0.0 0.0 2.6 2.6 0.0 0.0 12 0.0 0.0 2.5 2.9 0.0 0.0 ' Average: 0.0 0.0 2.5 2.7 0.0 0.0 Comments: Vertical (12 sec.) Bum Test: Average Self-Extinguish time may not exceed 15 sec. Average Bum Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Signed: VERT12-6124 Failed : ri • Page 7 SDNYG1.1_02753980 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40902 EFTA01326495 0 SDNY_GM_02753981 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240903 EFTA01326496 • SKAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: WO #: 46501-00 SYNCRO AIRCRAFT INTERIORS Date: 04/25/00 7701 WOODLEY AVENUE Test Plan it: 5902 VAN NUYS CA 91406 PO #: 09724 Aircraft: GULFSTREAM OW SIN: 1085 Rev: A VERTICAL FLAMMABILITY TEST RESULTS FAR 2_5.853 (a) Appendix F Part I (a) (1) (h) Conditioning Room: Tine; In: 04/24/00 9:00AM Time Out: 04/25/00 11:00AM Specimen P/N 5902-3 Desc.• • Test panels are 3" X 12" pieces of Bergamo Fabrics., Fabric 1797-1 Lavine treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric are tested. Flame Application (seconds) Flame Time (seconds) Burn Length (inches) Drippings (seconds) 12 Warp 0.0 Fill 0.0 Warp 0.9 Fill 0.7 Warp 0.0 Fill 0.0 12 0.0 0.0 0.8 0.9 0.0 0.0 12 0.0 0.0 1.0 0.8 0.0 0.0 Average: 0.0 0.0 0.9 0.8 0.0 0.0 Comments: Vertical (12 sec.) Bum Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed:❑ a Failed : Sign Page 8 ✓ERT12-6125 SDNYGIvl02753982 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40904 EFTA01326497 SDNY_GM_02753983 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240905 EFTA01326498 in C Sold To: SYNCRO AIRCRAFT INTERIORS INC CO 770I WOODLEY AVE Knoll VAN NUYS CA 91406 n H Purchase Order No. 09638 Purchase Order Release 7a Ln/ 0 Shp Dt Pattern Description 1.000 X1831 BUTAI, PEARL 4.000 54.00 Shipped Via: UPS Shipped Date: 32400 B.O.L.: 110248090000046 n-i 2.000 SHTX Shipping & Handling.- Textile 29.000 \ 1.00 0 7:3 C 7z) Knoll, ins Page: 2 Invoice Number 581029 Invoice Date 03/24/00 Qty List Price Discount Unit Net Price Extended Price 7D 7D in 02 'O tri ,E , 2 e, Terms Nit 30 DAYS Net Due 04/23/00 Tax Rt 8.250 C/ al - **-4 .00 54.00 • 216.00 Per YD .00 1.00 Per BA • 29.00 Merchandise Total: 245.00 • Sales Tax Total Order 17.82 Currency: 262.82 USD 4a EFTA01326499 SDNYGM02753985 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240907 EFTA01326500 SONY_GM_02 753986 This is to certify that the materials described below have been flame-retardant treated in order to meet the flammability requirements of FAR 25.853 (b) Amendment 25-32 by: SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40908 EFTA01326501 • • SDNY_GM_02753987 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240909 EFTA01326502 • BERGAMO FABRICS • INVOICE INVOICE * DI 031063 7 Win 22ND Sr. 2Nu FLOOs inw nits NY 10010 ill 212-•02-1010 FAX 212-462-1080 SOW TO . SYNCRO AIRCRAFT 7701 WOODLEY AVENUE . VAN NUYS VERONICA Ac II 7Rffd 3/1/93 CA 91406, SHIP TO 'SYNCRO AIRCRAFT 7701 WOODLEY AVENUE VAN NUYS VERONICA/ "116E-1532 TRANSACTION # • 695232-00 DATE . 03/29/2000 CA 91406 CUSTOMER P.O. SALESMAN SNOVIROOM DATE SHIPPED SNIPPED VIA TERMS .50 32015 03/29/2000 FEDEX IPD PROFORMA ITEM NO. DESCRIPTION QUANTITY UNIT PRICE AMOUNT 111#1-:.L. 1795-2 LHVANH/ QTY SHIPPED: 14.00 LINUS/ QTY SHIPPED: 2.00 14 IOW 111.1...i. /4/10 2.00 95.00 190.0E MATERIAL DISCOUNT MISCELLANEOUS FREIGHT& HANDLING 1660.00 37.50 PAGE 1 ALL ORDERS SHIPPED VIA FEDEX INTERNATIONAL PRIORITY DIRECTDISTRIBUTION'" SERVICE FecEx SALES TAX AMOUNT PAID ORIGINAL SDNYGlvl02753988 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 10 EFTA01326503 • • SDNY_GM_02753989 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 I I EFTA01326504 SONY_GM_02 753990 This is to certify that the materials described below have been flame-retardant treated in order to meet the flammability requirements of FAR 25.853 (b) Amendment 25-32 by: SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 1 2 EFTA01326505 r • SDNYGM02753991 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 13 EFTA01326506 MAY-26-2000 FRI 11:05 AN SCOTT GROUP MAY.26. 2020 9: 47AN DUNI, AVIATION • FAX NO. 616 954 9600 P. 02 M3.712 P.3/3 us DEPARTMENT OF TRANSPORTAMON POEM AMMAN ION STATEMENT OF COMPLIANCE WITH THEADMITTRA FEDERATL AVIATION REGULATIONS TAM 05126/00 OF Al CRAFT COMPONENT ID FICA- 10N MAKI. OULFSTREAM amMS moos Haw THE (MAWS, Ruda HoAtepfe0 AIRPLANE NAM OP APPUCAM SYNCRO AIRCRAFT MENTIFICATOR TITLE 0120 UST OF DATA SCOTT GROUP CUSTOM CARPETS 0 W16146M GLENCOE O.T. 100% WOOL CARPET DYE LOT 0 333118 PURPOSE OP DATA DEMONSTRATION OF COMPLIANCE WITH FAR MATERIAL FLAMMABILITY REQUIREMENTS APPIJOAKEREQUFREMENT6 (1.6 1 woe nacos; FAR MCI (a) AppeadtiR Part I I a )(fi( It ) 12 SECOND VERTICAL BURN MT. cmenrionoN Abider %Ape/ fluted by direction of tho Adrtinistralor of eppointnent under Part 183 of the Federal Aviation .Rnelgeris. have been examined ifl accordance with and In accordance WM conditions and limitations data geed above and on attached shoots fl ied established macadam and found to comply wth applicable requhemenla of th• Sand Aviation Rognaflons. I Mon toreforo 0 RecorMand /pp:OW of those data Ci AMINO them debt motanueem OF DillinittalTD ramorpeto ant tItsettrenvoMI PCSIONCRON MANURES) CIATSVICA110141) it/ rga# 09C . MA DERTMcascg FlAMMAIOLITY FAA Form 81104 (1140) SUPERSEDES PREVIOUS EDITION ode skis SDNYGIvl02753992 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240914 EFTA01326507 SDNYGM02753993 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 15 EFTA01326508 Test Number: 991342-1 4 : 'independent Textile P.O. Box 1948 I rdt g" Service, Inc. 1503 Murray Ave. Dalton, Georgia 30722-1948 • Phone 706-278-3013 • Fax 706-272.7057 • E-mail: ittslab@daltonmet TEST REPORT Customer Scott Group July 16, 1999 Subject "DOT, FM Title, 14, Part 25 - Airworthiness Standards: Transport Category Airplanes, Paragraph 25.853, Compartment Interiors, Sub-Paragraph (a) Vertical Flammability. ITTS's Certificate of Authority (DER) Designation No. SO.602. Sample Identification: Style: 333101 Town & Country Backing: Wide Cotton Back TEST RESULTS: P.O.# 09536 SCOTT GROUP# 333118 SIZE: 30sqyd!s PIECE: lofl all. ':.. PINSVOR:::'7:-”:, • • .. • . ,;-..-ARRligtro- -. : (sechnds). .Fffimean9-. - - (Seconds) ,FlarneTime - :. - PfieeitiO . (seconds) Pgri) 4M.41! (inches) Length 12 0 0 0 Length 12 0 0 0 Length 12 0 0 0 ,-.49010g0)_ - : .; . _ ;v.'. „.. -: . . - 0; .: .7: • 0 Width 12 0 0 0 Width 12 0 0 0 Width 12 0 0 0 Average - • lg - - 0 0 0 TEST REQUIREMENTS: Maximum Flame Time = 15 Seconds Maximum Flame Time Drippings = 5 Seconds Maximum Burn Length = 8 Inches (PASSES) L Kent Suddeth Executive Vice President Our letters and repot an forth culusive use of at caucus althorn they an eddressed. and that communication to arryotbas or the use of the name oflatlependentTaillaesting Sark; Inc.. must restive currier wrfuen apron/. °uction and rqxcts apply ocily to the uncle used edam not ntoessarily indicative orate qualities orapparendyidaileal or semau product The marts tad am and the name of the !navels:lent Tails TeitingService.the..ste not to be used u nder any tiro:Want:1ln advatisk,g tothepoen! public. - ----- , . • L/42 10IA (6A9) • SDNYGIvl_02753994 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240916 EFTA01326509 SDNYGM02753995 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 I 7 EFTA01326510 . U.S. DEPART/MR*OF TRANSPORTATION W . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 08, 2000 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION AKE .oULFSTFtEAM AEROSPACE MODEL NO. G-IV TYPE (Airplane. Radios Helicopter. etc.) Airplane NAME OF APPUCANT PETERSEN AVIATION UST OF DATA IDENTIFICATION 1171E DOCUMENT' STRUCTURAL SUBSTANTIATION - MINOR MODIFICATION TO 3- PLACE DIVAN, LH FWD. DIVAN MODIFICATION G-IV SIDE FACING DA-G1085 Rev. "NC" Dated: 5-08-2000 DRAWING: 50100-1085 Rev. "NC" Dated: 5-02-2000 • This approval indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as Applicable Requirements.' (Compliance to additional regulations not listed here may be required.) This form (does not) constitute FM approval of all the data necessary for substantiation of compliance to necessary requirements for the entire alteration/repair. (DETAIL DESIGN AND STRUCTURAL APPROVAL ONLY) • PURPOSE OF DATA TO SUBSTANTIATE THE MINOR MODIFICATION TO EXISTING 3-PLACE DIVAN ASSEMBLY ON GULFSTREAM G-IV AIRCRAFT, SIN 1085 ONLY ' ' APPUCABLE REQUIREMENTS (List specific sections) FAR 25.301, 25.303, 25.305, 25.307, 25.561, 25.603, 25.605, 25.607, 25.609, 25.613 and 25.789. CERTIFICATION - Under authority vested by dinmion of the Administrator and at accordance with conditions and limitations of appointment under Part NU of the Federal Aviation Regulations, data listed above and on attached sheets numbered ban boas examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. I 04) Matron = El Recommend Approval of these data Approve those data SIGNATURE'S) OF DESIGNATED ENGINEF_FLING REPRESENTAINEfs) ed.477r4d-err‘ -- DESIGNATION NUMBER(S) CLASSIFICATION X/c,CZIZZIZel d V DERT-605434-NM Structures Howard L Patterson FAA Form 8110-3 !11.701 SUPERSEDES PREVIOUS EDITION GPO 901413 SDNYGlvl02753996 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240918 EFTA01326511 • SDNYGM02753997 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240919 EFTA01326512 IV mar AIRCRAFT MODEL• GULFSTREAM G -IV AIRCRAFT REPORT NO. DA-G1085 PREPARED BY: DATE: 05-09-2000 REV: NC DYNAMO AVIATION STRUCTURAL SUBSTANTIATION- MINOR MODIFICATION TO IDOST1NG 3 -PLACE, DIVAN ASSEMBLY SHAHNAZ GALANTE 05-09-2000 APPROVED BY: HOWARD PATTERSON , 05-09-2000 REV DATE DESCRIPTION SDNYGM_02753998 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240920 EFTA01326513 SDNY_GM_02753999 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240921 EFTA01326514 TABLE OF CONTENTS I) References 2) Introduction 3) Structural substantiation — LH Fwd Divan modification Page 1 DA-G1085 Rev NC 05-08-2000 SDNYGIvl_02754000 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240922 EFTA01326515 SDNY_GM_02754001 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240923 EFTA01326516 1) REFERENCES 1 MIL-HDBK-5F Metallic Materials and Elements for Aerospace Vehicle Structures. 2 FAR 25. Page 2 DA- G1085 Rev NC 05-08-2000 SDNY GM 02754002 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240924 EFTA01326517 SDNY_GM_02754003 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240925 EFTA01326518 r • 2) INTRODUCTION This report provides structural substantiation on the modification of the LH Fwd divan on Gulfstream G-IV model aircraft, S/N 1085. The existing three place divan assembly is modified by moving the existing center truss structure aft by 4.75 inches and the fwd truss structure fwd by 4 inches. The center truss structure is connected to the outboard truss structure, however the basic outboard truss design has not changed significantly. The divan framing is made of 6061-T6 SQ tubing (for vertical and horizontal members) and Rectangular tubing for diagonal members. The divan was a TSO item and with this modification, the TSO Tag is removed and the divan is substantiated under a new part no. for the following load conditions. The gust condition of 7.2 G Down and 9.0 G Fwd load. 3.0 g side and 4.5 g up load. Divan new part number is: 50100-1085 I 40.00- 65.88 1 o 0 0 fa n VIEW B-B OLD FOOT PATTERN Exism4 a) Page 3 DA- G1085 Rev NC 05-08-2000 SDNYGlvl02754004 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240926 EFTA01326519 • SDNY_GM_02754005 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240927 EFTA01326520 3) STRUCTURAL SUBSTANTIATION: 3-PLACE DIVAN ASSEMBLY 9.0 O Fwd load Modified 3- Place Divan Weight including cushion, : 78 lbs Occupants : 3 x 170 = 510 lbs Total weight : 510 + 78 = 588 lbs .Total load : 9.0 x •588 = 5;292 lbs Attachment fitting loads The divan is tied down with six seat track fittings(Anchora) to the aircraft seat track. Load per fitting: 5,292 /6=882 lbs (shear) Tension load per fitting: (5,292 lbs x 22 in ) / 2 x 69.87 in = 833 lbs Minimum allowable for Tension for the seat track fitting is : 4000 lbs Minimum allowable for Shear for the seat track fitting is : 2000 lbs 1 MS = 1 —+ 1.05 [(882 / 2000)2 + (833 / 4600 )2] 1/2 X et t'x I ( ) Co 40.0 69.87 ° (%) ° (s) 4(5) ° (J (t-itotqcmD C onIF Page 4 DA- G1085 Rev NC 05-08-2000 SDNYGlvl02754006 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240928 EFTA01326521 • • SDNYGM02754007 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240929 EFTA01326522 3) STRUCTURAL SUBSTANTIATION: 3-PLACE DIVAN ASSEMBLY 9.0 G Fwd load Cont.d Fwd load on the divan, Outboard frame The Shoulder Harnesses are installed to the outboard divan frame for take off and landing. (The existing configuration). The center truss structurels connected to the outboard truss structure and by moving it to the aft by 4.7 inches resulted in minor redesigning of the outboard truss frame. The changes to the outboard truss structure are that the compression member (a) is longer by 3 inches and the tension member (b) is shortened by 4 inches. Since the basic truss design has not been changed, therefore it is still structurally adequate under fwd load and the change is considered minor. REMOVE LEGS (EX ISM-114G.) A I n ' tan via to -3 Cita ona,4 =WAD tat %IX ar PUY< FV11)..—.) (MODIFIED) Page 5 DA-G1085 Rev NC 05.08-2000 SDNYGlvl_02754008 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240930 EFTA01326523 SDNY_GM_02754009 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024093I EFTA01326524 3) STRUCTURAL SUBSTANTIATION: 3-PLACE DIVAN ASSEMBLY Center inboard/outboard truss structure The center piece moved to the aft and installed back as the original. Fwd . inboard/outboard truss structure The fwd truss structure moved to the most fwd frame. A SQ. Tube bridge is installed between the two top frames (fwd frames) and the existing vertical tube is welded to it and to the base frame. 0 groat.. 8 GUSSETS 10 BUSHING Page 6 DA- G1085 Rev NC 05-08-2000 SDNYGIv1_0275401 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240932 EFTA01326525 SDNY_GM_02754011 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240933 EFTA01326526 31 STRUCTURAL SUBSTANTIATION: 3-PLACE DIVAN ASSEMBLY 7.2 O Down load Pz = 7.2 g x 78 lbs = 562 lbs Load per three truss structures (inboard / out board): 562 lbs / 3 = 187 lbs See the end view (fwd end), load on the vertical post (-1). The post is at 18° Angle. Assume total 187 lbs acting on the -1 tube. Pz = 187 / COS 18° = 197 lbs for SG. Tubing: I= .0324 in4 A = .2300 in2 L = 12.62 13 inch PCR= n2 EI 2 /L 2 L=13 inch, E= 9.9X 106 PCR= C(712 E x .0324 ) / 132 -4 PCR = 606 lbs MS. = 606 / 197 -1 = + 2.0 -2 a ai tn) 1413 /D VIEW A-A M:177 165 10 BUSHING 0 Page 7 DA- G1085 Rev NC 05-08-2000 SDNYGIv10275401 2 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240934 EFTA01326527 • • SDNY_GM_02754013 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240935 EFTA01326528 3) STRUCTURAL SUBSTANTIATION: 3 PLACE DIVAN ASSEMBLY 7.2 G Down load Cont.(' Strength of the welded joint. The weld area is .176" x .176" x .25" Shear Stress of weld for a 6061-T6 material : 9,000 psi (ref. Lockheed weld design manual). P. = Area x Shear Stress T .707 S en' \2G . Area =tx L • 11 6" P = [(.707 x .176 x .25)1 x 9,000 = 280 lbs weld strength Pz= 197 lbs applied load MS = 280 / 197 -I = + .42 Page 8 DA- G1085 Rev NC 05-08-2000 SDNYGlvl02754014 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240936 EFTA01326529 • • SDNYGM02754015 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240937 EFTA01326530 C CD C L. rn n H 77 70 0 H rn n rn 0 77 rn 70 -o 70 Gl 70 cr) Co c) 2 y l to cu 0_ °,,, on C B A 4 M =XI MM Row =Man c was APOO .0 V= MORI MOW mlb0 COMM 00100115/11 07011•01 NM =ACME a UMW, MICR IteaCCI ORMAN Ram Dal WOO CC V Ti. 1. RELOCATE LEGS ON EXISTING DIVAN TO MAKE ROOM FOR 2 12 MAN LIFE RAFTS(61LBS EA), TO REPLACE ON 12 MAN AND ONE 6 MAN LIFE RAFT. 2. CUT LEGGS TO BE RELOCATED CAREFULLY, DO NOT DAMAGE REMAINING TUBING. 3. WELD LEGS PER MIL-W-2219 CLASS B, DYE-PEN INSPECT. ALL WELDED AREAS. NOTES: UNLESS OTP.ERMSE SPECIFIED 4 3 3 4 2 1 tatorrou twt 1 —41 -" 4 -$0 1 -0 -8 -7 -S OMMIIIR MS 0511-1 9(T1 waitasmasabinta _ 7V X I . 4541-19 %RIM VA1-11 DIM MR711:. 1-5 ;OM I'% A' X OM 5XCI 'As") 1. X A. X Of) KV Mt* • 8 1,45. ROL SO l'AC csr K41-11 SO ME I' ye', ou SO MI K01-10 PER 114-1-7:0/4 KR n -!-)Z/4 re in-i-70010 KR Vw-l-705/1 KA v•-4M1/1 7 • x 1041-10 'RI NOW S., PM WOO OISCROPVI PAP, LEVI WROACATOR A/ 5//11005 41/N (480-40 P<Y, ASV tee) CM Ns= •••=.0 C. TAYLOR 5/1/0) MOM gmG.:eta won, dna 424,2-4011 DIVAN MODIFICATION GIV SIDE FACING freartivi 2 • C $.4.1 1/I 1 SAVED AS: Ise I Or 1 1w— I-- 50100-1085 EFTA01326531 • SDNYGM0275401 7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240939 EFTA01326532 In co Cl -O 0 Cl 0 0 -O -O U) 9° N N O 2 ‘,1 4 II 3 4 2 REMOVE LEGS VIEW LOOKING OUTBOARD LEFT SIDE OF PLANE BEFORE MODIFICATIONS, REMOVED LEGS NOTED IN BLUE <---AFT FWD 3 t 2.' MOOS XVI MOIR MIAOW, MINE DIVAN MODIFICATION ON SIDE FACING J -' 501o0—lo&S 1/1 I sno /s: I —.dor 11'w EFTA01326533 SDNY_GM_02754019 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024[1941 EFTA01326534 4 -- tr) 0 c0 co oo In 0 O rnr z ce I- <▪ iL 0_ 0 U O L. (.4 G1 ; 3 ▪ Z < --- ‘=' O I n I 0 SDNYGNL02754020 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240942 EFTA01326535 SDNY_GM_02754021 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240943 EFTA01326536 Ln C CO rn n H 0 H rn n H rn 0 70 rn 77) -O 70 Gl 70 -O CO Co (-O O 2 'O I0 tl o_ 4 3 1 2 1 1SSET ADDED 3 PLACES O 58 O 7 O B NEW LEG AND ATTACHMENT 4S 3/4 SCALE 4 3 ..2 VYal%Y.0 win Lost q DIVAN MODIFICATION GIV SIDE FACING 7 — lb L'40 50100-1085 1 I -S K6 ruc EFTA01326537 SDNYGM02754023 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240945 EFTA01326538 00 VIP S. MEI C. CO O JI Os C) If) Cll Ifi CI • O I Cu r A In r, SONY GI,L 02754024 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240046 EFTA01326539 SDNY_GM_02754025 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240947 EFTA01326540 cr) co Cl H -O 0 0 0 -O -O Go C) f-r g CD_ -9 GUSSET 3 REQUIRED 910.88e -12 DOUBLER DIVAN MODIFICATION GIV SIDE FACING 7 50100-1085 r: isvio I... or EFTA01326541 SDNY_GM_02754027 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240949 EFTA01326542 co n -0 0 n 0 -0 lD p 2 U I ,c,„ 3 8 I 7 xs mar n “ rm. tam no. s Rolm lo no MI war.ca stn.= fa. 000 MIN... TRW", =4 SIM DM 141.50.01,41R1,111.11001N frEl Ktell I Ma 6 I 5 644,8. 30.00 25. -7 DIAGONAL MEMBER 49.2 47.5 075° 19.95 -6 DIAGONAL MEMBER 9.35 40.7 42.44' -5 DIAGONAL MEMBER 49.25° 42.44° 7.56° 64.62° EFTA01326543 r SDNY_Gtv1_02754029 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240951 EFTA01326544 In co Cl H 0 Cl 0 —O -6) -O V) .O N N 00 O Iv g CL 6(, - IJ In 4 3 2 1 4,88 4.06 -8 GUSSET 1.50 25.78' -2 DETAIL 115. 8° 11.61 -4 DETAIL 1.25 00.94 00.62r" -10 BUSHING 4 3 -7.19 12.62 \-) 71 2 PLS -1 DETAIL 15.00. 00.94 23.52 -3 DETAIL 25.08 2 -11 DETAIL Nte12800 ...mow., WI OWL II, III 01, Om 1.11411 DIVAN MODIFICATION GM SIDE FACING 7 i SINEO I". 3 Of 6 riC 50100-1085 1 EFTA01326545 SDNY_GM_02754031 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240953 EFTA01326546 • • -4 co 8 GUSSETS A 10 BUSHING (O (O 4- SDNYONL02754032 N 03 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240954 EFTA01326547 • • SDNY_GM_02754033 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240955 EFTA01326548 vid9 - 9c6ortoo (.1 co n H O -70 0 H n H 70 70 73 Gl 7J Cr) Co lO O 2 I— oJ F t= OJ Cl. 4 4 3 4 2 I 1 A A B - 12 DOUBLER WELD TO - 3 LEG 2 PLCS VIEW LOOKING OUTBOARD LEFT SIDE OF PLANE (---AFT FWD 4 3 2 MAYO " DIVAN MODIFICATION GIV SIDE FACING - 50100 - 1085 .. SOW AS, f se 2 Of 6 PNC 1 EFTA01326549 SDNYGM02754035 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240957 EFTA01326550 , lar .3 iI lei Oil illi . SDNY GM 02754036 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240958 EFTA01326551 • • SDNY_GM_02754037 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240959 EFTA01326552 . U.S. DEPARTIMI ..TT OF TRANSPORTATION W FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 15, 2000 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE GULFSTREAM AEROSPACE MODEL NO. G-IV TYPE (Airplane, Radio. Helicopter. etc.) Airplane NM E OF APPLICANT PETERSEN AVIATION LIST OF DATA IDENTIFICATION TITLE DOCUMENT: - SY-GL1085 Rev. "NC" Dated: 5-15-2000 • STRUCTURAL SUBSTANTIATION - TWO 17 INCH LCD MONITOR INSTALLATIONS RH/LH, FWD I AFT AND ENTERTAINMENT SYSTEM MODIFICATION: This approval indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements: (Compliance to additional regulations not listed here may be required.) This form (does not) constitute FAA approval of all the data necessary foi substantiation of compliance to necessary requirements for the entire alteration/repair. ,(DETAIL DESIGN AND STRUCTURAL APPROVAL ONLY) PURPOSE OF DATA TO SUBSTANTIATE THE INSTALLATION OF TWO 17 INCH LCD MONITORS AND ENTERTAINMENT SYSTEM MODIFICATION ON GULFSTREAM G-IV AIRCRAFT, S/N 1085 ONLY APPLICABLE REQUIREMENTS (list specific sections) FAR 25.301, 25.303, 25.305, 25.307, 25.561, 25.603, 25.605, 25.607, 25.609, 25.613 and 25.789. CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered • have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. I (3.11e) Therefore C Recommend Approval of these data l= Approve these data . SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION. mania /paraders- DERT-605434-NM Structures Howard L. Patterson FAA Form 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901.613 SDNYGlvl02754038 It SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40960 EFTA01326553 • • SDNYGM02754039 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024[1961 EFTA01326554 • AIRCRAFT MODEL: GULFSTRFAM G-IV • REPORT NO. SY-GL1085 8/N NO. : 1085 DATE: 5-15-2000 SYNCRO AIRCRAFT INTERIORS STRUCTURAL SUBSTANTIATION￾17 INCH LCD MONITOR INSTALLATION RH/LH, FWD/AFT BULKHEAD- MOUNT. AND ENTERTAINMENT SYSTEM MODIFICATION PREPARED BY: SHAHNAZ GALANTE 5-15-2000 APPROVED BY: HOWARD PATTERSON 5-15-2000 REV DATE SDNY GM 02754040 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240962 EFTA01326555 • • SDNY GM 02754041 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240963 EFTA01326556 TABLE OF CONTENTS 1) References 2) Introduction 3) Geometry 4) Structural Substantiation: Fwd and Aft RH/ LH 17" LCD Monitors Installation Page 1 SY-GL1085 Rev NC 5-15-2000 SDNY GM 02754042 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240964 EFTA01326557 • SDNYGM02754043 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240965 EFTA01326558 1) REFERENCES 1 MIL-HDBK-5F Metallic Materials and Elements for Aerospace Vehicle Structures. 2 FAR Part 25 Page 2 SY-GL1085 Rev NC 5-15-2000 SONY GM 02754044 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240966 EFTA01326559 • SDNYGM02754045 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240967 EFTA01326560 2) INTRODUCTION This report provides structural substantiation for the installation of twol7 inch LCD Monitors. One is mounted onto the Aft Bulkhead of the Fwd RH existing storage Cabinet (STA193) and the second one is mounted onto the fwd side of the Aft LH Bulkhead(STA442). The Aft LH Bulkhead is more like a divider than a load carrying Bulkhead for the existing Galley. The new 17 inch LCD monitors are installed in place of existing 14 inch monitors in exact locations. Also in the Fwd LH Comp (STA193). One Panasonic VCR Model PV4662, Weight 7.0 lbs is exchanged with DVD player model PS86802 , Weight 7.0. The subject installation and modification is on Gulfstream G-IV model aircraft SIN 1085. The subject installation is analyzed for the most critical load conditions. The following load factors are used herein: 9.0 G Fwd 7.2 G Down 4.5 G Up 3.0 G SIDE All the critical parts have been investigated, those not shown are considered not critical. Page 3 SY-GL1085 Rev NC 5-15-2000 SDNYGIvl_02754046 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240968 EFTA01326561 • • SDNY_GM_02754047 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240969 EFTA01326562 31 GEOMETRY- FWD/AFT RB/LR Bulkhead Mount, 17" LCD Monitor Installation art,Pith 0140 JO- tig„.a..12 Ebor ..3(ob ;opt ALIJA. iteu4Fbecibby cOrar Tritirt4ti Seal gevii LCD monin-00- rto Sand i7-‘43s. A041.e £ts4Y t.P /404434. •e./r Nett law. ovr-eor °La Mon/ wog- *" saitsch.I 7 Page 4 SY-GL1085 Rev NC 5-15-2000 SDNYGIvl_02754048 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40970 EFTA01326563 • • SDNYGM02754049 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024097I EFTA01326564 • • 4) STRUCTURAL SUBSTANTIATION- FWD/AFT R.H/LH Bulkhead Moon 17" LCD MonitorInstallation The subject LCD Monitor is installed on the Aft Bulkhead of the RH Fwd Cabinet with four Z- Brackets, top and bottom, Inb'd/Outed. The Z- Brackets are installed to the bulkhead with two #10-32 screws and NAS1836-13 inserts. Fwd LCD Installation WEIGHTS: New 17 inch LCD Monitor, Model # 170MP Total : 12.0 lbs Old 14 inch LCD Monitor. Weight 7.9 lbs 9.0 G Fwd load Px = 9.0 x 12 = 108 lbs total fwd load Load per 2-Bracket Px = 108 / 4 = 27 lbs Z- Bracket Supports. 2024-T3. t = .063" L = 5.0 in Rt = Px (2.0 in) / .50 in Rt = 108 lbs (tension in insert) Load per fastener. P = 108 /2 = 54 lbs (Tension) Bending stress of 2-Bracket, jb= 6M /b 12 width, b = 5.0" Max bending moment : 27 lbs x 1.0 in = 27 in-lbs .fro= 6 x27/5.0 in x.0632 =8,163 psi Ftu = 62000 psi for 2024-T3 (ref 1) MS = 62,000 / 8,163 -1 = HIGH Page 5 SY-CL1085 Rev NC 5-15-2000 SDNY Clvl 02754050 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240972 EFTA01326565 • SDNYGM02754051 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240973 EFTA01326566 • • 4) STRUCTURAL SUBSTANTIATION- FWDIAFT RA/LB Bulkhead Mount, 17"_LCD Monitor Installation Cont'd Fwd LCD Installation. Contd 7.2 G Down load Pz = 7.2 gx (12.0 lbs ) = 86.4 lbs Take the overturn by the upper and lower bracket Rrop= - Racer= (86.4 lbs x 2.0" ) / 12.88" Rrop = - Raman = 13.42 lbs Load per upper and lower bracket Down load Pz bears on the bottom Z-Bracket Rzsocke = 86.4 lbs Load per inserts (NAS 1836-3) Shear load: 86.4 lbs / 2 = 43 lbs Check bendino of the Z- Bracket Bending stress, fb= 6M /b tz width, b = 5.0" Max bending moment 86.4 lbs x 1.0 in = 86.4 in-lbs fb=6 x86.4 / 5 in x.0632 = 26,122 psi Ftu = 62000 psi for 2024-T3 (ref 1) MS=62,000/26,122 -1 = +13 1.5 a Aft load condition! Px = 1.5 x 12 =18 lbs (this load bears on the aft bulkhead) gst...(astree,,) • Esti Page 6 SY-GL1085 Rev NC 5-15-2000 SDNYGlvl_02754052 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40974 EFTA01326567 • • SDNY_GM_02754053 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240975 EFTA01326568 • 4) STRUCTURAL SUBSTANTIATION- FWD/APT RHJLII Bulkhead Monnt. 17" LCD Monitor installation Coned Fwd LCD Installation. Contd Check flange bending of the Z- Bracket Bending stress, fb= 6M /b t2 width, b = 5.0" Max bending moment: 13.42 lbs x. .50 in = 7.0 in-lbs fb= 6)(7.0 15 in x .0632 = 2,116 psi Ftu = 62000 psi for 2024-T3 (ref 1) MS = HIGH Check inserts. The largest Shear load and Tension Load on NAS1836-13: Pt = 54 lbs Ps = 43 lbs (Ref. P5,6) Insert Analysis Core shear allowable from: HEXCEL: 150 psi PALLowASLE = (150)(7t)(11 x .40) = 136 lbs Tension Bearing Allowable = Fen, = 121,000 psi (2024-T3) PALLOwASLE Br = (121,000 psi)(.02)(.451) = 1091 lbs Calculation of Margin of Safety Rs = 43/1091= .040 , R-r = 54/136 = .40 MS = 1/Rs + -1= 1/.040 + .40 = +1.27 Page 7 SY-CL1085 Rev NC 5-15-2000 SDNYGIvl_02754054 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240976 EFTA01326569 • • SDNYGM02754055 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240977 EFTA01326570 ) STRUCTURAL SUBSTANTIATION- FWD/AFT RH/LH Bulkhead Mount, 17" LCD Monitor Installation Cont'd Aft LH LCD Installation WEIGHTS: New 17 inch LCD Monitor, Model # 170MP Total : 12.0 lbs Old 14 inch LCD Monitor. Weight 7.9 lbs.. 9.0 G Fwd load Px = 9.0 x 12 = 108 lbs total fwd load This load bears on the bulkhead (this bulkhead is more like a divider than a load carrying bulkhead for the existing Galley, STA 442.). This Monitor installation is identical to the Fwd RH one shown on pages 4,5,6,7 . Page 8 SY-GL1085 Rev NC 5-15-2000 SDNYGIv1_02754056 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240978 EFTA01326571 0 0 SDNYGM02754057 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240979 EFTA01326572 AIRCRAFT INTERIORS, INC. EMPTY WEIGHT RECORD Aircraft type. Gulfstream GIV Serial # 1085 Registration- N677RP Weight Arm Moment Current Empty Weight from Jan. 28, 00 41887.7 460.95 19308255 Removed R/H 1 singe seat -67.5 172 -11610.0 Removed L/H 2 singe seat • . :96.0 225 -21600.0 Removed R/H 2 single seat -97.5 225 -21937.5 Removed R/H 3 singe seat -68.0 370 -25160.0 Removed R/H 4 single seat -68.5 424 -29044.0 Removed L/H 1 singe seat -68.0 172 -11696.0 Removed L/H 4 double seat - -1175 326 -38305.0 Removed L/H 3 double seat .. -119.0 272 -32368.0 Removed divan cushions -56.0 395 -22120.0 Removed galley linoleum -9.0 458 -4122.0 Removed VCR PV-4662 -8.0 145 -1160.0 Removed LCD Monitor SB1410AAB -7.9 ,151 -1192.9 Removed LCD Monitor SB1410AAB -7.9 443 -3499.7 Installed DVD PS8680Z +9.0 145 +1305.0 Installed LCD Monitor 170MP +12.0 151 +1812.0 Installed LCD Monitor 170MP +12.0 443 +5316.0 Installed R/H 1 singe seat +76.0 172 +13072.0 Installed R/H 2 singe salt +105.0 225 +23625.0 Installed R /1-i 3 singe seat +77.0 370 +28490.0 Installed R/H 4 singe seat +77.0 424 +32648.0 Installed L/H 1 singe seat +77.0 172 +13244.0 Installed L/H 2 singe seat +105.0 225 +23625.0 Installed L/H 3 double seat +143.0 272 +38896.0 Installed L/H 4 double seat +142.0 326 +46292.0 Installed divan cushions • +67.0 395 +26465.0 Installed galley carpet +18.0 458 +8244.0 New Empty Weight ( May 23, 2000) 42129.9 460.16 19386557.775 43.5914/ MAC Hours: ital Landings: 2111 PREPARED BY: Richard P. Jose 245198915 7701 WOODLEY AVENUE.VAN NUYS,CAUFORNIA 91406 • RioNE 818.901.9828 • Fax 818.988.5251 SDNYGlvl02754058 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40980 EFTA01326573 SDNYGM02754059 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240981 EFTA01326574 MATION.INIPR STANDARD AJAW011111INESS COMRCATEOCIN Nmu 'VrTYLT6-se "rsOLlsoni Fs. Form BICP2 SONY_CA1_02754060 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240982 EFTA01326575 SONYGM_027 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240983 EFTA01326576 cr) C co UNITED STATES CF AMERICA • DEPARTMENT OF TRANSPORTATION-FEDERAL AVLAION ADAENISTRATICN STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND 2 MANUFACIVRERANDMCCEL 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATIONMARKS NUMBER N677RP GULFSTRP,AM/GIV 1085 TRANSPORT IS AUTHORITY AND BASIS FOR ISSUANCE Ms sirwaltilnesi IMIRCAle Is Issued pursonl 10 to Federal MINIm AD of 1958 and cerlites that as «Ns ebbs of Issumee. 0 ne Goan lo whr.A &wed Pas been Foxe*, aid Mond lo omform lo the type Oillfleolo therefor. b be b comKon fee eale oPersOn and nos teen ire« to real In. req‘f romans of IRO Oppieable areonshensM DM &Mtn! Mr.ontWesa Cae as -o 73 mote by Area Elo Me CenvenlIcn of Wanorcnef CM Aw/S:n. MØ fes rried Pne Exce~ NONE 0 TERMS AND CCCITIONS Wins son sweerOarenl. mspended ietefied. IX a werineikm dW Y etIrelse eSISEININ4 by IM AdmnblRlp. INS tinvorflass torOlc.IM Is elSecOm as Mop es Oro noi-anence. nnweolot49 ermlnlsnetCR Md Illtealkm> are perfenred In iNcaclanos wln Pals 31. 43. end 91 <I Na Fedensl ASIOn Pernik,g as ndomdelat end ha elnyeAl Is fe~:1 M Ine Wiled DATE OF t331/ANCE REPAESENTA As, p er DESIGNATION NUMBER May 23 2000 L. 1,4O1TER WP-FSDO-01 An ~irk" ~nil^ la ~so al mala ~kola Mr be weal~le by a Y. *a wade, §1M9 am &where« rei 0~ 3 non AVIATION REGULA ai bat THIS CER NS TIPICATE MUST DE DISPLAYED N THE AIRCRAFT N ACCORDANCE WITH APPLICABLE FEDERAL TIO FAA Eon 8100.2 (Rod) APSE:can:Me Fain Sy!~ • JolFarn Foials• 12/19913 e as. EFTA01326577 SDNYGM02754063 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240985 EFTA01326578 .e • 'I T: r •I7 • 0 • - • ' MAJOR REPAIR tp USOerotineni oftroaserrako Fedora Aviation (Airframe, Rowerplant Aro d i \ L\ ALTERATION enE0 &Arian ... 10) Form AOPirked OMII No 2120.0020 For FAA Use ONy • Office Identification GI_ 13 Administnalen INSTRUCTIONS: Print or type all entries. See FAR 43.9. F 43 Appendix B.,:and AC 43.9- (or -70 subsequent revision thereof) for instructions and disposition o this form. This report is required by law (49 U.S.C. 1411). Failure report can result in a civil penalty not to exceed $1,000 for each vielationiSection 901 of Federal Aviation Act of 1958). Make &airstream Aerospace Cow: Model GM 1. Aircraft SaiaiNo. 1085 Nationality and Regetration Mark N864CE 2. Owner Name lessikoseroirmistatira rarcs tecia ... 1a) Coca Cola Enterprises Inc. Address iershounariniptatearerkkes) 2500 Windy Ridge Rosy SE Atlanta ,GA 30339-5677 3. For FAA Use On y 4. Unit Identification S Type Unit Make Model Serial No. Repair AJteration AIRFRAME described in item X As 1 above) powERriaa PROPELLER APPLIANCE TYPO Manufacturer G. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Gulfstream Aerospace Corporation W6365 Discovery Drive Appleton, WI 54915 U.S. Certikated Mechanic GIFE100Y Foreign Certificated Mechanic X Certified Repo': Station Manufacturer D. I certify that the repair and/or alteration made to the tin' (s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is this and correct to the best of my knowledge. Date DEC 1 0 1998 Signature e rd iii . 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified In item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and IsPlAPPROVED CI REJECTED FAA FIL Standards Inspector Manufacturer Inspection Authorization Other (Spee) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 0 i898 Certificate Of Designation No. GIFR1OOY Signatur odzed Indi r du FAA Form 337 ozak (CamputerGonended) SDNY_GIvl_02754064 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240986 EFTA01326579 NOTICE • • • • • Weight and balance limitation changes shall be entered In the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If mom space is required, attach additiOrtal sheets. Identify with aircraft nationally and registration mark and date work completed). Repaired L/H Flap "A" track recess I.A.W. Gulfstream Aerospace Corp. (FAA Approved) Structural Repair Manual Drawing 1169RDCS280 Rev. C dated 41-88, -901 Installation. Repaired R/H Flap "A" track recess per -904 installation same dwg. Note on -904 install, Sea. NAS1921M05-3 fasteners were substituted with tea. NAS1919M06-3 and lea. OSMLS100M04-03 per Gulfstream Service Engineering E-mail transmittal dated 12-6-98. Reworked L/H and Ft/H °A" flap tracks per -905 and -906 installation same dwg. END O Additional Sheets are attached. SDNY_GM_02754065 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240987 EFTA01326580 0 MAJOR REPAIF uswparrnw (Airframe, Powerpla curranomwm n - Federal Aviation Administration . id t iptValan • " I I Fare Approved OMB No.2120-0020 For FAA Use Only Office IdentificaterGL i 3 - . INSTRUCTIONS.Print or type all entries. See FAR 43.9, FAR-48-Appondi. O. oratA0 43r9al(a subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1.000 for each violationfSecgon 901 of Federal Aviation Act of 1958). Make. . Gulfstream Aerospace Corp. Model GIV 1. Aircraft Serial No. 1085 Natonaity and Regatation Mark N864CE 2. Owner Name (Ass/rowan fristfailonarrAfca.49) Coca Cola Enterprises Icc. Address (As goose or I fayStratiof makes) 2500 Windy Ridge Pkwy SE Atlanta ,GA 30339-5677 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME described in X (As Item 1 above) POwERMAiir PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement AL Agency's Name and Address B. Kind of Agency C. Certificate No. Gulfstuam Aerospace Corporation W6365 Discovery Drive Appleton. WI 54915 U.S. Certificated Mechanic GIFRIOOY Foreign Certificated Mechanic • X Certified Repair Station Manufacturer D. I certify that the repair and/or alteration made to the uni (s) Identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my knowledge. Date DEC 1 0 I000 Signature of AutinrizJ, I raidual ca. ".4 .4-- 7. Approval for Return To eevlco Pursuant to the authority given persons specified beew, the unit identified In item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is EL APPROVED 0 REJECTED FAA FIL Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection • DEC 1 0 1998 Certificate or Designation No. GIFRIOOY 22of Authr I al AA Form 33 (12-aM (Compute. Generated) SDNY_GIvi_02754066 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240988 EFTA01326581 NOTICE Weight and balance limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Doscription of Work Accomplished. • (If more space is required. attach additional sheets. Identify with aircraft nationality and registration mark and data work completed). Complied with Gulfstream Aerospace Corp. (FAA approved) Aircraft Service Change 400 dated 9-22-98 Structures - Aluminum Collar - Pressure Bulkhead FS 596 - Terminating Action. Aircraft weight and balance, Equipment list, and Electrical load is negligible or unchanged. END CI Additional Sheets are attached. SDNY_GM_02754067 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40989 EFTA01326582 - • • II" • ti - •" 0 MAJOR REPAIR AND ALTERATION I •-•• • US Depotrod (Airframe, Powerplant, Propfellebror A ppline) aratisartaron Administration 1 it , ; ULU 1 O Federal Aviation I. \‘: !it"; -:'. -tn￾f 1 Form Approved OMB No. 2120-0020 For FAA Use Only ) Office IdentificatioG4._ i INSTRUCTIONS: Print or typo all entries. See FAR 43.9, FAR Appendix:ff. altI7(C-439-110mtuiSquent revision thereof) for instructions and disposition o this form. This report is required by law (49 U. 14..F_ailtrileJarnErtEnaesR in a civil penalty not to exceed $1,000 for each violation (Section 901 of Federal Aviation Act of 1958). 1. Aircraft Make Gulfstrearn Model G-IV Serial No. 1085 Nallerialit), and RegStraticn Mark N864CE 2. Owner Name (rtsslotrwaregisfrationtarriffsafe) Coca Cola Enterprises, Inc Address (Assbonnoaregisbaliontertikale) 2500 Windy Ridge Pkwy SE Atlanta, GA 30339.5677 3. For FAA Use On y 'The data/alteration identified herein cowries with the applicable airworthiness requirements and Is approved for the above described aircraft subject to calamity inspection by a person authorized In FAR 43, Section 43.7'. Date iz/9/9( FAA Inspector GL13 4. Unit anti cation 6. Type Unit Make Model Serial No. Repair Alteration AIRFRAME As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Culla:tam Aerospace Corporation W6365 Discovery Drive Appleton, WI 54915 U.S. Certificated Mechanic Foreign Certificated Mechanic GIFR100Y X Certified Repair Station Manufacturer D. I certify that the repair and/or alteration made to the uni Cs) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date /2/9/98 Signature of Authorized In • ual • t 7. Appro r Return To Service Pursuant to the authority given persons specified below, unit identified in Item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is (APPROVED CI REJECTED FAA FR Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection /2 -4)-9se -• • - --- - - --- -- Certificate or Designation Designation No. Signature of AVUodiedl ual r Genera SDNY_Gtvl_02754068 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240990 EFTA01326583 NOTICE Weight and balance limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DescdptIon of Work Accomplished Qf more space is required. attach additional sheets. Identity with aircraft nationally and registration mark and date work Completed). Replaced one AD rivet in clip angle bracket on the under side of right cockpit floor.structure, F.S. STA 56.812, forward of floor access panel FLR-4 installing a Hi-Lok P/N: HL18 fastener. Also installed an additional Hi-Lok P/N: HL18 fastener in adjacent hole of same clip, found missing since production. END O Additional Sheets are attached. SDNY_GM_02754069 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024099I EFTA01326584 - e 7.••• c r1 Ora .0 MAJOR REPAIR AND AL USecoretmere ontensooncoon (Airframe, Powerplant, Propelle Asepearericasen Admmemmon --• 7 . -7. . 2..0 1 441998 I;l _ JO. :Form Approved OMB No. 2120-0020 For FAA Use Only Office Identificatioph., 13 INSTRUCTIONS:Printer type all entries. See FAR 43.9, FAR43 A subsequentrevision thereof) for Instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to repo can result in a civil penalty not to exceed stood tor each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE Model G-IV • Serial No. 1085 Nationality and Registration Mark N864CE • • 2. Owner Name (As shown on registration certificate) COCA COLA ENTERPRISES, INC. Address (As sltown on registration certilkate) 2500 WINDY RIDGE PKWY SE ATLANTA, GA 30339-5671 3. For FAA Use Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME • • (As described in Item I above) X . • ^. . . . POWERPLANT • PROPELLER APPLIANCE Type . Manufacturer . S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certi kale No. GULFSTREAM AEROSPACE CORP. W6365 DISCOVERY DR. APPI.PTCK WT T•421% U.S. Certificated Mechanic G1FR100Y Foreign certificated Mechanic It Certificated Rees& Station _ issausuturar D. I certify that the repair and/or alteration made to the un t(s) identified In Item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein Is true and correct to the best of my nowledge. Data • DEC 1 0 1998 . Signatur f Authottect' • 7. Approval for Return To Seneca Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is MAPPROVED 0 REJECTED BY FAA Fit. Standards Inspector Mariblacturer Inspection Authorization Other (Specify) FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of AppitNal or Refection DEC I 0 1998 ' Certificate or Designation No. G1FR100Y Signal Authoriz Inds • ual A Form 337 ilVeal SDNY_Givl_02754070 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240992 EFTA01326585 NOTICE Weight and balance oroperating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Descdption of Work Accomplished (II more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Modified the existing Third Comm & Nat Systems by removing the Gables G6860-09 Conun/Nav Control Head, and installing a Collins CTL-23 Digital Control Head, P/N 622-9851-001. The third Comm / NAV system's interface was retained as previously installed with the exception of the controller. GAC modifications to the aircraft wiring for the new control head interface is depicted on the GAC revision to Western Commander Inc. wiring diagrams: No. 3 VHF COMM, 08069110; and No. 3 VHF NAV, 08069128, of which the electrical/electronic aspects of the GAC listed revision is DER approved by N. Kopesky, CHI-262. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes iri system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A, Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END ❑ Additional Sheets Are Attached OILS. GOVERNMEET PRINTING OFFICE: t902-760-012/E0I57 SDNY_GM_02754071 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240993 EFTA01326586 0 MAJOR REPAIR ANII! us oecerirreni co tensonoton Acurmumnian (Airframe, Powerplant, PripterWergdgg) Federal manse 6 .• — — Ail I I Form Approved OMB NO. 2120-0020 I f For FAA Use Only li i. j Office Identificatior 1 3 (.71, k , i INSTRUCTIONS:Print or type all entries. See FAR 43.9. FAILSAppandiatranclACAS.W.US.16bsequent revision thereof) for instructions and disposition of this form. This report is required by law ( 9 U.S.C.1421 ). Failure to report can result In a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Akcraft Make GULFSTREAM AEROSPACE Model G-IV Serial No. 1085 Nationality and Registration Mark N864CE - . . 2. Owner Name (As shown on registration certificate) COCA COLA ENTERPRISES, INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PKWY SE ATLANTA, GA 30339-5677 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME . ' (As described In Item 7 above) X . .. . POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8 Conformity Statement A. AgencYs Name and Address B. Kind of Agency C. Ceni kate No. US. Certificated mechanic G1FR100Y GULFSTREAM AEROSPACE CORP. Foreign certificated mechanic W6365 DISCOVERY DR It Certificated ROPOtStalion APPT MICK MGR 5491c Manufacturer D. Icertifythat the repair and/oralteration made to the un have been made in accordance with tht requirements furnished herein is true and correct to the best of my Rat Identified in item 4 above and described on the reverse or attachments hereto of Part 43 of the U.S. Federal Aviation Regulations and that the information nowledge. Date DEC 1 0 1998 Signatu Authord . I WI • 7. Approval for Return To nice Pu suant to the authority given persons specified below, the unit identified In Item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is CkAPPROVED O REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 0 1908 • CertlficaM or Designation No. GIMUDOY Signatu Author Nast . - , orm 337 mast SDNYGM_02754072 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240994 EFTA01326587 • r . NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate effete( t record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished - • . (It more space is required, attach additional sheets. Identify withaircralt nationality and registration mark and date work completed.) Installed an Allied Signal Avionics Enhanced Ground Proximity Warning System (EGPWS), computer P/N 965-0976-003-104-104, as per Guffaws= Aerospace Corporation (GAC) STC ST01445AT. In order to facilitate this installation, the existing MK-V Ground Proximity Warning System (GPWS), computer P/N 965-0676-0010 (installed per Sits SA218850, FAA Form 337 dated 9/7/89 & ST00714AT, FAA Form 337 dated 1/26/96) was roved from the aircraft Additionally, the three (3) each Honeywell SG-884 Symbol Generators, P/N 7008570-904 have been modified to -905 and the two (2) each Honeywell DC-884 Display Controllers, P/N 7007540-942 have been modified to -946 to allow for EGPWS selection and display of the enhancement features. Deviations to STC ST01445AT include: • Utilized existing wiring where practicaL • Retained the previously installed GPWS circuit breakers and some of the annunciation by incorporating them into the new EGPWS system. System interface and wiring as depicted on GAC wiring diagram GIV-31085-34-10 is electrically equivalent to the aforementioned STC. • Mounting the computer in the R/H radio rack extension at the same location as the removed GPWS computer. Expanded the STCd EGPWS Relay Unit design to house system components. Installed this newly fabricated Avionics Interface Unit in the R/H radio rack extension, adjacent to the EGPWS computer, picking up existing structure. FAA Approved Airplane Flight Manual Supplement, SC41 349M37 dated 8/8/97, with Rev. 02 dated 4/8/98 is required for this approval and supersedes all previously issued AFMS' pertaining to GPWS. Maintenance Requirements - Instruction for Continued Airworthiness, GAC Document No. 5C41 349A01, Rev. 1, dated 6/22/97 with attached AlliedSignal.Line Maintenance Manual, Doc. No. 060- 4199-014 is required for this approval. Eating wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A, Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END O Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING °EPICS: 1912-769-012/60IS7 SONY _GM_02754073 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240995 EFTA01326588 " 0 MAJOR REPAIR AN I I ) ' fRILT I I 1 TIO 1 1998 i I Form Approved OMB No. 2120-0020 uscepamert (Airframe, Powerplant, Pr dTrarasatatian wiener, or ApAliance) j For FAA Use Only Uldi Office klentficationGL Federal Aviation Administration /3 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 4247ZEftendirtralttlertraffitrzybesquent revision thereof) for instructions and disposition of this form. This report M required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each violation (Section 901 of Federal Aviation Act of 1958). Make. Gulfstrezun Aerospace Corp. Model GIV 1. Aircraft Serial Na Iffil5 Nationality and Registraticn Mark P1864CE 2. Owner Name aflame oitapistrattisaceritecak) Coca Cola Enterprises Inc. . Address (As shaman faySiMaancefffitak) 2500 Windy Ridge Pkwy SE Atlanta GA 30339-5677 3. For FAA Use On y 4. Unit Identification 6. Type Unit Make Model Serial No. Repair Alteration AIRFRAME X (As descabcd in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. IGnd Of Agency C. Certificate No. Oulfstream Aerospace CorpenitiOn ' W6365 Discovery Drive Appleton. WI 54915 U.S. Certificated Mechanic GI FRI 00Y Foreign Certificated Mechanic X Certified Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified In item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is hue and correct to the best of my knowledge. Date DEC 1 0 1998 . SIgnatu refuel 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified In item 4 was inspected in the manner prescribed by the AdmInisUator of the Federal Aviation Administration and isySAPPROVED CI REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC. 1 0 1998 Certificate or Designation No. GIFRIODY Signal Authoo rni f t nn 337 (1248) (Compote: Generated) SDNY_Gtvl_02754074 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240996 EFTA01326589 NOTICE Weight and balance limitation changes shall be entered tri the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity With the applicable airworthiness requirements. 8. Description of Work Accomplished , (If more space Is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed). Removed Bendix Instrument Landing system (ILS), consisting of 2ea. ILS Receivers, 2ea. racks, and lea. ILS controller. The ILS system was originally installed at the factory. The ILS system was previously disabled I.A.W. AD 89.02-12 R1 dated March 21, 1994. #1 and #2 ILS circuit breakers were previously removed. Connectors are capped, bagged, and stowed. Removed the following equipment: 2ea. Bendix ILS Receivers P/N 2104-1230-3504 lea. Bendix ILS Controller P/N 1159SCAV404-3 lea. ILS Rack P/N 1159AV40369-1 lea. ILS Rack P/N 1159AV40369-2 The weight and balance manual and equipment list were revised. END ❑ Additional Sheets are attached. SDNY_GIvl_02754075 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240997 EFTA01326590 .0 MAJOR REPAIR US Cocain/al orlandomaron Administration (Airframe, Powerplant, P Federal Aneden re:-Q7: r : •._,,, ts _., • ITERATION regal; Ay/ El I &zee Form Approved OMB NO. 21204020 For FAA Use Only Office IdentificationGt 13 INSTRUCTIONS:Print or type all entries. See FAR 43.9, F and disposition of this form. This report Is required by lave44946S.G..1421)...Eatakirggenad for each such violation (Section 901 Federal Aviation Act kR43Appendix 8. an = 01 1958). or ulnas:went revision thereof) for instructions result in a civil penalty not to exceed $1,000 1. Aircraft Make GULFSTREAIA AEROSPACE ' Model G-IV Serial No. 1085 Nationality and Registration Mark N864CE • z Owner Name (As shown on registration certificate) COCA COLA ENTERPRISES, INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PKWY SE ATLANTA, GA 30339-5677 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item 1 above) X • ' ',.. - . P0WERPLANT PROPELLER APPLIANCE Tyne • Manufacturer . 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C: Certificate No. GULFSTREAM AEROSPACE. CORP. W6365 DISCOVEItY DR. ADM PION, WI Sal 5, (U.S. Certificated mechanic • GIFRIOOY ' Foreign Certificated Mechanic Certificated Repak Station Manufacturer D. I certifythat the repairand/or alteration made to the un t(s)identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my nowledge. Date DEC 1 0 1998 Signature of Authorized Indiv u • 7. Approval for Return To Send Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is [(APPROVED . CI REJECTED BY FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station A oved by es Person Transport Canada Ainvonhin ppr s GrouP Dale of Approval or Rejection DEC 10 1998' Certificate or Designation No. GIFRIDOY Signatu uthorized dd - lt • FAA Form 337 ordist. SDNY_GI.1_02754076 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240998 EFTA01326591 NOTICE Weight and balance or operating limitation changes shall be enterid in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished . (It more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Installed dual digital Collins RTU-4210 Radio Control Units in the center pedestal in accordance with Atlantic Aviation/Delta Engineering STC ST00717NY-D, dated May 19, 1998, replacing the GAC installed Gables Comm/Nav/ATC/ADF / TCAS Control Heads. Newly installed equipment includes: 2 Ea. Collins RTU-4210 Radio Tune Units, P/N 822-0836-005 Removed equipment includes: 2 Ea. Gables 700-D36407A-002 Comm Controls 2 Ea. Gables 700-D36409A-002 Nav Controls 2 Ea. Gables 700-D36411A-002 AIDE Controls 1 Ea. Gables 700-D36413-008 ATC 1 Control 1 Ea. Gables 700-D36413-003 ATC 2 Control 1 Ea. Gables 700-D36415A-003 Marker Control 1 Ea. Gables G6969-04 TCAS Control Refer to GAC drawings: VHF Comm Mods, GIV-31085-23-20; VHF NAV/DME Moth, GIV-31085-34- 26; ADE System Mods, GIV-31085-34-32; ATC System Moth, GIV-31085-34-35; Control Heads, GIV￾31085-34-37; and FMS Mods, GIV-31085-34-58, which is electrically equivalent to the aforementioned STC. FAA Approved Airplane Flight Manual Supplement, 62743606-340 dated 5/19/98, with Rev. — is required for this approval and supersedes the existing AEM and attached supplements only in the areas contained therein. Maintenance Manual Supplement, Delta Engineering Document No. 727-03609-340 dated 5/19/98, with Rev. — is required for this approval. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A, Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END 0 Additional Sheets Are Attached dV.S. GOVERNMENT PRINTING OFFICE: 1,12-755-017/60I57 SONY GM 02754077 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40999 EFTA01326592 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATION DATE February 9.1996 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream MODEL NO. G-IV TYPE (Airpkne,Radiodielicopter etc) Airplane NAME OF APPLICANT The Jet Center LIST OF DATA IDENTIFICATION TITLE Drawing Number Rev. Date 0 Shts Drawing Tide 3 FMS 1 & No. 2 Global Position and approved as it pertains to only. 08069100 08069324 A 01/20/96 5 No. A 01/20/96 1 No. 'END' Note: The above data is reviewed electrical systems and equipment PURPOSE OF DATA To show compliance with applicable Federal Airworthiness Regulations for minor deviations to S.T.C. SA3774NM for Gultstrearn G-TV, S/N 1085, N88GA ONLY via FAA. Form 337. APPLICABLE REQUIREMENTS Vitt specific sections) FAR's: 25.1301(nkod); 25.1309(a,b,c); 25.1322(be,d); 25.1355(c); 25.1357(a,c,d). CERTIFICATION - Under authority vested by direction of appointment under Part 183 of the Federal Aviation none have been examined in accordance of the Administrator and in accordance with conditions Regulations, data listed above and on attached sheets with established procedures and found to data and limitations numbered comply with applicable requirements of the Federal Aviation Regulations. I ewe) Therefore A Recommend approval of these Approve these data SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) .gLits,ci re rt nA--- NM-2128 Systems & Equipment Sarlds A ICara,guzian . orm EI 10-3(11.70) SUPERSEDES PREVIOUS EDITION GPO 901-613 SDNYGlvl_02754078 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241000 EFTA01326593 SDNYGM02754079 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241001 EFTA01326594 . A. A ch-cf4:-c-s C 1 U.S. Department MAJOR REPAIR AND ALTERATION of Transportation (Airframe Powerplant, Propeller, or Appliance) 'Federal Aviation Administradon Form Approval OMB No. 2120-0020 For FAA Use Only Office Identification STITS11O.11 .,114STRUCTI0NS. Print or type all antics. See F AR 43.9 FAR 43 Appendix B. and AC43.9-1 (cesubscquent revue= thereof) for =ass and cIsposilkm dais tbrin. Ibis report is required by law (49 U.S.U. 1421). Faun to report can remit illation penalty not to exceed $1,000 for cub nub violation (Section 901 Federal Aviation Actor 1938). 1. Aircraft Make Gulfstream Model (MV Serial No. 1085 Nationality and Registration Marks U.S.A. N864CE 2. Owner Name at shown on registration Certificate) Coca-C-ola Enterprises Inc. Address (As shown on registration certificate) 3931 Ann Dr NW Atlanta, GA 30336-1512 3. For FAA Use Only • 4. 17alt Identification 5. type Unit Make I Model I Serial no. Repairs Alterations Airframe - — X (As described in irem I above) P ea— Powerplant Propeller Appliance Type ManUfaCtUrtr 6. Conformity A. Agency's Name and Address B. Kind of Agency C. Certificate No. Gulfstream Aerospace Corporation P.O. Box 2206 - Travis Field Savannah. GA 31402-2206 U.S. Certificated Mechanic Foreign Certificated Mechanic FAA CRS GR4R216M X Certificated Repair Station Manufacturer D. I cab& that tbe repair andlor alteration made to the =Ns) idadified m item 4 above and !wailed ca the muse or anathacrits bare have been made in accordance with the requirements of Part 43 efthe US. Federal Regulations and that the information garnished benzin is true and ant the bet army knowledge￾Date 09/05/97 Signature of Authorized Indivi ual Steven Sweeney 7. Approval for Return To Service Punuant to the authority giveo persons specified below, the unit identified in ban 4 was inspected in the manner prescribed by the Atli:enteral& Federal Aviation Administration and is El APPROVED O REJECTED BY FAA FIt. Standards Inspector￾Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Ai worthiness Group Date o Approval dr Rejection - - 09/05197 Certificate or - - Dedgoation No. FAA CRS GR4R216M Signature of Assiberized individual Jimmie K. Smith . ' A,.. g ntei, . SDNYGlvl_02754080 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241002 EFTA01326595 • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate tuft retort An alteration must be compatible with al t previous alteration to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished: (temote space is requited snub soiTstional sheets kleo* vale ainraft Whoa* end registration mark iodate bark completab. Aircraft Model: G-IV Aircraft Time Since New: 2853.9 Aircraft Serial No.: 1085 Aircraft Landings Since New: 1227 Aircraft Registration No.: N864CE Reference: Gulfstream Aerospace Corporation Workorder No.: C04-1085-097-0042 1. Incorporated the following FAA approved major Gulfstream Aircraft Service Changes: ASC No.: Subiect: 135 A2 ECS Pack Sequencing During Engine Start End O Additional Sheets Are Attached SDNY_GM_02754081 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241003 EFTA01326596 -- 8TAWDARISAIRWOMINES8 CITTFICATI II866CZ 0:11.18118Sall/GIV 10115 MUM= • J•I•antr".•••• WWI. ::•••.:::========" " "" Ion • 71:3. 12-16-88 Vitt FM Fo, Me" man SDNY_GM_02754682 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241004 EFTA01326597 SONY_GM02/59083 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241005 EFTA01326598 . _ • !r,7-• •-• • \\ (Cly t ; • II f - 6 L.,:,7 MA. mmn (Airframei if • • R REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification - AI /3 ClitragtFriRroitype an en and disposition of this form. This report for each such violation (Section 901 des. See FAR 43.9, FAR 43Appendix B. and AC 43S-1 (or subsequent revision thereof) for instructions is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 91,000 Federal Aviation Act of 1958). 1. Aircraft Make Gulfstream Aerospace Model—-1.,-IV Serial No. 7085 Nationality and Registration Mark N 2. Owner Name (As shown on registration certificate) Coca-Cola Enterprises, Inc. Address (As shown on registration certificate) 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA Use Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PROPELLER APPUANCE Type Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated mechanic QK2R112L K-C Aviation, Inc. Foreign Certificated Mechanic 301 Discovery Drive X c•niscanics sops swan Appleton, WI 54915 Manufacturer D. I certify that the repair and/or alteration made to the un have been made In accordance with the requirements furnished herein is true and correct to the best of my know t(s) identified in Item 4 above and describedon the reverse or attachments hereto of P n 43 of the U.S. Federal Aviation Regulations and that the Information edge. Date DEC 20 1996 Signature of Authorized Ina( ual 7. Appro I or Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Ft.APPROVSO - 0 REJECTED FAA Rt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date& Approval or Rejection DEC 20 1996 Certificate or Designation No. ClK2R112L Signature of Authorized Ind' 'dual (cdseine. • FAA Form 337 /2.s SDNYGIvl_02754084 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241006 EFTA01326599 NOTICE Weight and balance or operating limitation changesshall be entered in the appiopriate aircraft record. An alteration niust be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (II more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed:) . Fabricated and installed life raft storage provisions for two rafts under divan, F.S. 379 and F.S. 415 in accordance with K-C Aviation, Inc., Structural Drawing GIV-25-01-222, sheet 1. DER approval is in accordance with 8110-3 form dated 12/20/96 by A. Duncan, CHI-424. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC-43.13-1A chapter 6 as a guide. Materials used meet the requirements of FAR 25.853. END O Additional Sheets Are Attached OILS. 00VICRNMENT PRINTING OPPIGC: I192-749-0I2/101117 SDNY_GM_02754085 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241007 EFTA01326600 Form Approved OMB No. 2120-0020 MAJOR - 6 tlAn1d rams) Aviation tmrlinn IL" ' REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) For FAA Use Only Office Identification Ch/3 atiglIaLICTIOAMPrig4014490411-sa and disposition of this form. This report for each such violation (Section 901 ries. See FAR 43.9, FAR 43Appendix EL and AC 43.9-1 (or subsequent revision thereof) for instructions is required by law (49 U.S.C. 1421). Failure to report can result In a civilpenalty not to exceed S1.000 Federal Aviation Act of 1958). 1. Aircraft make Gulfstream Aerospace Model G-IV Serial No. 1085 Nationality and Registration Mark N88GA t Owner Name (As shown on registration certificate) Coca-Cola Enterprises, Inc. Address (As shown on registration certificate) 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA UVVEINIXIA/ALI trUAI ILMIrrilzIJAIti ILltN I II-ICU ItHtinil GUM Itb WI I H I It mar 4GAbLt REQUIREMENTS AND IS APPROVED DESCRIBEDAIRCRAFT, SUBJECT TO INSPECTION BYA PERSON AUTHORIZED SECTIO 43. HIFIVVUti I FOR THE CONFORMITY I I-IINtbb ASOVE AR 3IGNA—U 4. Unit 'dentin; . Unit Make Model IAA MICE FSDO Serial No. Repair Alteration AIRFRAME (As described in Item 7 above) X POWERPtAfff PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Cenificated Mechanic QK2R112L K-C Aviation, Inc. Foreign Certificated mechanic 301 Discovery Drive x Certificated Repair Station Appleton, WI 54915 manufacturer D. I certify that the repair and/or alteration made to the un have been made in accordance with the requirements furnished herein Is true and correct to the best of my knowledge. t(s) identified in item 4 above and described on the reverse orattachments hereto of Part 43 of the U.S. Federal Aviation Regulations and that the information Date DEC 0 9 1996 Signature of Authorized Individual -kO . 7. App a tor Return To Service Pursuant to the authority given persons specified below, the unit Identified In item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Q, APPROVED O REJECTED FAA FIL Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee ., A Repair Station Person Approved by Transport Canada AIMOilhintSS Group Date of Approval or Rejection DEC181996 i 8 1996 Certificate or Designation ignation No. 0K2R112L Signature of Authorized Individual Coma ‘....a FAA Form 337 02401 SDNYGIvl_02754086 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241008 EFTA01326601 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be corn/sat/We with all previous alterations to assure continued conformity with the applicable airworthinesi requirements. 8. Description of Work Accomplished (If more space is requited. attach additional sheets. Identify with aircraft nationality and registration mark and dale work completed.)- ... Removed all 10 existing Aircraft Modular Products cabin chairs P/N: 1250-1399-001; P/N: 1250- 1399-002, forward (2 ea.), center group (4 ea.), aft group (4 ea.), retractable tables (6 ea.) and (2 ea.) left and right forward cabin cabinets at F.S. 176. Installed six new single ISO C39a Aircraft Modular Products chairs, two double TSO C39a Aircraft Modular Products chairs and a Tosington side facing three place TSO C39a, Type I divan reconfigured to 13 place passenger cabin in accordance with K-C Aviation, Inc., floor plan drawing GIV-25-05-200, sheet 1 dated 10/29/96. Seats and divan are installed in the conventional manner using new seat track over existing aircraft seat track in accordance with K-C Aviation STC SA1266GL approved drawing GIV-25- 50-205, sheet 1, revision B in the positions listed below: #1 IJH P/N: 2524.014(-866C) Aft Facing F.S. 173 #1 R/H P/N: 2524.014(-866D) Aft Facing F.S. 173 #2 L/H P/N: 2524.014.01(-874B) Forward Facing F.S. 225 #2 R/H P/N: 2524.014.01 (-874A) Forward Facing F.S. 225 #3/4 L/H P/N: 2524.015(-167C) Aft Facing F.S. 272 #5/6 L/H P/N: 2524.015(-1678) Forward Facing F.S. 326 #7 R/H P/N: 2524.014(-866A) Aft Facing F.S. 370 #8 R/H P/N: 2524.0141-866A) Forward Facing F.S. 424 Divan P/N: T480-40 Side Facing F.S. 397 All seats installed with new ISO C-22F color coordinated seat belts by C & M Marine. Details of additional interior components depicted and installed in accordance with floor plan drawing are approved on separate FAA form 337's. The floor plan drawing will be referenced for location purposes. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. Fasteners torqued using AC.43.13-1A chapter 5 as a guide. END ❑ Additional Sheets Are Attached 0 U.S. GOVERNMENT SMINTINO OF NCI: 1M-769-012/60157 SDNY_GM_02754087 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241009 EFTA01326602 in Vat IS g Lt.,. I,.. MA 4 - 6 Iiigrframe Ansa await f • i • OR REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No. 21200020 For FAA Use Only Office Identificatiory is, alif...1 NSTRUCTIO NS: Print or type all e ermicitspositiorrof this . for each such violation (Section 901 ries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions is required by law (49 U.S.C. 1421). Failuret0 Alpert can result Ina civii penaity not to excee351800 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace u ModeL• -IV Serial No. 1085 Nationality and Registration Mark N88GA z Owner Name (As shown on registration certificate) Coca-Cola Enterprises, Inc. Address (As shown on registration certificate) 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described In Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. U.S. Certificated Mechanic OK2R112L K-C Aviation, Inc. Foreign Cann-mated Mechanic 301 Discovery Drive y Certificate:1 Racal/ Station Appleton, WI 54915 ' Manufacturer O. I certify that the repair and/or alteration made to the un have been made in accordance with the requirements furnished herein Is true and correct to the best of my t(s) identified in item 4 above and described on the reverse or attaChmentS hereto of Part 43 of the U.S. Federal Aviation Regulations and that the information knowledge. Date DEC 18 1996 Signature of Authorized lndiv ual 7. Approv or Return To Service Pursuant to the authority given persons specified below. t unit identified in item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is (APPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 8 1996 Certificate Or Oesignation No. OK2R112L Signature of Authoriz Indi dual CI A,-4-, c • FAA Form 337 02441 SDNYGIvl_02754088 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241010 EFTA01326603 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Wotk Accomplished of more Space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Fabricated and installed the following new interior components in accordance with K-C Avlation, Inc., Floor Plan Drawing GIV-25.05-200, sheet 1 and the below listed Structural Drawings: GIV-25-02-203 Sheet 1 Rev. - Subwoofer Installation GIV-25-01-209 Sheet Rev. - Game Table Leaf Assembly GIV-25-02-209 Sheet 1 Rev. - Enflight Table Installation GIV-25-09-210 Sheet 1-3 Rev. - Galley Aft Right Modification GIV-25-10-210 Sheet 1-2 Rev. - Galley Aft Left Modification GIV-25-07-223 Sheet 1 Rev. - Aft Divan Cabinet Installation GIV-25-08-223 Sheet 1 Rev. - Forward Divan Cabinet Installation GIV-25-06-226 Sheet 1-5 Rev. - Credenza Details and Installation GIV-25-53-286 Sheet 1-2 Rev. - Conference Table Dual Pedestal Installation Subwoofers installation consists of four units installed below cabin window ledges at the following locations: two each forward left and right cabin F.S. 163; one each right aft cabin F.S. 350 and one each right aft cabin 436. Fabricated and installed three stowable game tables in the following locations: two each left and right forward cabin F.S. 198; one each right aft cabin F.S. 397. Fabricated and installed new manual height adjustable conference table in center left cabin F.S. 299. Fabricated and installed new credenza cabinet in right center cabin extending from F.S. 255 to F.S. 345. Credenza contains six drawers in center for miscellaneous storage and hinged compartments on each end for pillow and blanket storage. Fabricated and installed new divan forward and aft divan armrest cabinets located at F.S. 355 and F.S. 434. Cabinets contain drawers for miscellaneous storage. Modified left galley to include removal of decanter cabinet, replacing Sharp microwave oven P/N: R-1 M53 with new larger Tappen unit P/N: TMS083U1W and replaced 13" Hitachi TV monitor P/N: CT1386B with new 14" Baker LCD monitor P/N: TW1400. Modified right galley removing hot cup dispenser, replacing circuit breaker panel, adding the following equipment: new Krups coffee maker, hot and cold water spigot and sink, Nordskog Hi￾Temp oven P/N: 50231 and new trash receptacle. New trash receptacle is in compliance with the flammability requirements of 14CFR25 (part 25), paragraph 25.853(h), amendment 25-83. DER approval is in accordance with 8110-3 form dated 12/18/96 by A Duncan, CHI-424. Electrical aspects covered separately. Cabin interior compartment placards description detailed in K-C Aviation drawing GIV-25-01-218 and layout per drawing GIV-25-04-218. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC 43.13-1A chapter 6 as a guide. Weight and balance accomplished using AC43.13-1A chapter 13 and the aircraft manufacturer's weight and balance manual as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END 0 Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1192-769-012/60157 SDNY_GM_02754089 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002410I I EFTA01326604 0 . I ; Vi L3 MAJOR US Doormen Mitenspermson - 6 Lymnr . Fare' krtallen An REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved ome No. 2120-0020 For FAA Use Onty Office Identificatiwi NJ3 itlUCTIONS: -for Ctla tU Print or type alt entries. ispositicusoLthWoraatiisseairt each such violation (Section 901 See FAR 43.9. FAR 43 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for instructions Is required by law (49 U.S.C. 1421). Failure to report can result In a civil penalty not to exceed $1.000 federal Aviation Act of 1958). Make Gulfstream Aerospace Model G-IV 1. Aircraft Serial No. 1085 Nationality and Registration Mark N88GA Z Owner Name (As shown on registration certificate) Coca-Cola Enterprises, Inc. Address (As shown on registration certificate) 2500 Windy Ridge Parkway Atlanta, Georgia 30338 ,I.t_j,:,,,,rminajtmiu l 3 4;enotreers, .. ForFAmp .. . tf. ,v4H44.h.7ipptitheipteleaFivvom rt REQUIREMENTS DESCRIBED INSPECTION SECTION ne-re zl AND IS APPROVED AIRCRAFT, SUBJECTTO BYA PERSON AUTHORIZED 7 1 In FOR THE CONFORMITY IN miciEsr -.,:r ABOVE 43 4. Unit Identification FAA NIKE I-SDO Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. . US. Certificated Mechanic CIK2R112L K-C Aviation, Inc. Foreign Certificated mechanic 301 Discovery Drive x Certificated Repair Station Appleton, WI 54915 Manufacturer D. I certify that the repair andtor alteration made to the un have been made in accordance with the requirements furnished herein is true and correct to the best of my knowledge. t(s) identified in item 4 above and described on the reverse or altachrnemts hereto of Part 43 of the U.S. Federal Aviation Regulations and that the information Oate DEC 0 9 1996 Signature of Authorized Individual c 7. App for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is Ck.PPROVED CI REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other Meal BY FAA Designee KRepair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 8 1996 Certificate or No. Designation2R112L CIK Signature of Authorized Individual Qs...-. cd-jd￾FAA Form 337 11206) SDNYGIvl02754090 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241012 EFTA01326605 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required attach additional sheets. Identify with aircraft nationality and registration park and date work completed.) Modified existing forward right vestibule crew cabinet, F.S. 163 in accordance with K-C Aviation, Inc., Structural Drawing GIV-25.05-216, sheet 1 and PS100-26.04-600. Cabinet rework consists primarily of the following changes: Compartment #1 (Upper): 1) Removed existing upper cabinet compartment tambour door installing new hinged door 2) Relocated existing bleed air temp indicator in upper portion of compartment adjacent existing data loader and removed existing water tank from lower portion of compartment. Area now used for miscellaneous storage. 3) Compartment placarded 4.0# maximum Compartment #2: 1) Removed existing Proctor Silex coffee maker P/N: A607 installing new Krups auto fill maker P/N: 321 to existing slide out tray. 2) Installed new Baker 14' LCD TV monitor aft facing and adjacent to coffee maker. Monitor is retained in the cabinet by a removable shroud assembly, fabricated from Norlam aluminum sandwich panel P/N: NL610-10111-375, .75" X .75" X 0.050" 2024-73511 extruded aluminum angles and TYE 2004 thru inserts and TYE 2001 potted into cabinet. Compartment #3 (Drawer): 1) No changes 2) Compartment placarded 5.0# maximum Compartment #4 (Drawer): 1) No changes 2) Compartment placarded 10.0# maximum Compartment #5 (Bottom): 1) Removed two existing drawers installing new single drawer to fit compartment. 2) Compartment placarded 20.0# maximum Replaced all compartment drawer and door latches with new Actron positive type latches P/N: A23060-9 and A23551-35. Electrical aspects covered separately. All metal fabrication practices per K-C Aviation Process Specification 106. All threaded fastener installations per K-C Aviation Process Specification 105. Fabrication of bulkheads, cabinets, drawers and doors per K-C Aviation Process Specification 116. Cabin interior compartment placards description detailed in K-C Aviation drawing GIV-25.01-218 and layout per drawing GIV-25-04-218. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC 43.13-1A chapter 6 as a guide. Weight and balance accomplished using AC43.13-1A chapter 13 and the aircraft manufacturer's weight and balance manual as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END ❑ Additional Sheets Are Attached nu.s. aote vitamin T PRINTING OFFICE 1991-769-01 5/40157 SDNY_GM_02754091 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241013 EFTA01326606 . "; \1121 1 • JAN — 6 I997 OR REPAIR AND ALTERATION (AM , Powerplant, Propeller, or Appliance) ackremmenew, Form Approved OMB No. 2120-0020 For FAA Use Only Office Identifies,' ic)gn lig INSTRUCTIONS:Print or type all entries. See FAR 43.9. FAR 43 Appendix Et and AC43.9-1 (or subsequ nt revision thereof) for instructions anddisposition of this form. This report is required by law (49U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act 01 1958). 1. Aircraft Make Gulf stream Aerospace Mode IG-IV Serial No. 1085 Nationality and Registration Mark N88GA 2 . owner Name (As shown on registration certificate) Coca-Cola Enterprises, Inc. ,._ , Address (As shown on registration certificate) 2500 Windy Ridge Parkway Atlanta, Georgia 30338 .,,..,,;.., „,...,, „„,„...,.,,,,,,..„.0‘.,....wicil miziks:IN 3. For FAA Urie(Gartel IFS WITH THE APPI CAR) F AIRIANIRTHIMFRR REQUIREIviENTS AND IS APPROVED DESCRIBED AIRCRAFT, SUBJECT TO INSPECTION BY A PERSON AUTHORIZED SECTION 7- DATE. ea- SIGNKRIRF. FOR THE ABOVE CONFORMITY IN F 43, 4. Unit Identification FAA MKE FSDO S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As clisSeribed in hem 1 OM") X . POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Cerli icate No. K-C Aviation, Inc. 301 Discovery Drive Appleton, WI 54915 U.S. Certificated mechanic C1K2R112L Foreign Certificated MeChailiC x Certificated Repair station Manufacturer D. I certify that the repair and/or alteration made to the can t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein Is true and correct to the best of my knowledge. Date DEC 0 9 1996 Signature of Authorized Individual (" ......A. . 7. Ap al for Return To Service Pursuant Administrator BY to the authority given persons specified below, the unit identified In Item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is GAPPROVE0 0 REJECTED FAA Flt. Standards Inspect or Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport Canada AInvorthiness Group °aloof Approval or Rejection 18 1996 Certificate or Designation No. 12K2R112L Signature of Authorized Individual DEC C)S`" d e"-" .• FAA Form 337 02.8e) SDNY_CM_02754092 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_0024I0I4 EFTA01326607 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued LOnlOrmily with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required attach additional sheets. Identity with aircraft nationality and registration mark and dale work completed) Removed existing cabin window ledges and lower sidewalls, modified existing vestibule, cabin, aft galley headliner and existing floor conditioned air ducts, installed new window desiccant system, upper sidewall speakers, new ledges and lower sidewalls and two additional oxygen presentation units as detailed below. Interior components located in accordance with K-C Aviation, Inc. floor plan drawing GIV-25-05-200, sheet 1. Cabin peripheral interior rework extends from forward cabin bulkheads F.S. 155 to aft cabin bulkheads F.S. 445. Modified by sectioning existing cabin headliner into five 48.00" long sections using the following K-C Aviation drawings: GIV-25-50-213, sheet 1, rev. A - Headliner Vestibule Assy and Installation; GIV-25-50-213, sheet 2, rev. A - Headliner Main Cabin Bracket Details; GIV-25-01- 213, sheet 1 -Headliner Support Bracket Installation. The five panels interlock together on the forward and aft ends when installed in the aircraft with a flange and slot assembly fabricated from .040" 2024-T3 aluminum flat stock and 5 slots fabricated from 0.75 X .025" X .075" 2024-T3511 extruded aluminum Z angle. The headliner is retained in the aircraft on the outboard edges using existing isolator mounting provisions and ten 34.00" long support angles (5 ea. side) fabricated from 0.063" 2024-T3 aluminum installed between each existing headliner bracket. Added two new Scott dual oxygen presentation units P/N: 833-610 in left headliner F.S. 286.5 and 307.5 and two duel presentation units, one left valance F.S. 213.81 and one in right valance F.S. 213.81. All new units are plumbed to existing system. Additional presentation unit installation and seating configuration does not exceed limitation requirements of Aero Interiors continuous flow supplemental oxygen system STC SA4416NM. Fabricated and installed 11.0" X 5.0" light bracket assemblies in vestibule between F.S. 85.0 and F.S. 97 (1 ea.) and galley (2 ea.) using K-C Aviation, Inc. drawing GIV-25-50-213, sheet 4, rev. A - Headliner Aft Galley Assy and Installation. Each bracket assembly is fabricated from .040" 2024-T3 aluminum. Each assembly is retained by four brackets fabricated from 1" X 1" X .050" 2024-73511 extruded aluminum L angle riveted or hylocked to adjacent frames. Bracket assembly provides mounting surface for dome style lights. Fabricated and.installed mounting provisions for five upper sidewall entertainment system speakers on each side of the cabin between each cabin window, F.S. 200, 250, 301, 350 and 395 in accordance with K-C Aviation Inc., drawings GIV-25.02-211, sheet 1 & 2 - Upper Sidewall Speaker Installation. Each assembly consists two formed angles and four brackets constructed from 0.063" 2024-T3 aluminum to accommodate the 8.50" X 5.00" Baker HF93 speaker assemblies. Each speaker is retained to the aircraft by the four angle brackets riveted to the adjacent frames, four each isolator mounts P/N: 100147-40-062; four each MS21059L3 nutplates and MS227039-1 screws, two each formed angles and hardware provided by the speaker manufacturer. Fabricated and installed replacement left and right ledges using K-C Aviation, Inc., drawings GIV￾25-51-203, sheet 2, rev. A - Lower Sidewall Ledge Assembly and Install; GIV-25.04-203, sheet 1 - Ledge VIP Panel Installation; CL600-25-17-203, sheet 1 - Ledge Lid And Storage Compartment Install Installation consisting primarily of four sections fabricated from NL610-10122-500 and - 250 Norlam sandwich panel; two left and right forward and one right aft section with retractable table provisions; left aft section behind divan. Each section is secured to each side of the cabin below the window line using TYE 2004A3-500 and TYE 2001-08-10 thru and threaded inserts potted into ledge, isolators P/N: B-532-1 and MS hardware into a formed aluminum assembly consisting of a full length intercostal, aluminum gussets, angles, webs and gusset plates riveted together and to the aircraft structure. Ledges contain cup holders and electrical membrane switches at seating locations, VIP panel and Magnastar handset and cell phone storage at #2 left and right forward cabin seats. The lower sidewall panels are fabricated from NL 610-10111-250 Norlam sandwich panel and close-out area below ledges to existing floor conditioned air duct. Panels are sectioned for easy access and retained by the ledge end cap and an aluminum angle running full length of ledge. The lower end of sidewall panel is retained using an aluminum angle blind riveted to existing conditioned air duct and Velcro loop and hook fastener material. rif Additional Sheets Am Attached *U.S. GOVERNMENT PRINTING OFFICIO IS112-761-0ISNSOIS7 SDNY_GM_02754093 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241015 EFTA01326608 Gulfstream GIV, S/N: 1085 N88GA Page 2 Reworked existing floor length left and right cabin conditioned air ducts due to removal of previously installed cabin stowable tables at F.S. 206, 297 and 395 in accordance with K-C Aviation, Inc., drawing GIV-25-01-207, sheet 1 - Conditioned Air Heat Duct Repair. Rework consists of closing out upper duct recesses using a 0.040" 2024-T3 aluminum panel blind riveted with NAS9301B-4 rivets and PR1422 sealant. Relocated existing cabin temperature sensors P/N: 926485-1-1 in accordance with floor plan drawing. Right forward temperature sensor moved from F.S. 219 to F.S. 250 and left aft moved from F.S. 436.5 to 345. Fabricated and installed new left and right cabin window desiccant systems using K-C Aviation, Inc., drawing GIV-25-51-203, sheet 6, rev. A • Lower Sidewall Window Desiccant System Installation. Each desiccant system is constructed of 2.0" X 21.0" long Excelon tube bonded with 2.0" PVC end caps bonded on each end with PCV adhesive. One end cap contains a hose barb fitting P/N: 125HBL4-4 the other with an MS 20913-4D fill plug. Desiccant tubes are mounted below window ledges in lower sidewalls at F.S. 200 with two MS21919WH32 clamps and a bracket fabricated from 0.050" 2024-T3 aluminum riveted to the aircraft structure. Each desiccant tube is plumbed to each window with 5052-0 0.25" tubing, Tygon polyethylene tube, Nalgene nylon TEE P/N: 582707C/15221CA and Y P/N: 582747C/13366CA fittings as required. Performed an oxygen drop-out test in accordance with Gulfstream Aerospace Maintenance Manual chapter 35. Electrical requirements for above installations covered on separate form 337. All metal fabrication practices carried out per K-C Aviation Process Specification 106. All threaded fastener installations carried out per K-C Aviation Process Specification 105. Riveting accomplished using AC43.13-1A chapter 2 as a guide. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC43.13-1A chapter 6 as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END SDNY_GIvl_02754094 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241016 EFTA01326609 SDNY_GM_02754095 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002410 I 7 EFTA01326610 migrgoweE• C. • - "'"— -- lii US ontra— 6 ici l tJOR i lit g. iliviniten 'I REPAIR AND e, Powerplant, Props !' fRato3N6 mg It • or Appliance) II' i' La I IL' : Form Approved OMB NO.2120-0020 For FAA Um Only Office identification 6 4 ia INSTRUCDO.NS:RsinSeotypea entries. See FAR 43.8 FAR 4 Appendix B. and AC 4.371-"Mu s7Vertu —ird nt revision thereof) for instructions disposition of this form. This report is required by law (49U.S.C. 1421). Failure to report can result i a civil penalty not to exceed $1.000 for each such violation (Section gat Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace M°deb-IV Serial No. 1085 Nationality and Registration Mark 2. Owner Name (As shown on registration cenifkate) Coca-Cola Enterprises, Inc. Address (As shown on registration cetlificatel 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA Use Only 'The data/alteration identified herein complies with the applicable airworthiness requirements and is approved for the above discribed aircraft to conformity inspection by a person authorized in FAR 43, Section 43.r. Date \ 7 \s::\‘,0 FAA \ Inspector . k—L GL13 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive Appleton, WI 54915 V.S. Certificated Mechanic QK2R112L Foreign Certificated Mechanic x Cenificated Repair Station Manufacturer D. I certify that the repaira/xi/or alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of P n 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date • DEC 09 1996 Signature of Authorized individual 7. Approv r Return To Service Pu suant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and s ja,APPROVED 0 REJECTED FAA FIL Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 18 1996 Certificat atie or Desnig on No. QK2R112L Signature of Authorized Individual gsn,o FAA Form 337 one) SDNY_ GE/1_02754 096 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024I0I8 EFTA01326611 NOTICE • • Weight and balance or operating limitatiorrafangesshalf qe entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished of more space Is required. attach additional sheets. Identity with akeraff nationality and registration mark and date work completed.) Remounted interior cabin door at F.S. 155 to hinge from right side. Door installed with new hinge assembly fabricated in accordance with K-C Aviation, Inc., drawing GIV-25-50-229, revision A, sheet 10. Door is retained in the open position by a door stop installed on lower vestibule storage cabinet. Fabricated and installed mounting tray for HPA/LNA on right lower cabin sidewall F.S. 250.5 in accordance with K-C Aviation, Inc., structural drawing GIV-25-51-203, sheet 7. Mounting tray is constructed from 0.040" 2024-T3 aluminum sheet. Tray is mounted using MS24693-10 screws and MS21059L3 nutplates to the aircraft structure between adjacent frames using brackets fabricated from 0.050" 2024-T3 aluminum sheet riveted to the aircraft structure. Fabricated and installed mounting trays for CDBR-2 on center right lower cabin sidewall F.S. 238 and CDBR-2 on left aft cabin below ledge, F.S. 430 in accordance with K-C Aviation, Inc., structural drawing GIV-23.02-301, sheets 1 & 2. Trays are constructed from 0.040" 2024-T3 aluminum mounted to the aircraft structure with four brackets fabricated from 0.050" 2024-T3 aluminum with rivets and MS hardware. Fabricated and installed miscellaneous electrical component mounting trays located on left lower forward cabin below ledge F.S. 170 and right forward cabin behind coat closet F.S. 127. Trays are primarily constructed from 0.050" 2024-T3 aluminum sheet mounted to the aircraft structure with MS hardware to 2.75" X 4.5" brackets fabricated from 0.050" 2024-T3 aluminum sheet riveted to frames or stringers as required. Overall dimensions of left trays (2 ea.) at F.S. 170 are 6.5" wide and 16" wide; 3.5" wide and 12.0" long. Overall dimensions of right forward tray F.S. 127 is 9.0" wide and 19.5" long. Trays provide mounting surface for cabin lighting power supplies, terminal strips and entertainment system controllers. Fabricated and installed new replacement lavatory vanity fluorescent accent light bar, F.S. 502. Unit is constructed from NL610-10111-250 Norlam aluminum honeycomb panel contoured to headliner extending from lavatory door to vanity top. Overall dimensions are 2.125" wide and 58" long. Light bar is mounted to the existing bulkhead using three 1.25" X 1.0" X 0.063" 2024-T3511 extruded aluminum L brackets, TYE threaded inserts potted into bulkhead, MS screws and nutplates. The light bar contains mounting provisions for two fluorescent tubes. Unit constructed using K-C Aviation Process Specification 106 and fasteners installed per Process Specification 105. Fabricated and installed feed thru behind entertainment cabinet for micellaneous electrical cable routing in accordance with K-C Aviation drawing GIV-25-15-293, sheet 1. Fabricated and installed replacement left and right life lines only. Lines fabricated in accordance with K-C Aviation emergency equipment and location drawing GIV-25-00-222, revision C, sheet 1. Life lines attach to existing seat tracks below emergency exits and when in use, to existing eye mounts on each wing. ❑ Additional Sheets Are Attached GOVOINMENT PRINTING OFFICE: IM -769-012/60167 SDNY_GM_02754097 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241019 EFTA01326612 Gulfstream GIV, S/N: 1085 N88GA Page 2 Fabricated and installed a new cockpit curtain and track assembly, F.S. 73. Curtain is constructed from 100% wool pleated and sewn to the dimensions of 67.0" high and 24.0" wide. Curtain slides with nylon curtain guides on a curtain track P/N: 9046 fastened to the headliner MS hardware. Curtain is retained in the open position with two straps fabricated from same material as curtain and snaps. Electrical aspects covered separately. Cabin interior compartment placards description detailed in K-C Aviation drawing GIV-25.01-218 and layout per drawing GIV-25.04-218. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC 43.13-1A chapter 6 as a guide. Weight and balance accomplished using AC43.13-1A chapter 13 and the aircraft manufacturer's weight and balance manual as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END SDNYGIvl_02754098 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241020 EFTA01326613 SDNY_GM_02754099 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241021 EFTA01326614 T. • i • q I I il . • : JAN — 6p.?7, il,IAJOR REPAIR AND ALTERATION t0000101 (Airframe, Powerplant, Propeller, or Appliance) ;v 91imb 0, iF rM Approved OMB NO. 2120-0020 Use°ifil I Office IdeF:trifiFcAAa ri..13 tsrent or type of this form. such violation (Section 43.9, FAR 43 Appendix B.andAC 43.9-1 (or subsequent revision thereof) tor instructions by law (49U.S.C. 1421). Fa lure to report can result Ina civil penalty not to exceed S1,000 Act of 1958). , OCTieff4S-: and disposition for each all entries. See FAR This report is required 901 Federal Aviation 1. Aircraft Make Gulfstream Aerospace ModelG-IV Serial No. 1085 Nationality and Registration Mark N88GA 2 . Owner Name (As shown on registration certificate) Coca-Cola Enterprises, Inc. Address (As shown on registration certificate) 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA UslrOMt I fUrtl-i ti-U4i 5...filintiJFtliri lOhlq I I hitU FIEHIN t•UlYie Itb Wit H I It AYFLIUMULt AIM/KA-CI HIrsik&S REQUIREMENTS AND IS APPROVED FOR THE ABOVE DESCRIBED AIRCRAFT, SUBJECT TO CONFORMITY INSPECTION BY A PERSON AUTHORIZED IN F 43, SECTION 43.7. 4. Unit IdenTfiggiart-11VI Vie StuNAt UR . Unit Make Model FAA MKE FS • • Serial No. Repair Alteration AIRFRAME (As described in !tern 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive Appleton, WI 54915 V.S. Certificated mechanic QK2R112L Foreign Certificated Mechanic y certificated Repair Station manwactunw O. I certify that the repair and/or alteration made to the un t(s) identified in item 4above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my knowledge. Date DEC 0 9 1996 Signature of Authorized Individual 7. App for Return aToService Pursuant Administrator BY to the authority given persons specified below, the unit Identified in item 4 was inspected In the manner prescribed by the of the Federal Aviation Administration and is ikAPPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 18 1996 Certificate or Designation No. QK2R112L Signature of Authorized Ind idual C stsre. d . FAA Form 337 112•0 SDNY_GM_02754100 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241022 EFTA01326615 NOTICE Weight and balance or operating limitation changes shall be entered in the approprlate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (lf more space is required, attach additional sheets. identity with aircraft nationality and registration mark and date work completed.) Reworked existing left vestibule entertainment cabinet at F.S. 144 as follows: Removed the following equipment: 1) Stereo cassette deck, Sony P/N: TC-WR808M 2) Stereo amp, Sony P/N: TA-808M 3) AM/FM tuner, Sony P/N: ST-707RM 4) CD player, Sony P/N: CDP-5107 5) Video switch, ASINC P/N: 912001 6) VCR, Panasonic P/N: F85A30987 7) Video monitor, Sony P/N: PVM-2030 8) Video distribution amp, United P/N: PD-6 9) Removed upper shelf and compartment doors retaining forward and aft bulkheads. 10) Relocated existing data loader P/N: DL-800 from upper cabinet to right vestibule upper crew cabinet. Fabricated and installed new replacement compartment cabinet to accommodate new ententainment equipment and provide miscellaneous storage. Compartment cabinet peripheral is conitructed.,from,ML610-10111-V5 Aluminum honeycomb panel assembled together in accOrdance-withi0C Aviation PrdbUOPecification 116. Overall dimensions of cabinet are 34.5" high, la".5" wide and 24.125" deep. Cabinet contains two compartments, an upper removable entertainment cabinet fabricated similarly to compartment cabinet using NL610-10111-250 aluminum honeycomb panel. Cabinet dimension are 17.25" high, 18.5" wide and 14.5" deep and contains mounting provisions for the following new equipment: 1) CD magazine or tape storage 3) AM/FM cassette player, Alpine P/N: TDA7552 3) CD changer, Sony P/N: CDX-91 4) CD controller, Sony P/N: RM-X59RF 5) VCR, Panasonic P/N: PV4662 Lower compartment dimensions are 16.0" high. 18.0" wide and 24.125" deep and is used for miscellaneous storage. The overall compartment cabinet is retained to the existing lower compartment structure and bulkheads using MS hardware and threaded inserts installed per K-C Aviation Process Specification 105. Entertainment and miscellaneous storage compartment are closed out with a hinged doors ancActron positive type latches. Fabricated and installed a new tapes and CD storage drawer in lower compartment. Overall dimensions are 5.0" high, 18.5" wide and 23.0" deep. Door is hinged with Brusso L23 knife hinges and retained in the closed position using an Actron positive type latch P/N: A23060-9. Entertainment cabinet compartments maximum placarded weights are as follows: 1) Upper CD magazine and tape storage compartment - 5.0 Lbs. 2) Miscellaneous storage compartment - 25.0 Lbs. 3) Fitted tapes/disc storage drawer - 25.0 Lbs. Electrical aspects covered separately. All metal fabrication practices per K-C Aviation Process Specification 106. All threaded fastener installations per K-C Aviation Process Specification 105. Fabrication of bulkheads, cabinets, drawers and doors per K-C Aviation Process Specification 116. Cabin interior compartment placards description detailed in K-C Aviation drawing GIV-25-01-218 and layout per drawing GIV-25.04-218. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC 43.13-1A chapter 6 as a guide. Weight and balance accomplished using AC43.13-1A chapter 13 and the aircraft manufacturer's weight and balance manual as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END 0 Additional sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1912-769-0I2/601S7 SDNY_GM_02754101 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241023 EFTA01326616 I MAJOR REPAIR AND ALTERATION uS For — 6 Pgirtramd, Powerplant, Propeller, or Appliance) , halt 'I • ' Onkel*, Form Approved OMB No. 2120-0020 FAA Use Only Office Identific2o22; _INSTRUCTIONS: Print or type all ntries. See FAR 43.9. FAR 43 Appendix B.and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of thirferTrii. port is required by law 09 U.S.C. 1421). Failure to report can result in a civil penalty net to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Al ft Make GULFSTREAM AEROSPACE model GIV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA, GA 30338 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity SlatomeM A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C AVIATION INC. 301 DISCOVERY DR. APPLET0N, WI 54915 U.S. Certificated Mechanic QK2R112L Foreign Certificawd mechanic X1 Cenificated Revak Station . manufacturer 0. I Certify that the repair andior alteration made tothe un fts) identified in item4 above and described on the reverse or attashmentshereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date DEC 16 1996 Signature of Authorized Individual 1.50-nitle,-te 4., 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is (1) APPROVED 0 REJECTED FAA Fit. Standards i Inspector Manufacturer I Other (Sandy) Inspection Authorization BY FAA Designee XX Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Remotion DEC 1 8 1996 Certificate or Designation No. OK2R112L Signature (loin. of Authorized Individual tlLZ2 FAA Form 337 .12 or SDNYGtvl02754102 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241024 EFTA01326617 NOTICE Weight and balance oroperating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished pl more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Installed a GTE/Magnavox C-2000 Digital Airborne Telephone System consisting of: 1 Ea. Air Radio Telecommunications Unit (ARTU), P/N 724855-801 1 Ea. ARTU Rack, P/N 724868-802 1 Ea. Duplexer, P/N 620317-1 3 Ea. Cabin Data Bus Repeater (CDBR-1), P/N 724864-801 '1 Ea. Cabin Data Bus Repeater (CDBR-2),'P/N 902205-803 1 Ea. CAS Unit, P/N 725256-801 1 Ea. Analog Interface Unit (AIU), P/N 724986-801 4 Ea. Phone Assembly, P/N 724866-801WH, -805PL, & -807PL 1 Ea. Antenna, P/N 902131-2 Two Global Wulfsberg Flitefone VI Radio Telephone Systems were removed to facilitate this installation. Removed components consist of: 2 Ea. GWS RT-18D Transceivers, P/N 400-0125-000 2 Ea. GWS WH-I0 Flitefone VI Handsets The newly installed antenna is located on the underside fuselage at FS 100 as per KCA Structural Drawing: Radio Telephone Antenna Installation, 1159-23-01-301, sht. 1, of which the structural aspects are DER approved by M. Lieblich, FAA DER SW-811. The C-2000 system wiring accomplished as per K-C Aviation Drawing: Radio Telephone, GIV-31085-23-98, of which the electrical/electronic aspects are DER approved by N. Kopesky, CHI-262. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conduc￾tor shielded wire meets MIL 27500. All work done IAW AC43.13-2A Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END ❑ Additional Sheets Are Attached GU.5. GOVERNMENT PRINTING OPPICC: It02-769-0I2/60I37 SDNY_GM_02754103 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241025 EFTA01326618 ir g 14/5-7 ! • • ' ' . ! I MA,JOR 1 6 I;TAiriniOi , • REPAIR AND ALTERATION , Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification. R ./.1 INSTRUCTIONS:Print or type :ties. Se•FAR 43.9. FAR 40 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions —enddisposition of thisiormitt rt is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty nol to exceed $1.000 tor each suc violation (Section 901 Federal Aviation Act of 1958). 1 .Aircraft Make GULFSTREAM AEROSPACE Model GIV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA, GA 30338 3. For FAA Use Only 4. Unit Identification 5. Tyr). Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERFLANT PROPELLER APPLIANCE Type Manufacturer & Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C AVIATION INC. 301 DISCOVERY DR. APPLETON, WI 54915 U.& Certificated Mechanic QK2R112L Foreign Certificated Mechanic XX Certificated Repair Station manufacturer D. I certify that the repair and/Or alteration made to the un Its) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information - furnished herein is true and correct to the best 01 my nowledge. Date DEC I 6 1966 Signature of Authorized Individual CFP6424, A t t , Z,e r 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the mariner prescribed by the Administrator of the Federal Aviation Administration and is 01 APPROVED 0 REJECTED I FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY I FAA Designee 111 XX Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 181998 Certificate or Designation No. QK2R1I2L Signature of Authorized Individual C14,-. , ' *- ,_ FAA Form 337 .12 MP) SDNYGivl_02754104 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241026 EFTA01326619 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (II more space Is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Installed an Allied Signal Satellite Data Communications System (SDCS), interfaced to the existing Airborne Flight Information System (AFIS). The AFIS system is integrated with the GAC installed Honeywell Flight Management Systems providing complete flight plan and weather information through self-contained VHF COMM data link with the Global Data Center. The SDCS is interfaced to the AFIS and provides additional cabin/cockpit communication capabilities. Installed SDCS system components include: 1 Ea. Satellite Comm Unit (SCU), P/N 153-017311-01 1 Ea. SCU Antenna, P/N 121-017537-01 (Sensor P/N S65-8282-101) 1 Ea. HPA/LNA, P/N 153-017310-01 The SCU Antenna is installed as FS 265 in accordance with KCA Dallas structural drawings; 447-5338, of which the structural are DER approved by M. Lieblich, SW-811. The SCU is located in the R/H radio rack extension and the HPA/LNA is located in the R/H cabin sidewall at FS 250 on existing structure. Refer to KCA Drawing: AFIS/SDCS, GIV-31085-34-63, of which the electrical/electronic aspects are DER approved by N. Kopesky, CHI-262. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conduc￾tor shielded wire meets MIL 27500. All work done IAW AC43.13-2A Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END 0 Additional Sheets Aro Attached *U.S. 00VCIIHMENT PRINTINCt OIPICI 1192-70-012/10157 SDNY_GM_02754105 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241027 EFTA01326620 rirc.-7,77 . O., i . 3M - 6 1.997M or won (Akira onmsan • , REPAIR AND ALTERATION of owerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identificaip2 i i INSTRUCTIONS:Print or type a en les. See FAR 43.9. FAR 43 Appendix B. and AC43.9-1 (or subsequ nt revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only ',The dna Ident if fed herein compiles with the applicable airworthiness requirements oral I. approved for the above described aircraft subject to conformity inspect in by a parsers authorized in FAR 43, Section 43.7". Date DEC 1 0 ME IAA Inspecte 61.13 4. Unit Identification 8. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described In horn 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive A ppleton, WI 54915 US. ceni Heated Mechanic QK2R112L Foreign Cenificated mechanic X Cenificated Repair Station Manufacturer D. !certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on t e reverse orattachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date DEC 1 0 1996 Signature of Authorized Individual 47-ser/V er,IZZ---• 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XX APPROVED CI REJECTED FAA Fit Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 8 1996 Certificate or Designation No. QK2R112L Signature of Authorized Incrvidual cap.,- • FAA Form 337 ono SDNYGlvl_02754106 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241028 EFTA01326621 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be conipatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Modified the previously installed Galley and Cabin electrical system by removing previously installed equipment and wiring and installing new equipment and associated wiring. Installed the following equipment: lea Nordskog HI Temp Oven P/N: 50231L. lea Microswitch Leaf Actuator P/N: JV-26. lea Rotron Fan P/N: FS24H3. lea Tappan Microwave Oven P/N: TMS083E1S0. lea Krups Coffee Maker P/N: Pro-Cafe. 2ea Grimes Light Assembly P/N: 34170-1. lea Audio Int. High Current Control P/N: MSM285. lea Audio Int. Aft Lav Switch Panel P/N: SPS-4-1-1759. lea Audio Int. Aft VIP Switch Panel P/N: SPS-5-3-1761. lea Audio Int. FWD VIP Switch Panel P/N: SPS-5-3-1753. lea Audio Int. Divan Switch Panel P/N: SPS-4-1-1762. lea Audio Int. Divan Switch Panel (Master) P/N: SPS-4-1-1758. lea Audio Int. R/H Galley Switch Panel P/N: SPS-6-2-1754. 2ea Audio Int. Credenza PSU Switch Panel P/N: SPS-3-1-1757. 4ea Audio Int. Passenger Service Unit Switch Panel (PSU) P/N: SPS-4-1-1756. 4ea Audio Int. PSU Switch Panel (Master) P/N: SPS-4-1-1755. lea Audio Int. Vestibule Switch Panel P/N: SPS-6-1-1760. Wiring for the newly modified / installed Galley and Cabin electrical systems is per K-C Aviation,Inc electrical drawings: Electrical Power Distribution (Galley Power), GIV-24-1085-100 (Sheets 1 & 2); Galley and Cabin Electrical Interface, GIV-24-1085- 110 (Sheets 1 thru 3); Water Drain System, Water/Drain Heaters (Digital Switching), GIV-38-1085-112 (Sheets 1 & 2) and Electrical Switching and Control GIV39-1085-126 (Sheets 1 thru 9). Structural aspects of the newly installed/modified Galley and Cabin electrical systems are approved separately. Existing aircraft wiring diagrams affected by the above installation/modification are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapters 1 & 2 and manufacturers installation data. Aircraft equipment list and Electrical Load Analysis revised. Aircraft reweighed. END ❑ Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1112-761-012/G0IST SDNY_GM_02754107 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241029 EFTA01326622 li r , t& ment 6 ) f t , Oewo MAJOR . i ' twai.1 — 6 (Airframe); ' REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office identigption ttl~ OF I matklispositionof.thisloanahimapart for ..• 4STRUCTIONS: Print or type all envies. each such violation (Section 901 See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequ nt reviSiOn then:eel) for instructions is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not toexceed51.000 Federal Aviation Act of 1958). 1. Aircraft make GULFSTRENI AEROSPACE Model G-IY Serial No. 1085 Nationality and Registration Mark Ni38GA 2. owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only oThe dateallIIIIIIIIIIIrldentif led herein =plies with the applicable •Irworthinesa requirements and Is approved for the tows disarmed aircraft subject to cceiformi ty inspection by a person authorized in FAR 43, antigen 43.70. Date DEC 1 0 1996 FM Inspector CUM 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agencys Name and Addres B. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive U.S. Certificated Mechanic Foreign Cenificsted Meenanie I Cen Manufacturer D. I certify that therepair and/or alteration made to theun t(s) identified in item 4aboveand described on the reverse or attachments hereto have been made in accordance with the requirements of P rt 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my nowledge. Date DEC 10 1996 Signature of Authorized Individual e efwa4/A°' / 0-7..:, 7. Approval for Return To SeMce Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XX APPROVED 0 REJECTED FAA Eli Standards inspector Manufacturer inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 8 1996 Certificate or Designation No. 0K2R1121. Signature of Authorized Indivdual Catfrp.., c FAA Form 337 meat SDNY_Giv1_02754108 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241030 EFTA01326623 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be corripatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Removed the previously installed cabin and lavatory lighting system and installed a new cabin and lavatory lighting system with Ordinance Signs consisting of the following equipment: 3ea Aerospace Lighting Corp, Lighting Inverter P/N: AL-0581. , 18ea ALC Lighting Power Supply P/N: AL-5112. 2ea ALC Lighting Power Supply P/N: AL-2000. lea Grimes Light Assembly P/N: B3550. 2ea Grimes Light Assembly P/N: 34170-1. lea Luminator Light Assembly P/N: L16256-1. 21ea Wemac Light Assembly P/N: 2520-3. lea Bruce Industries Ordinance Sign P/N: BR9206-907. 4ea Wemac Ordinance Sign P/N: 3585. Wiring for the newly installed cabin and lavatory lighting systems are per K-C Aviation,Inc electrical drawings: Feature Panel Lighting (Digital Switching), GIV￾33-1085-111; Overhead Cabin Lighting (Digital Switching), GIV-33-1085-122; Vestibule Dome & Boarding Light, GIV-33-1085-114; Reading and Table Lights (Digital Switching), GIV-33-1085-115; Ordinance Lights, GIV-33-1085-125; Lav Lighting, GIV￾33-1085-106; Cabin Aisle Lights, GIV-33-1085-102 and Cabin Terminal Junctions, GIV￾39-1085-128. Structural aspects of the newly installed cabin and lav lighting systems are approved separately. Existing aircraft wiring diagrams affected by the above installations are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets NIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAN AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list revised. Aircraft reweighed. END 0 Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: Illt2-769-012/60157 SDNY_GM_02754109 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241031 EFTA01326624 11.5 (q;1,• I.: V; i *; I . • US NII9OR - 6 gmrtnint • • REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Only Office Identillcati7Use ICISTRUCTIONS.Print .loadisposition for 1.." nes. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instructions is required by law (4(1U.S.C.1421). Failure to report can result Inacivil penalty not to exceed $1.000 federal Aviation Act of 1968). or type all e attlaisforro,Thittegort each such violation (Section 901 1. Aircraft Make GULFSTREAN AEROSPACE Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only *The data /a identified herein is approved for the above sneer ibad aircraft in FAR 43, Section 43.74. Date DEC 1 0 100$ FM Inspectorr ie r carpi fee with stasJect the applicable to conformity airworthiness requirements inspection by a person authorized 0u3 4. and Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. ngeneys Name and Address B. Kind of Agency C. Certificate No. K-C Aviation, Inc. . 301 Discovery Drive Appleton, WI 54915 U.S. Certificated MeChenie QK2R112L Foreign Coniticaled Mechanic X Certificated Repair Malian manufacturer D. Icertify that the repair and/or alteration madeto the un t(s) identified in item 4 above and described on the reverseor attachmentshereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date DEC 10 1996 Signature of Authorized Individual 101.04 /1,r,..11*.Z.:4 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below, the unit Identified In item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is =APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 8 1996 Certificate or Designation No. QK2R112L Signature of Authoriz Individual (14..40 s, - FAA Form 337 (12461 SDNY_GM_02754110 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241032 EFTA01326625 NOTICE Wert and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description ofWorkAccomplIshod Olmom spacers required. attach additional sheets. with aircraft nationalityandlegistralionmade and date work completed.) Removed the previously installed cabin audio and entertainment systems in their entirety and installed a new cabin audio and entertainment system consisting of the following equipment: 10ea 10ea 2ea 4ea lea lea lea lea lea lea lea 4ea 2ea lea 2ea 2ea lea lea lea lea lea lea lea lea Audio International Headphone Control Baker Speakers P/N: HF93. Quam Speakers P/N: 4C5Z8. Baker Subwoofer Speakers P/N: LF91. BBE Sonic Maximizer P/N: SM-4012. Collins ATR Rack P/N: 622-1196-001. Stereo/PA Amplifier P/N: M3070M. Archer Amplified Coupler P/N: 151116. Audio Int. Video Switcher P/N: VSSO4. Audio Int. Video Switcher P/N: VSS04T. Audio Int. Audio Switching Controller P/N: MSM2804. Baker Audio PreAmp/Power Supply P/N: M1084PS. Audio Int. Infrared Receiver/Transmitter P/N: Alpine FM/AM Cassette P/N: TDA7552. Baker 14" LCD Monitor P/N: 990-4110-002. Panasonic VHS Hi-Fi VCR P/N: PV-4662. Sony CD Changer P/N: CDX91. Sony CO Controller P/N: RMX59RF. Airshow Genesys DCU P/N: 920060. Airshow Short Mount P/N: 914026. Asinc TTD Controller P/N: 911010-2. Audio Int. Mouse Switch Panel P/N: SP-450-1. Rosen 6.4" LCD Monitor P/N: RLCD64-1-1ACB. Rosen Power Converter P/N: RISR-28-12-6. Panel P/N: HSP-037-1. IFR9A-A-38. Wiring for the new cabin audio and entertainment systems is per K-C Aviation,Inc electrical drawings: Cabin Audio, GIV-31085-23-61 (Sheets 1 thru 4); Cabin Entertainment, GIV-31085-23-62 (Sheets 1 thru 9) and Airshow, GIV-31085-31-52 (Sheets 1 & 2). Structural aspects of the newly installed cabin audio and entertainment systems are approved separately. Existing aircraft wiring diagrams affected by the above modification/installation are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAN AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list revised. Aircraft reweighed. END ❑ Additional Sheets Are Attached *us GOVERNMENT PRINTING OFFICE: I992-769-011/60137 SDNY_GNL02754111 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241033 EFTA01326626 . -=--.- 1' vs mere f• Ilmn s II a 6 I-Cir:,(A. fri t I • AJOR REPAIR AND ALTERATION es Powerplant, Propeller, or Appliance) I Form Approved OMB No. 2120-0020 For FAA Use Only Office Identilicfroni3 INSTRUCTIONS. Print or ry --anddispositionPi form. This for each such violation ( 110n al I entries. See FAR 43.9, FAR 43 Appendix B. El and AC43.9-1 (or subsequent revision thereof) for instructions eport is required by taw (49 U.S.C. 1421). F Ilure to report can result in a civil penalty not to exceed S1,000 01 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAN AEROSPACE Model G -IV Serial No. 1085 . Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. AddreSS (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Us* Only •The data/FS identified herein complies with the applicable airworthiness requirements and is approved for the above discribed aircraft abject to conformity inspection by a person authorized in FAR 43, Section 43.70. Date DEC 1 0 1996 FAA Inspect . GL13 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As deserted in item I above) X POWERPLANT • PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated mechanic 0K2R112L K-C Aviation, Inc. Foreign Certificated Methanic 301 Discovery Drive y certificated Revak Station Appleton, WI 54915 amubOwer D. I certify that therepairand/oralteration made to the un have been made in accordance with the requirements furnished herein is true and correct to the best of my knowledge. t(f) identified in item 4 above and described on the reverse orattachments hereto of Part 43 of the U.S. Federal Aviation Regulations and that the information Date DEC 1 0 1896 Signature of Authorized Individual odoe. 4Y/ent-- T. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is )(It APPROVED 0 REJECTED FAA Fit. $IBMard9 Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Dateof Approval or Rejection DEC 18 1886 Certificate or Designation No. RK,R119L Signature of Authorized Individual C20w-wr c 16.-: FAA Form 337 0240 SDNYGIvl02754112 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241034 EFTA01326627 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircral t record. An alteration must be coMpatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. identify with aircraft nationality and registration mark and date work completed.) Modified the previously installed 115 VAC 60Hz Conveiter system by installing new outpu wiring to the existing galley circuit breaker panel and adding (6ea) new 115VAC outlets per K-C Aviation, Inc. electrical drawing: 115VAC 60Hz Converter, GIV-24-1085-147 and Utility Outlets, GIV-24-1085-146. Structural aspects of the newly modified 115VAC converter system are considered minor. Existing aircraft wiring diagrams are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapters 1 & 2 and manufacturers installation data. Aircraft equipment list and weight & balance revised. END ❑ Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-M/60157 SDNY_GM_02754113 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I035 EFTA01326628 i)N(e-'7 1 • PI -,- i J.:40 — 6 l'.;:: ,t MA OR REPAIR AND ALTERATION o (Airfr# , Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification A. -4//_.; tidnumtromm - —4 • INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for instructions and disposition el this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only •The data, identified herein complies vi h the applicable airworthiness readrements rd is reproved for the above discribed aircraft subject to conformity irapection by a person authorized in FAR 43, Section 43.7a. Date DEC 1 0 1996 FM Inspector • C- - - 61.13 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X . . POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive Appleton, WI 54915 U.S. Certificated mechanic QK2R1I2L Foreign Caelificated mechanic x oolitic's«, rt.pattsumto,, Manufacturer O. I Certify that the repair andlor alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date DEC 1 0 1996 Signature of Authorized Individual c 6,..3„.47,e,"Z:e-.... 7. Approval for Return To Service Pu suant to the authority given persons specified below, the unit identified in Item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XXAPPROVED Cl REJECTED FAA Fit. Standards Inspector Manufacturer Inspection AuthOdzation Other (Specify) BY FAA Designee A Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 18 1996 Certificate or Designation No. OK2R112L Signature of Authorized Individual 570,--- t d —IL FAA Form 337 112481 SDNYGIvl02754114 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241036 EFTA01326629 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (It more space is required. attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Modified the existing electric toilet system by installing a new Lav Switch Panel P/N: SPS-4-1-1759 per K-C Aviation,Inc electrical drawing: Electric Toilet, GIV-38- 1085-101. Structural aspects of the modified electric toilet are considered minor. Modified the previously installed electric window shade system by installing new wiring and new passenger Service Unit Switch Panels per K-C Aviation,Inc electrical drawing: Electric Window Shades, GIV-25-1085-127. Structural aspects of the newly modified electric window shades are considered minor. Installed wiring for (2ea) new electrical adjusting passenger seats per K-C Aviation, Inc electrical drawing: Electric Chairs, GIV-24-1085-129. Structural aspects of the new electrical adjusting seats are approved separately. Existing aircraft wiring diagrams affected by the above modifications or installations are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list and weight & balance revised. END ❑ Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 166x-766-01L6016T SDNY_GNL02754115 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241037 EFTA01326630 I ; i \ .. f C l uS4in:crimen :. . illiVOR • - REPAIR AND ALTERATION Powerplant, Propeller, Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only ? 6 r,cyxAi rt Airnirisnotion e, or Office IdentifiesIon in 6".Z.1-, J I) INSTRUCTIONS: Print or type a - anddisposition of thiSform...112dreport for each such violation (Section I entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for Instructions is required by law (49 U.S.C. 1421). Failure to report can result in &civil penaitynot to exceed 51.000 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only "The data. (dent if fed herein cowl les with the applicable airworthiness requirements ard is approved for the above described aircraft subject to conformity inspection by a person authorized in FAR 43, Section 43.7s. Date nFe 1 n 1005 FM I nspectr,, i - SI.13 4. Unit Identification 5- Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer S. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. K-C Aviation, Inc. . 301 Discovery Drive A ppleton, WI 54915 US. Certificated Medtanic QK2R112L Foreign Certificated Mechanic X Certilkated Midair Station Manufacturer 0. I certify that the repair and/or alteration made to the un t(s) identified In item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is trUltand correct to the best of my knowledge. Date . DEC 1 0 1996 Signature of Authorized Individual d.sesmi.A° 7 7“. 7. Approval for Return To Service Pursuant to the authority given persons specified haw, the unit identified in item 4 was Inspected in the manner prescribed by the • Administrator of the Federal Aviation Administration and is X APPROVED 0 REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Dale of Approval or Rejection DEC 1 8 1996 Certificate or Designation No. QK2R112L Signature of Authorized Individual 'gen,. FAA Form 337 id.ed SDNYGIv1_02754116 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I038 EFTA01326631 NOTICE Weight and balance oroperating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is ICQUired, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Modified the previously installed Cabin Call System per K-C Aviation,Inc. electrical drawing: Call System, GIV-33-1085-124. Structural aspects of the modified Cabin Call System are considered minor. All work done TAW AC43.13-2A chapter 1 & 2. Aircraft equipment list, Electrical Wiring Manual revised. Aircraft reweighed. END O Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: t992-769-012/60157 SDNY_GM_02754117 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241039 EFTA01326632 L. . \--. . MAJOR REPAIR AND ALTERATION nw 3 0 'Airframe, Powerplant, Propeller, or Appliance) • msm .I..:> fowMm j n Form Approved OMB No. 2120.0020 For FM Usa Only Office IdentifiZ 1.. fri INSTRUCTIO • ' tries. See FAR 43.9. FAR 43 Appendix B, arr AC43.9-1 (or subsequent revision thereof) for instructions t of this form. This report is required by law (49 U.s . .1421). Failure to report can result in a civil penalty not to exceed$1,000 for each such violation (Section 901 Federal Aviation Act of 1858). 1. Aircraft Wdr AEROSPACE Model FSTREAM G-IV Serial No. 1085 Nationality and Registration mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive Appleton. WI 54915 U.S. Certificated mechanic QK2R112L Foreign Canificated mechanic X Certificated Repair Station Manulacturer D. I certify that the repair and/or alteration made to the un t(s) dentif led In item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Data SEP 2 4 1996 Signature of Autho zed WU 'dual 7. Approval for Return To Service Pu suant to the authority given persons specified belOve, the unit identified in item 4 w peeled In the manner prescribed by the Administrator of the Federal Aviation Administration and s ,R. APPROVED 0 REJECTED FM Flt. Standards Inspect or Manufacturer Inspection Authorization Other (Specify) Inspeet. BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approvalor Rejection SEP 2 4 1996 Certificate or Designation No. QK2R112L Signature of Au th ed Individual (C421 C 1-- FAA Form 337 oar SDNY_GM_0275aile SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00241040 EFTA01326633 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record4seh.prati compatible with all previous alterations fo assure continued conformity with the applicable ainvorfh I--ust be tits. 8. Description of Work Accomplished Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Repaired left (02 from outboard) and right outboard flap drive rods and ground existing structure that rod goes through in accordance with Gulfstream Aerospace Standard Repair Drawing 5E05807901. Removed left and right main gear forward trunnion bearings, removed corrosion in trunnion support and plated in accordance with Gulfstream Aerospace Standard Repair - Spherical Bearing - Main Landing Gear - Sponson Rib - Trunnion repair drawing 5E45732901. No weight and balance change. END 0 •Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60IST SDNY_GM_02754119 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241041 EFTA01326634 017M41143•1 co wg?Inosircei..."'"".“nosmasherroArse " " • STANDARD AIRWORSHNSSS CERTIFICATE att., NORGA istfacM10•••••••00124 cocrarReam / vxv LOSS ASSORT Yw 12/14/88 CL atis— TAY (WO °"`ARYCOSNEN% VMS CII•t0Call M CMPAII) •• 114 WIWI' w ACCOOISCII WPM AMON. Raft FAA Fain 11103-2 ww SONY GM 02754120 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15 EFTA 0024I042 EFTA01326635 SDNY_GM_02754121 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241043 EFTA01326636 0 MAJOR REPAIR AND ALTERATION US Deponent (Airframe, Powerplant, Propeller, or Appliance) of toreceubo• Fekel Medea elsothenneee Fee Armed 020 Na 21200720 For FAA Use Only office identification ii 9—O7 INSTRUCTIONS- Print or typo all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9.1 (or subsequent evision thereof) for instructions and eitsposillon of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G - I V Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above X Powerplant Propeller - Appliance Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X U.S. Certificated Mechanic Foreign Certificated Mechanic AP 1864049 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unfits) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation R lations and that the information furnished herein is true and correct to the best of my knowledge. Date 7....70 -ft S • • • r 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit id ntified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 121 APPROVED O REJECTED BY FAA Rt. Standards Inspector Manufacturer X Inspection Authorization Other (Specily) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 7 -A9 -fAr Certificate or Designation No. 526705494 IA Signature of Auth • In dual Ls GL Michael Donnelly FAA Form 337 (07-96) This is a computer ed form created by Michael Donnelly. SDNY_GM_02754122 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_OO241O44 EFTA01326637 NOTICE Weighrand balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) In order to provide continuity during fitture inspections, maintenance or alterations a true dopy of this FAA form 337 and all listed Wiring Diagrams must be kept with the aircraft's records as long as the alteration remains in effect. July 10,1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet A I2EA. Aircraft in-service data: 2241.9 hours & 932 landings. Refer to the following FAA Approved Data: GAC Aircraft Service Change {ASC} 143 (ATA 24) Alternator Field Current Overcurrent Monitor, dated: October 7, 1994; and FAA Form 81 I 0-3, dated: 7-10-96, Identifying: Drawing No. ASC 143-062096, Titled: TOP DRAWING ASC 143 (ATA 241 Alternator Field Overcurrent Monitor Original Issue (no revisions), dated: 7-9-96, — the following Wiring Diagrams are listed on the TOP DRAWING: • Wiring Diagram No. 06209601, Titled: }.EFT SIDE DEVIATIONS dated: JUL 09/96 and • Wiring Diagram No. 06209602, Titled: RIGHT SIDE DEVIATIONS, dated: JUL 09/96, as approved data, signed by: John R. Chambless, NM-567, Systems and Equipment (Electrical). The purpose of this alteration is provide an indication that maintenance personnel can use to determine that an overload condition has occurred in a main engine alternator field circuit. This alteration adds a current sensor assembly and fault latch indicator to the left and right converter shelves and modifies the aft equipment compartment wiring. The above referred to Wiring Diagrams show deviations that were made to ASC 143 in order to provide a way to disconnect a DC Current Sensor or Alternator Overcurrent indicator display without cutting wires. These deviations also add a shield braid for each existing alternator (+) field wire and bond both DC Current Sensors, eliminating the need to run new wires to the left and right engine disconnect plugs. Performed all of the modification instructions of ASC 143, except as provided for on the above listed Wiring Diagrams. All parts were purchased from Gulfstream Aerospace Corporation — Savannah, GA and were new at the time of installation. Successfully performed — ASC 143 Operational Test in accordance with Paragraph E. of the ASC's instructions and noted no abnormal conditions or unusual operation. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. Incorporation of this alteration adds 0.2 amps to the Essential 28 VDC bus. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. This is • computer generated fan created by: Michael Donnelly ASC14388.DOC WORD 7.0 07/10961239 PM NO ADDMONAL SHEETS ARE ATTACHED. •END' ❑ Additional Sheets Are Attached SDNYGIvl_02754123 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241045 EFTA01326638 -Pi JR . U.S. DEPARTMENT OF TRANSPORTATION , • FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7-10-96 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE ei il ,„ GULESTFEAM AEROSPACE MODEL NO. G -IV TYPE (Airplane, Radio, Koko: Net, etc.) AIRPLANE NAME OF APPLICANT THE DIAL CORPORATION / UST OF DATA IDENTIFICATION TITLE DRAWING NO. ' REV DATE #SHTS ASC ALIEFtNATOR CURRENT BY DRAWING TITLE ASC-143-062096 N/C 7-9-96 1 °THE ABOVE DATA N REVI WED NAME: ..a .7 TOP 143 DER DATE DRAWING (ATA-24) FIELD OVER MONITOR CANDIDATE 7-9-96 Michael natty PURPOSE OF DATA TO SHCE4 OCMPLIAI4CE WITH FEDERAL AIRWORTHINESS REGULATIONS, ON AIRCRAFT MODIFICATION WIRING DIAGRAM CN ANY GULFSTREAM G-IV HAVING ASC-143 APPUCABLE REQUIREMENTS (List spades sections) 25.1301(a,b,c,d); 25.1309(bl); 25.1353(a,b); 25.1357(a,c); 25.1431(c) CERTIFICATION — Under authority vested by direction of appointment under Part 183 of the Federal Aviation - NONE - have been examined of the Administrator and in accordance with Regulations, data listed above and on attached in accordance with established procedures conditions and limitations sheets numbered and found to comply with applicable requirements of the Federal Aviation Regulations. I (We) Therefore 0 Recommend approval of these data F3 Approve these data SIGNATUREtS) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) I DESIGNATION NUMBER(B) CLASSIFICATONIE) dr ... 4 or ..7 /.2ser....a.,,,..4 6 John R. Chambless NM-567 Systems &Equipment (EleCtrical) FAA Form 6110-3 (11-70) SUPERSEDES PREVIOUS EDITION 7.00 Qj 011 YNN0P This a a cernpuhr geneated lam anted (0995) by: hada& Dannelly 9t92 6St Z0L 0C:60 96/0T/L0 SDNYGM_02754124 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241046 EFTA01326639 SDNY_GM_027.125 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I047 EFTA01326640 ASC 143 (ATA 24) Alternator Field Overcurrent Monitor LEFT SIDE DEVIATION The Dial Corp Aviation Department WIRING DIAGRAM No. 06209601 Original Issue JUL 09/96 , ASC 143 (ATA 24) Alternator Field Overcurrent Monitor RIGHT SIDE DEVIATION The Dial Corp Aviation Department WIRING DIAGRAM No. 06209602 Original Issue JUL 09/96 The Dial Corp Aviation Department 2505 E. Airlane Blvd. Phoenix, AZ 85034 602-207-5363 voice 602-207-5353 fax Gulfstream Aerospace Model G-IV effective all S/N aircraft having ASC 143 (ATA 24) Alternator Field Overcurrent Monitor TOP DRAWING No. ASC143-062096 Original Issue JUL 09/96 SDNY_GNI_02754126 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241048 EFTA01326641 SDNYGM02754127 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241049 EFTA01326642 V1013A20— › bød • ~0 TO IJCItt *PI Cain tut Otleantl4.1 Namur mar ~ma we Nunn.. ~et The Dial Corp Mtalniittitlemeta 23,3 Z. AMY* OW& non» At 11414 60201141 ere 00000 In 02.1•1 Mgt Cata V.013020 Ma ACC NC DIAL CORP »ANC NACAMA 000141A1C Iq MGM SIDE DEVIATION' VINIX20 edd VIMILANUI TV10,114 W CONN WI PC" AHCOII •Ltat lEIAPRO 1~ .1~1~ MU) WO ~ILO Y •••41.11.8 tat 1•110.0.8S11År . ~Ns Mtn ~Ka lababre• LEFT µNA arg OVORGURROKT m» NOCAT011 1•01.7.021 nit tic saw Mr» Male » amommmer Ma— »re« • paltatitneett. — ~It att ...es .25 MPG Imo» Rob» On M lamed 18 DOG metro Gødø 1 (NO ALT» MUD CtMAINT 2040.1 Ms CT.» WA til~Milit tattilitt Pmet•Imetw HI GA@ 44.43 .0~ • • •••• a ~S. —• •••• • • •••••• LEFT CONVERTER SHELF no roam» ~moon --a otthanam• =it% oq LEFT »WM OttCON/ICCT S010 ret Aka tft do rae• GI.0 11• td.143. »We» «Met» el Pent NTA 341 AM. natas field Ovensmem10MMA Tids Waco Nap ~a» an Adana lb Immeonel »A en »acme« monn« b. occombø De ~mar ~en» Ton ..Mn aeon 5.1.• won •••••••••••.» to i» W I.M,011 vermorme WM. imbo »OD« irgapommicammelmaimids• TMtl rianae. ono» ~WM» NM MAID 143 InM.rb Moan • Way W distant • OG GoribM Sal« M AgrnnM Ostonat ~My dibia.1~ maim •••• TIN ~Sea MO ~Me •OCA ~lie ~mar 1./.4.11 • bonds M. DC Gam» tam" emnaads. No MIN bisatt ~el let ~NA »4 MN taiatit‘i40~1...• d+å »Am» ea Mad wools 1141.0210/18me »see et» Mom Nina am.b• »mum» M/ »men ammo GAG Wig» tam SI dap» nova IN» at At Ow» 10•41—.~...1~ »a • mapieSTR. oie es Der. Hy outmost St ~Myth" Ailen.mbie lanai 13-1V effliam ø• AM »emit 55.1.» Alt 10 1ATA LI Anortelor PAM Oremmn». »MI« LOOT SIM pre101014 WIRMO DIMULUI No DHOW» Orameed Ina AA 0.At • SDNY_GM1,1_02754128 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241050 EFTA01326643 - SDNY_GM_02754129 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024105 I EFTA01326644 PONT CONVERTER a MCI M ARLO AUX root WAY SOX • 33333 sot SAP PRESTO TOMER E wan nit - WISP'S nino.• • SE add VP lA.2 a• so• Eno Apia Einem c...•... ouftinipi ism is as realm, ••I Maas* fa. at The Dial Corp ARAMs Coorrpro >14I E. Plop PAL rbarak.AE 111.14 142.7874311) rwa 1141.38NS //I to SPAIN, M TRECTIR SEE DM OUR co*I waimi ..._ ÷ UPOO *MAMIE t µ 042 PO E Mal AEC IP ra PP ID OCT 744 UL IMO Gana00, Odd POI PP SCP µ %WHAM Ho VS 11M011 µ 111016"20 µ so econocap Mop laa APRS POW )m• -Mal. ••••••••• atlas Yr Waal Dar e tall ••• Iwo al Wad •I awn. LEPT Ma DEVIATIONS IIOLOC• slat OPP ao• RIGHT AETN OVERCURRENT NOVATO* US32.7/014 cal• WI MD DUD 11•01 SOC MAIO lat•LACC araCOSLICV•gl Ihanaltall INILI IIMO ••• 0•1110.47 21 VDC Seal REVCO INN* Rant Cal eras. REVCO RASE CT•02 R ENO ALTAR REED CURRENT SENSOR µ TVS'S.% mm SLOW am Runup Ana 0.4 Illa••••••••• OYU •4•IJSIN.• C••••• lame, la CAC A.C.43 Dia gab Mayas, aa••••••• Poen gnome PECOPINECT SIAM Aarpott *tyke agape NAPA S P EREPall In. CA • PI Airanippr INN Ovonai WOrmil masons= Ch SW. 100•14111 an b•ONabot NMW1MW pinolinal Oat an aborarrrent CMIONEa Ns PAPP la • perealr OHO areal TIP pearl PPP POE • wanM Wa0 t 111•0•00/N .M 401 COVV•110/ Saha al modes me an elpairesi toopasnat RONA O P Spin Pop driNplona Salvers ASAP AEC 143 laaa N Walla • al 10 Ilalatel • DC Comae Sapp or *Rammer Oprearrani PEONS Sap vitheal OAP. Pp. Tit -* Iµ440 EIEE PLOP PO Ealip ellepelerl•I n o µ bonds DC Comet Sanwa. .404040E 0a PRI * no Amman4o Op NN PA OSP AR" "al". OS EARN PP'S. MI µ.4.t* N ikAVARRIONS•ix CAM Opiralon alb may be liebtalbuid. Pt PPS APP. SAC 111,18.1041$04• RP POPO Mn Pad by Po fly. RIGHT CONVERTER SNEER spoon- - -RP site. inol. M1 rod•-lII 0.01*••• Panora. RAM 04V 4040-* al Sal it Gra Paso ASO PS IAEA SO Altornirtor Okla p•nanµ PROW MOM net OCVLAIIONE PROP INAGRAII Na.PRAM Coos! lawn ENLOE/PI • • N • SDNY_Givi_02754130 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241052 EFTA01326645 SDNY_GM_02754131 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I053 EFTA01326646 .- rb isio MAJOR REPAIR AND ALTERATION a.r (Airframe, Powerplant, Propeller, or Appliance) Mr ha° AIW0nd MIX*. 21204020 ForFAA Use Only Office Identification ItISTRUCTIONS' Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of (hi /can. This report is required by ism (49 U.S,C. 1421). Failure to report can result In a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G - I V Serial No. 1 0 8 5 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above) X Powerplant Propeller Appliance Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X U.S. Certificated Mechanic Foreign Certificated Mechanic A P 1 8 6 4 0 4 9 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made o the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my Imowledge. Date Si o o ed Individual ""717`- p( t e 7. Approval for Return to Service Pursuant to the authority given persons pccified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is al APPROVED 0 REJECTED BY FAA Flt Standards Inspector Manufacturer X InspectionAuthorization Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 4-- /8 -94 , Cenifieste or Designation No. 526705494 IA Signature of Au e 71 d Michael Donnelly FAA Form 337(114s) This is a cater generated form created by Michael Donnelly. SDNY_GM_02754132 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_0024 (054 EFTA01326647 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 06/17/96 Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al 2EA. Aircraft time in service: 2234.1 hours and 929 landings. FAA Approved Data: FAA Form 8110-3 Statement of Compliance with the Federal Aviation Regulations dated 11/01/94 for Gulfstream Model GIVAirplane, listing GAC Drawing No. SE45807901 - REV. A - 10/31/94, effective for S/N 1000-1195, title: STD REPAIR — BREATHER WING T.E. BOX - F.S.498.00 (MAJOR), signed by Structures DER John G. Wilder, Designation Number SO-483. The purpose of this repair is to remove the existing GAC P/N 1159W40226-17/-18 (aluminum) breathers that are cracked beyond limits from the aft side of the trailing edge (T.E.) box beam and replace them with new P/N SE45807902-11/-12 (stainless steel) breather on the forward side of the beam as shown on the above referred to drawing. Removed the existing breathers from the aft side of the left and right wing trailing edge boxes by drilling out the attaching fasteners. Trinuned the perimeter of the new SE45807902-11/-12 breathers to fit the installation and match drilled 0.164-0.167 inch diameter holes in the breathers to existing aircraft rivet hole locations. Finished fay surface of SE45807902-11/-12 breathers with two (2) coats of #2012 Epoxy Primer and one (1) coat of 2013 epoxy top coat paint. Attached the prepared left and right breathers to the forward side of their respective beams using new Hilok fasteners P/N HL 10V5-2 Hi-Lok and P/N HL, 70-5 collar at each of the 10 inboard attach points; and new P/N HE., 30-5-3 (-4 at the top position only) Hi-Lok and Bl, 70-5 collar at each of the 6 outboard attach points. Note: All fasteners were installed wet with pro-seal 870 (or equivalent product per MIL-S-81733). Changes to the aircraft's weight and balance were negligible. This computer generated form was prepared by: Michael Donnelly. NO ADDMONAL SHEETS ARE ATI-ACHED. oalD• O Additional Sheets Arc Attached SDNYGIvl_02754133 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241055 EFTA01326648 CIS MI 0c';_,:y‘F.IVED FAA 4 1)' . (../ MAJOR REPAIR AND ALTERATIOW B 121°96 us oeconnwar cliemponmen (Airframe, Powerplant, Propeller, or A PPIIMYSSDO Weed Aviatio Administration n Form Approved OMB No. 2120-0020 For FAA Use Only office Identification VW ite—6PD INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43Appendix B. and AC 43.9-1 (or subsequent revision thereof) tor instructions and disposition of this form. This report is required bylaw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Gulfstream Aerospace Corporation Model G-IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Nam.kiels shown on registration certificate) Mellon Financial Corp. Ni Address (As shown on registration certificate) 4444 One Mellon Bank Center Pittsburgh, PA 15258 3. For FAA Use Only • .0. Unit Identification S. Type Unit Make Model Serial No. Repair Anatol,: AIRFRAME .. (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CFC Aviation Company,LI-C dibta The Jet Center 16300 Daily Drive Van Nuys, CA 914064283 u.s. Cenificateo Mechanic C9FI1844.1 Airframe 3,4 Ptilid10 112 & 3 Limited Powerplant, instrument & Accessory Foreign Co:Ideated Mechanic X eormieatee Repair Station manuractwer D. I certify that the repair and/or alteration mode l° the un't(s) identified In item 0 above and described on the reverse or attachments hereto . have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date FEB. 9 1,38 Signature of AuthOr Individual • '. 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below, the unit identified In item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is 0 - APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada AirworthineSS Group Date of Approval Or Rejection FEB' 9 1996 Ceniticale or Designation No. C9FR844J Signature of Authorized lndi • al ..a.-4.-c-t 2 ...--4,...t...4" FAA Form 337 SDNY_GM_02754134 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024I056 EFTA01326649 NOTICE Weight and balance or operating limitation changesshall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations fO assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished- (If more space Is required, attach additional sheets. identity with aircraft nationality and registration mark and date work completed.) 02/09/96 GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA This is to amend FAA Form 337 dated 01/26/96 regarding the provisional installation of a Honeywell NZ-2000 FMS Computer modified to software version 4.1 which functions as an independent third navigation system and as a warm spare to replace either FMS-1 or FMS-2 including its aircraft systems interface. An upgrade to previously installed dual Honeywell GPS sensors from PN: HG-2021-AB02 to HG-2021-GD-02 was also incorporated in conjunction with the third FMS. These modifications were incorporated in accordance with the applicable technical data contained in configurations 13, 15,16 and 17 of The Jet Center Configuration Control Document 08006005 Rev. D dated 01/20/96, FAA approved 02/02/ as a later revision to plemental Type Certificate No. SA3774NM. Airplane Flight Manual Suplement Document Nos. 08015090 Rev. N/C, 08015091 Rev. N/C, 08015009 Rev. A, and 08015011 Rev. B, all of which were FAA approved on 02/02/96, have been provided to the operator. Minor deviations to the STC with regard to the electrical installation were accomplished in accordance the following Jet Center wiring diagrams which are FAA approved by Sarkis A Karaguzian, FAA Systems and Equipment DER NM-2128 on FAA Form 8110-3 dated 02/09/96: 08069100 Rev. A dated 01/20/96 - No. 3 FMS 08069324 Rev. A dated 01/20/96 - No. 1 & No. 2 Global Position The 3rd FMS computer may be installed in the mount provided. The circuit breakers controlling power to the two GPS sensors can be closed. The placard stating "FMS-3 AND GPS INOP PENDING FAA APPROVAL" placed on the instrument panel can be removed. The effect of these modifications upon the aircraft empty weight was reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagrams listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END O Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: I992-769-012/60157 SDNY_GM_02754135 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241057 EFTA01326650 'at—!o ff 0 • . MAJOR REPAIR AND ALTERATION USCepeetrrent or soNsoonsson (Airframe, Powerplant, Propeller, or Appliance) hwassiatioilai Adrewstration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identlficatlpp Illig -P 512O INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix Et and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1400 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make GWfstream Aerospace Corporation Model G-IV Serial No. 1085 Nationality and Registration Mark N811GA 2. owner Name (As shown on registration certificate) Mellen Financial Services Corp. ft3 Address (As shown on registration certificate) 4444 One Mellon Bank Center Fittsburgh,PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certi Nate No. CFC Aviation Company, L.LC. d/b/a The Jet Center 16300 Daily Drive Van Nuys, CA 91406-1283 U.S. Certificated Mechanic C9FR844.1I Airframe 3,4 Radio 1,2 & 3 ..irnited Powerplant, .ost rument & Accessory Foreign Certificated Mechanic X Cenificaled Repair Station Manufacturer D. I certify that therepair and/or alteration made to the un t(s)Identif led in item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my nowledge. Date JAN 2 6 1996 Signature of Authorf Individual 7. Approval or Return To Service Pursuant Administrator BY to the authority given persons specified below, the unitidentified In Item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is er -APPROVED 0 REJECTED FAA FP Standards Inspector Manufacturer Inspection Authorization other(Specify) (Specify) FAA Designee X Repair Station j Person Approved by TrariSPOrt Canada AinvonhIness Group Date of Approval or Rejection ;JAN 2 6 1996 Certificate or Designation No. C98148443 Signatur Authorized Individual -4-4-6-4- - C FAA Form 337 meal SDNYGl.l02754136 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241058 EFTA01326651 NOTICE Weight and balance oroperating limitation changes shall be entered in the appropriate sacra I t record. An alteration most be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished' (It more space Is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS . Removed an existing Honeywell NZ-920 acting as the third Flight Management System Computer with its mount, and the dual Honeywell HG-2021-AB-02 Global Navigation Satellite Sensor Units previously installed per STC #SA3774NM. Flight Manual Supplement Numbers 08015014 and 08015015 "Original" Revisions dated 07/18/91 for FMS-3 and Dual Honeywell Global Positioning Sensor System were removed from the Airplane Flight Manual. Installed provisions for a third Honeywell NZ-2000 Flight Management System (FMS) computer modified to software version 4.1C a ong with mounting provision and a configuration module to function as an independent third navigation system and as a warm spare to replace either FMS￾1 or FMS-2 including its aircraft systems interface. Electrical provision were also made for dual Honeywell HG-2021-GD-02 Global Navigation Satellite Sensor Units that are installed in conjunction with the third FMS. Parts 1 and 2 of the Type Inspection Authorization for FAA Project No. SA4222LA-T have been satisfactorily completed and issuance of the revision to STC SA3774NM is pending FAA approval. Electrical provisions were installed in accordance with the following Jet Center Wiring Diagrams which are FAA approved by Sarkis A. Karaguzian, FAA Systems and Equipment DER NM-2128 on FAA Form 8110-3 dated 01/26/96: 08069100 Rev. A dated 01/20/96 - No. 3 FMS 08069324 Rev. A dated 01/20/96 - No. 1 & No. 2 Global Position The #3 Navigation Computer was installed on an existing avionics shelf located in the right hand avionics bay at Fuselage Station 162.0 (Horizontal Arm 102.0). Both GPS Sensor Units are installed in the existing mount structure used for the removed sensor units beneath floor 15. These installation meet the static load requirements of AC 43.13-2A Chapter 1. The 3rd FMS computer is not installed in the mount provided. The circuit breakers controlling power to the two GPS sensors are locked open pending FM approval. A placard stating "FMS￾3 AND GPS INOP PENDING FAA APPROVAL" is placed on the instrument panel. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagrams listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END El'Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-0I2/601S7 SDNY_GM_02754137 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241059 EFTA01326652 t14/4,4,0 Tx"- ? /, OP MAJOR REPAIR AND ALTERATION uSeaslOttfred creonspcneton (Airframe, Powerplant, Propeller, or Appliance) Wirer *Melon Aaminumnion Form Aeon:wed OMB No. 2120-0020 For FAA Use Only Office Identification I/WV—FWO INSTRUCTIONS: Print or type all entries. See FAR 43-9. FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C.1421). Failure to report can result in a civil penalty not to exceed $1000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Gulfstream Aerospace Corporation Model G-IV Serial No. 1085 Nationality and Registration Mark NSSGA 2. Owner Name (As shown on registration certificate) Mellon Financial Services Corp. 83 Address (As shown on registration certificate) 4444 One Mellon Bank Center Pittsburgh, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME _ (As described in Item 1 above) X POWERMANT PROPELLER .SCEIVED FAA APPLIANCE Type JAN 2 9 1996 ' NV FSDC% Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CFC Aviation Company, LLC. dlb/a The Jet Center 16300 Daily Drive Van Nuys, CA 914041283 us gene:cats Mechanic FR844J Airframe 3,4 dlo 1,2 & 3 ted Powerplant, strument & Accessory Foreign Certificated Mechanic X Certificated Repair Station Manulacturer 0. I certify that the repair and/or alteration made to the un t(s) Identified In item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my nowledge. Date .IAN 2 6 19 9 6 Signature of Aut I ed Individual . - e SA 0 017 . --ne---4-1----- - 7. Approval for Return To Service Pu Administrator BY suanl to the authority given persons Seedbed below, the unit identified In item 4 was inspected in the manner prescribed by the of the Federal AviatiOll Administration and is rr APPROVED ID REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rekection JAN 2 61996 Certificate or Designation No. C9F118441 Sig natur of Authorized Inclivpcit! ) ..A....e...a... FAA Form 337 rizen SDNY_Glvl_02754138 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241060 EFTA01326653 NOTICE e • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS The following major Gulfstream Aerospace Aircraft Service Change is incorporated into this aircraft: ASC No. 349 with Amendment 1 - Navigation (ATA 34) Nav System Upgrade to NZ-2000 The amendment upgrades navigational computers 1 & 2 to software version 4.1. Gulfstream Aerospace Airplane Flight Manual Supplement No. GIV-95-04, FM approved on Nov. 3, 1995, required with this change, has been inserted into the Airplane Flight Manual. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list has been added to the aircraft records. The work described has been found to be in conformity with the above mentioned FM approved ASCs. The aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work order 9042, on file with this agency, covers the above described work. END ❑ Additional Sheets Are Attached OU.S. GOVERNMENT PRINTING OFFICE: 1092-769-012/60167 SDNY_GM_02754139 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241061 EFTA01326654 MAJOR REPAIR AND ALTERATION USOmerunere eflecepCeleaa. (Airframe, Powerplant, Propeller, or Appliance) Feelefol fretleflon Adminhaemen Form Approved OMB NO. 2120-0020 For FAA Use Only Office Identification nt" -590 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43Appendix Mend AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of thisformThis report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1 .Aircraft Make Gulfstream Aerospace Corporation model G-W Serial No. 1085 Nationality and Registration Mark NSSGA 2. Owner Name (As shown on registration certificate) Mellon Financial Services Corp. #3 Address (As shown on registration certificate) 4444 One Mellon Bank Center Pittsburgh, PA 15258 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 abo 0) X POWERPLANT PROPELLER APPLIANCE Type Manulacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CFC Aviation Company, LLC. dibla The Jet Center 16300 Daily Drive Van Nuys, CA 91406-1283 us. certificated Mechanic C9F11844J Airframe 3,4 Radio 1, 2 & 3 Limited Powerplant, Instrument & Accessory Foreign Cenificated Mechanic X 0min:sled Repair Station Manufacturer 0. I certify that the repair and/or alteration made to the un t(s) Wenn! ied in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date JAN 2 6 1696 Signature of Authorized Individual 7. Approval for Return To Service Pu Administrator BY suant to the authority given persons specified below, the unit-identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is 2 -APPROVED 0 REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada AinvorthineSs OreeP Date of Approval Or Rejection JAN 2 6 1996 Certificate or Des na C9 tionNo Signature of Authorized Individual a4/-4 C. Ccja-e-tra.-4 1 FAA Form 337 na-ae/ SDNY_GIvl_02754140 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241062 EFTA01326655 NOTICE • 41" Weight and balance oroperating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished' (II more space is required, attach additional sheers. Identity with aircraft nationality and registration mark and date work completed.) 01/26/96 GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS Removed existing Sundstrand Mk. V Ground Proximity Warning Computer PN: 965-0676-006 from this aircraft. Flight Manual Supplement Number 41 349607-04 dated 10/14/87 for Sundstrand Digital Ground Proximity Warning System was removed from the Airplane Flight Manual. This unit was replaced with Allied Signal Mk. V Ground Proximity Warning Computer PN: 965- 0676-010. The new computer was installed in accordance with data contained in Gulfstream Aerospace Index List No. SC41-349836 Rev. C dated Feb. 20, 1095 reference on Supplemental Type Certificate No. ST00714AT issued on March 15, 1995. FM approved Airplane Flight Manual Supplement SC41 349M36, Rev. "Original" dated March 15, 1995, which is a required part of this STC, has been placed in the Airplane Flight Manual. Minor deviations regarding the electrical installation of this modification where accomplished using data contained in The Jet Center Wiring Diagram No. 08069434 Rev. N/C dated 10/09/95, "Ground Proximity & VVindshear" which is FAA approved by John R. Chambless, FM Systems and Equipment DER NM-567 on FAA Form 8110-3 dated 01/26/96. A forward pressure bulkhead feed through at Fuselage Station 85.5 was added to provide wiring &togs for stall warning computers. This was accomplished using data contained in Engineering Change Order EO043 applied to The Jet Center Drawing No. 08088188 Rev. N/C dated 01/17/96. This drawing is FAA approved by Joseph R. Holton, Jr., Structures DER SW-862 - on FM Form 8110-3 dated 01/26/96. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagram listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END O Additional Sheets Are Attached CU.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/601 67 SDNY_GM_02754141 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241063 EFTA01326656 fer Ftelb ArtC0•44 OMID Na 31204030 MAJOR REPAIR AND ALTERATION For FAA Use Only ar net (Airframe, Powerplant, Propeller, or Appliance) rouenntim • Dews me Ader**Lesil mo ei Office Identification aef7 INSTRUCTION& Print or type as envies. See FAR 43.9. FAR 43 Appendix B, and AC 43.9-1 (or subsequent r Ion thereof) for instructions and disposition of INS lent. This report Is required by law (49 U.S.C. 1421). Failure to report can taunt In a OA penalty not to exceed $1,000 for each such violation (Sedan 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G-IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item 1 above X Powerplant Propeller Appliance Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X U.S. Certificated Mechanic Foreign Certificated Mechanic AP 1864049 _ Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unk(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirem nts of Part 43 of the U.S. Federal Aviation Regu ations and that the information furnished herein Is true and correct to the best of my knowledge. Date /ci t " re Signature of Audio ' ivi — Ce 7. Approval for Return to Service Pursuant to he authority given persons pecified below, the u it identified in item 4 was inspected in the manner prescribed by the Admin'strator of the Federal Aviation Administration and is C33 APPROVED Cl REJECTED BY FAA Flt. Standards Inspector Manufacturer X Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection / - 9 - - 94 Certificate or Designation No. 526705494 IA Signature of Authorized In ual Michael Donnelly FAA Form 337(l1.95) This is a computer gyyriyedfonn created by Michael Donnelly. SDNYGM02754142 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241064 EFTA01326657 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) In order to provide continuity during future inspections, maintenance, or alterations a true copy of this FAA form 337 must be kept with the aircraft's records as long as the alteration remains in effect. January 05, 1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2090.8 hours & 877 landings. Refer to the following FAA Approved Data: FAA Form 8110-3 dated November 17, 1995 identifying Aircraft Alteration Report No. 23-100895 AFIS PRINTER Original Issue no revisions dated October 8, 1995 Pages 1 through 15 as approved data, signed by John R. Chambless NM-567 Systems and Equipment (Electrical). Refer to the following FAA Acceptable Data: ACCULEX DPP-210/410 THERMAL PRINTERS User's Manual for operator instructions, maintenance, and other information. The purpose of this alteration is to install a miniature thermal printer that will print Airborne Flight Information System (AFIS) received messages. This alteration installs a modified ACCULEX model DPP-410 thermal printer in the co-pilot's side console, associated wiring to the existing AFIS Data Management Unit (DMU), and a I amp circuit breaker on the co-pilot's circuit breaker panel. The installation requires approximately 24 man-hours to incorporate. Performed all of modification instructions listed in the above referenced Aircraft Alteration Report. Printer was modified to -503 status by and purchased from Gulfstream Aerospace Corp. Long Beach, CA. Successfully performed an AFIS message — Operational Test in accordance with the instructions contained in the above referenced Aircraft Alteration Report. The aircraft may be dispatched with the AFIS PRINTER in-operative provided the AFIS PRINTER circuit breaker is pulled and an IN-OP placard is placed on the printer. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. Operation is automatic and straight forward and no Airplane Flight Manual revisions were required or installed as a rcsult of this alteration. The effect of this alteration on the aircraft's electrical load analysis was negligible and no changes were made to the aircraft's electrical load analysis report. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. this is a computer generaced loon created by: Michael Donnelly PRINTER.DOC WORD 6.0a: 01!05#96 7:43 PM NO ADDMONAL SHEETS ARE ATTACHED. •END' O Additional Sheets Are Attached SDNY_GM_02754143 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241065 EFTA01326658 yt` 0 MAJOR REPAIR AND ALTERATION US. Dtparimett (Airframe, Powerplant, Propeller, or Appliance) N Tenticanitica ntral A•loan A 4thilsinttlan RIM APMW. am NO 21200020 For FAA Use Only Office Identification a t -/C54 6 INSTRUCTIONS: disposition of this each such viotati Print Cf typo as entries. See FAR 43.9. FAR 43 Append% B. and AC 43.9-1 (or subsequent revision thereof) for instructions and form. This report Is required by law (49 U.S.C. 1421). Failure to report can result In a civil penalty not to exceed $1,000 for n (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G-IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification • 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above ***** ************** X Powcrplant Propeller Appliance TYPc Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X U.S. Certificated Mechanic Foreign Certificated Mechanic AI' 1864049 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regu ations and that the information furnished herein is true and correct to the best of my knowledge. Date /— g - n Signature of zed Ingidu ./.:ct 7. Approval for Return to Service Pursuant to the authority given persons pecified below, the unit identified in Item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Ell APPROVED O REJECTED BY FAA Flt. Standards Inspector Manufacturer X Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date o Approval or Rejection /Ale‘ Certificate or Designation o. 526705494 IA Signature of Authorize Indivi I reAe r Michael Donnelly FAA Form 337 (11-95) This se a ter generated form creased by Michael Donnelly. SONY_GM_02754144 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241066 EFTA01326659 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) January 08, 1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2090.8 hours & 877 landings. Refer to the following FAA Approved Data: Gulfstream Aerospace Corporation Aircraft Service Change 364. subject: DOORS (ATA 52) 12th STAGE AIR SOURCE - DOOR SEAL SYSTEM PRESSURE, dated September 26, 1995. The purpose of this alteration is to reduce the potential for door seal deflation by ensuring a constant high pressure and maximum flow output from the door seal regulator. This Service Change installs additional pressure supply lines, one from each engine, routed from a port located in the pylon upstream of the 12th stage H.P. valve to the existing door seal regulator pressure supply lines located in the tail compartment. The existing pressure supply lines are re-routed to separate the water system pressure tap and the total air temperature probe pressure supply form the door seal pressure supply lines. A separate air supply manifold now supplies this circuit. This Service Change modifies door seal plumbing in the tail compartment and in both nacelles. The installation requires approximately 90 man-hours to incorporate. Performed all of modification instructions listed in the above referenced Aircraft Service Change. All parts installed were provided in kit form by Gulfstream Aerospace Corp. Savannah, GA. Successfully performed a Bleed Air System — Operational Test in accordance with the instructions contained in the above referenced Aircraft Service Change. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. Entered a change of + 8.0 pounds at horizontal arm 627.7 (ES. 609.7) to the aircraft's basic weight and balance report. this is a computer generated form created by: Michael Donnelly ASC364.0OC WORD 6.0a: 0U08/967:13 PM • NO ADDITIONAL SHEETS ARE ATTACHED. •END• 0 Additional Sheets Are Attached SDNY_GM_02754145 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241067 EFTA01326660 . , 0 MAJOR REPAIR AND ALTERATION u.S. Drys:moil (Airframe, Powerplant, Propeller, or Appliance) "r"°""°` TochnlAvIstlea Mallalstra4.• Rs Aro.41 OMB Na 21204020 For FAA Use Only Offee Identification 554 -- Flea INSTRUCTIONS Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instruellons and dIsposIdon of thl form. This repents required bylaw (49 U.S.C. 1421). Failure to report can result Ina civil snaky not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G-IV Serial No. 1085 Nationality and Registration Mark NS8GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item 1 above 71 Powerplant Propeller Appliance Type Manufacturer 6. Conformity Stat went A. Agency's N me and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 13560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 8S258 X U.S. Certificated Mechanic Foreign Certificated Mechanic AP 1864049 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date liC6-fr￾Signature of on Indiv au. I 7. Approval for Return to Service Pursuant to the authority given persons pecified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED CI REJECTED BY FAA Flt. Standards Inspector Manufacturer x Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Ithaspon Canada Airworthiness Group Date of Approval or Rejection ide /e5 r￾certificate or Designation No. 526705494 IA gnatu of Autho' d Michael Donnelly FAA Form 37 (I I-95) This is a co efgenerated form totaled by Michael Donnelly. SDNY_GM_02754146 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241068 EFTA01326661 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identify with airman nationality and registration mark and date work completed.) In order to provide continuity during future inspections, maintenance, or alterations a true copy of this FAA form 337 must be kept with the aircraft's records as long as the alteration remains in effect. November 05, 1995. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2073.2 hours & 869 landings. Refer to the following FAA Approved Data: FAA form 8110-3, dated September 14, 1995 for Gulfstream Aerospace Model O-111 airplane, Identifying: The Dial Corp Aircraft Alteration Report No. ST4502LA-T; Titled: APU HOUR METER MONITOR Original Issue, dated September 08, 1995 — No Revisions — Pages: 1 through 14. The purpose of this alteration is to provide current limiting protection for the Auxiliary Power Unit's {APU} Electronic Control Unit {ECU} that will prevent a short circuit in the hour meter or associated wiring from affecting the normal operation of the APU. This alteration also provides a visual cue that maintenance personnel can use to monitor the operation of the APU Hour Meter. Past experience has shown that if the APU Hour Meter or associated wiring short circuits while the APU is running an unwanted APU shut down will occur and normal starting will not be possible. It has also been demonstrated that the ECU can be damaged if repeated start attempts are made with a shorted APU Hour Meter or associated circuitry. Performed all of instructions listed in the above referenced Aircraft Alteration Report. Successfully performed an APU operational test using the FAA Approved G-IV Airplane Flight Manual and while the APU was running above 95% APU RPM (+ 4 seconds time delay) verified that the APU HOUR METER MONITOR indicator was ON (dim) and pulsed (bright) approximately once every 3 seconds. Shut down the APU and verified that the APU HOUR METER MONITOR indicator was OFF. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. The effect of this alteration on the aircraft's electrical load analysis was negligible and no changes were made to the aircraft's electrical load analysis report. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. HR_MTR.DOC WORD 6.0x IIMPIS II:26 AM NO ADDMONAL SHEETS ARE ATTACHED. *MD* Cl Additional Sheets Me Attached SDNY_GM_02754 147 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241069 EFTA01326662 • U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE September 14, 1995 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream Aerospace MODEL NO. G-IV TYPE MIS RS Holkoptor. so) Airplane NAME OF APPLICANT The Dial Corp LIST OF DATA IDENTIFICATION TITLE AIRCRAFT ALTERATION REPORT Report No. ST4592LA-T APU HOUR METER ORIGINAL ISSUE No Revisions Pages: 1 through THE ABOVE DATA NAME: — 14 MONITOR dated: September B EVI D 08, 1995 ‘& BY DER DATE: ( 8, .c.)., 5I _ e i r tA° CANDIDATE September 19. 1995 Michael Donne PURPOSE OF DATA In support of Supplement Type Certificate (STC) for the Installation of Current Limiting Protection and Monitoring of the Auxiliary Power Unit's Hour Meter in the Gulfstream Aerospace G-IV Aircraft. APPLICABLE REQUIREMENTS (List specific sections) 25.1301 (a) (b) (c) (d); 25.1309 (b) 1; 25.1353 (a) (b); 25.1357 (a); and 25.1431 (c) CERTIFICATION — Under authority of appointment under Part 183 of the NONE have been vested by direction of the Administrator and In accordance Federal Aviation Regulations, data listed above and on attached examined In accordance with established procedures and Aviation Regulations. with conditions and limitations sheets numbered found to comply with applicable requirements of the Federal approval of these data these data N Recommend I (tse)Therefore M Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMBERM CLASSIFICATION(S) / 44 7 efi7 6 Z-apf John R. Chamblass NM-567 Syistems. ai tquipment (E =trio FAA Form 8110-3 (11.70) SUPERSEDES PREVIOUS EDITION T006j GET VNN0D nes Ise =craft genecated form anled OM by: (.9:oot Donnelly 9695 696 Z0L 3Y3 LS:ST 28/SO/TT SDNY_GM_02754148 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241070 EFTA01326663 SDNY_GM_02754149 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241071 EFTA01326664 SDNY_GM_02754150 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241072 EFTA01326665 a IAA AIRCRAFT REGISTRY CATIERA NO. a DATE: 5 - . - • ' MAJOR REPAIR-AND ALTERATION ligiel. — -' • - ' (Airframe, .. Powerplant, Proper, Or AppRinee) • lem Apo.. means® For FAA We Oa Offse leant-two .57:x - t e) a iNTIRUCKINS: ingthotions and penalty not to Print or roe all aunts. See FM 43.9, FM II Appendix B. and AC 43.9-1 (or subsequent ration thereat) for disposidon of dos form. This Noon Is moat by law (49 U.S.0 1421). snore to report can !teak In a ad acted $1,000 for each such *anon (Section 901 Federal Avladon Acid 199). I. Aircraft Make Gulfstream Aerospace Model G-P/ Serial No. . 1085 Nationality and Registration Mark • N8RGA" 2. COM16F . , Name (As shown on registration certificate) ; ; Mellon Financial Services Corp /13 .. . . : Address (As shown on registration as ficate) 4444 On Mellon Bank Center Pittsburgh, PA 15258 • 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make j Model Serial No. Repair Murton Airframe (As described in Item I above) X Powerplant • Propeller - • Appliance -1,Tc Mandan 6. Caforathey &maw • - . A. Agency, Name and Address B. Kind of Agency C Certificate Ne. LANCE A. MATTESON 6560 E.SAN FE LTPE DRIVE SCOTTSDALE, AZ 0.5250." X U.S. Certificated Mechanic Foreign Certificated Mechanic AP 10.64049 Certificated Repair Sudan Manta: am D. (certify the the 'w aneVor amen= made to the wills) identified in item 4 above and demnbcd on the '<verse a seachments berm have then ma to scostace with the requirements (Part 43 of the U.S. Federal Aviation Reganon, IS th.c the infosintion finished Inns is eye and area co the beatof my knowthige. • Date 2.5-0i4 +-cal. itter....- &pane of • ind z.. • d 'l • 7. Approval for Raton to Sawn Puma= to thc =betty give paces specified below, the unit tanned en etam 4 was inapsted in a manna *thothed by the Administrator of the Fulani Aviation Administration and is la APPROVED El REJECTED - BY FAA Rt. Scents Seems Manufacturer x Ramon Authorise* .i Otha (fiPendY) FAA Deep= aeprir Sluice :- ?CM= Approved by Transport - Canada Aiswordaess Orem Caen ApprOVal or /Sc --/P￾Cavan or DetisoadonNo. 526705494 IA Signsten of Authorized r Michael Donnelly FAA Fero ) • • - 4 — SDNY GM 02754151 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00241073 EFTA01326666 IAA AIRCRAFT REDGAI TSTER? .7_ 7... Fs CAnES RD* • tympani* Weight and with baler all previous or operating limitation airy, shall be entered in the appropriate aircraft record. An alteration must he alterations to conatinued conformity with the applicable Unworthiness requiranents. t Description of Work Accomplished - (If more space is required mach idelinond them. Identify with secret =keenly sod rcipstrenon mart =4 Eats work oxonktedi Form In order 337 to is provide required continuity during future inspections, maintenance and alterations a true copy of this FAA to be kept on board the aircraft as long as the alteration remains in effect. FAA March Aircraft 24, 1995. Type GulfstreaniAerospace Certificate Corporation (GAC} Model G-IV, Serial Number 1085, N8801‘ Data Sheet Al2EA. Aircraft in-service data = 1896.4 hours ft 784 landings, Service Refer to Change the following FAA Approved Data: Gulfstream Aerospace Corp. Model G-IV (GAC) Aircraft REROUTE (ASC) 234 SUBJECT: ELECTRICAL POWER (ATA 24) ESSENTIAL BUS FEEDERS — dated December 16, 1993. . _ 26, Refer dated to the following FAA Ac: ptable Data: Gullet:ream IV Computerized Maintenance Program (CMP) Revision September 30, 1994; <IIIIIIONN> denotes applicable wok code. The purpose of this alteration is to separate electrical feeder cables and remove unnecessary wire connections. bliagfiaci Removed the Left Cockoitlunction NW (30 SAD as fol km; (see figwe 2 of the above listed ASC) 1X562D16C. and discarded the following woes from comectors 305A112 and 30:MI112: 1X560016A, I X5611216B. and Removed Removed the following wires from connector 305A1P2:1X560E16A. DC561E168. and 1X562E IOC. Using the following wires from connector 305A1P12: I X560A16A: IX561A168, and I X562A16C. 1X560516A a GAC & P/N GASSOSM blue splice committed the following piths together rim the 305A I bosom plug connectors: 1X560Al6A; 1 X.561E16B & I X561;416B; and DC562E16C & I X562A16C. Removed Modified the Right Cockpit Junction Panel (10AA1 we follows. (see fig= I of the above listed ASC) 2X5621:06C. and discarded the following wires from aninecton 306AIM and 305A1113: 2X56013I 6A. 2X5611316B, and - .. . . Removed the following wires from connector 306A IN: 2X5MEMA,230611I68, and 2X562E16C. Removed the following wires from connector 305A1P13: 2X560A16A, 2X561A16B, and 2X562A16C. Using a GAC P/N GASSO5A4 blue splice connected the following pairs tOgether near the 306A —1 hottattplagesearactx 2X560E16A & 2X560A16A; 2X561E168 & 2X561A16B; and 2X562EI6C & 2X562A16C. )lgglifiggign aircraft wiring as follow, (refer to the above listed acceptable data) ill Removed accordance and with installed C43025>. Power Distniation Box in accordance with C4505@. Removed and installed lbansformer Ftectifler Unit electrical feeder cables Separated (from each other) the craning pilot's electrical feeder cables Item the exist ing copilot's break= panels. After that nth from the Pow= Distribution Box (05A2) to the pilot's (315A1) and to the copilot's (314A1) chair possible reviewing the existing approved configurations it was determined the: dorm limited wirt-ron space and separating interference the with =rating avionics and electrical installations it wu act practical to comply with the ASC's purpoae of 4244045> and left, AC / right, DC Power and essential Distribution bets feeders (from each other). Performed AC Power (26 Voh) System - Operational Ter; - Function Tat 045051>. Recorded compliance with this FAA form 337 in the Masts maintenance records and =reed the stash to Mat Same. . . No changes to the south's tier:M=1.10nd analysis Suited hem this Cation The weight effect and of balance this change on the airendrs Weight and liaise= Ins OtieigthIC and no tinges were made to the Maras sash report Buseaccepra generstai farm card by: eras Desalt WORDia 01249511M MI NO ADDRIONAL SI TS ARE ATTACHED. *END' O Additiceal Sheets Are Attached • C C al'aga SDNY_GM_02754 1 52 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241074 EFTA01326667 0 MAJOR REPAIR AND ALTERATION VI Otswena . sibuqns• (Alrlesine, Powerpl an I, Propeller, or Appliahce) . F a iat...o s ar ria Rt.Ma-a Oa as :tamp For FAA Um Ord1 Offtee Marairmatiaa a C • hOP INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-I (or subsequent :canon thereof) for Instructions and disposition of this form. This report is required by law (49 U.S C 1421). Failure to report can result In a chit penalty not to teed 51,000 for each such violation (Section 901 Federal Aviation Act-of 1958). 1. Aircraft Make - . ' Ca/Usti-mum Aerospace. Model G-IV Serial No. 1085 Nationality and Registration Mark N118GA Name (As shown on regrowth.* certigrtee) - T. Owe Mellon Financial Services Corp 03 Address (As shoat on registration certificate) 4444 One Mellon Earth Center Pittsburgh,. PA 15258 3. For FAA Use Oaly . 4. Dalt identification 5. Ten Uoit I • Model I Serial No. Repair Akeradon Airframe . , ••••••••••"••••••• (As descratird in Item. I ton) X . Powerplant Propeller SPOSts-t. .1)F " i Mahan ' • 6. CoMormith Statement ' A. Agra Name and Address ' B.- KIS of AiOnc, C. Cerlifmata N. • . LANCE A. MATTESON •• , 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X US. Certificated Mechanic ' Foreign Certificthed Mechanic AP 1864649 • Certificated Repair Slalom Manufacturer D. 1 earn the the repair ardoraltaalloa nude to the math) identified in item 4 above sad described co the reverse or atiactimerth hereto have tom mak in eat with the requirements of Pan 43 of the US. Federal Anson Regalia= end thee the information tieraithed herein 4 Se ad CPTIX310 the ben of my knowledge. Daft ... . Ai-aid/acne /per _ •• - . . . Signature 7 dua Zt . .7. Appeoral f or Return to Sank, Pornisa Adrokasterne BY to the aaboriry given persons podded below, the St identified in item 4 was Imparted leathern/met preserazd by the of the Federal Aviation Adatthistration and a OE APPROVED CI REJECTED . FAA Ft Sande* awn Mande:pm _x rasp:arm Authonzadoe . . Other (Speedy) PAA Doha" Repair Radon • Person A4Vorned by Toreson Canada Mniortainesa Grow Dale of Appomere Rejection ' 3/2.5115 - - Sarsthma or thaintien No. 526705494 u t Signature a( A r Michael Donnelly - 1 cailaPerec - „ cajole? SCINT GM_02754 153 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241075 EFTA01326668 FAA AIRCRAFT REGISTRY ^ CAKERA ro Diaz t NOTICE compatible Weight and with balance or operating limitation changes shall be enured in the appropriate aircraft record. An alteration must be all previous alterations so assure continued conformity with the applicable airwonhiness requirements. 8. Description of Work Accomplished elf rote spec is required. 11111.6 OddlUalla steers. Iskatify with aircraft =noway a a:Otani:in matt and date work completed) March 24, 1993. Gulfsircani Aetolpace Corporation (GAC) Model G-1V, Serial Number 1085, NS8GA, FAA Aircraft Type Catifintitopsta Sheet A PEA. Aircraft in-service data • 1896.4 hours & 784 landings. . . Refer to the following FAA Approved Data: FAA Form 8110-3 dated 11.22.93 for Gulfstream Model (3-IV identifying GEAR GAC drawing oust I1590D1.40140 REV C (dated 11-17.93), AXLE FI777NG ASSY MAIN LANDING • (five sheets), as FAA Approval data signed by John G. Wilder Structures DER 50-483. Refer 26. dated to the September following FAA Acceptable Data: Gulfstream IV Computerized Maintenance Program (CMP) Revision 30..1994; d 0 0 018> denotes applicable work code. The purpose of this alteration is to install bushings into the boles for both main landing gear (MLG) axle fitting locking pins. <324011> In accordance 024012> with the above lined acceptable data: lacked the aircraft: <323001>. Removed four MEG wheel assemblies: Removed <324013> <324014>. Removed four MIA brake assemblies: <324104> <724105> <324106> <324107>. i 159U:440140 (car MIA -II MEG wheel axle speed season: <324187> <324188> <324189> <324)541>. Removed the left and right GAC P/N fining assemblies. In plating accordance was with the above listed approved data: Modified both MLG axle fitting locking pin holes. Cadmium and -13 bushings done by: Able Metallic Services - FAA repair station UMBR 624K - lob* 13253. Fabricated 2 each -II painted, and (see Table I) and installed a -11 and a -13 bushing into each MLG axle fitting assembly. Prepared, Changed installed both MLG axle fitting assemblies; Left S/N CPT 5102 HSM and Right S/N CPT 5221 HSM. identification of both MLG axle fittings by lining an existing GAC P/N 11591-M40140-II and adding pi identifying mark I I590DLK114434. Note: Installed a new GAC P/N 1159L1420151-I I Ma gear axle fining locking Righi (no S/N S/N) CPT and 6152 a new GAC PIN I15912440148-13 main gear axle fining attach pin: Left SIN CPT 6121110M and 10M, into each MLG assembly. . . MLG Restored wheel the speed following so:mom equipment <324187> to original configuration is meordanee with the above lined acceptable din;,Installed four <324105> 024106> <324188> <324189> <124490>. lassalled four MLG brake assanblits; <324104> 024107>. Installed Inspected and packed all MU) wheel beesiaga <324051> <32.4.032>024053P <324054;. four MW wheel assemblies; <324011> <324012>-.02A0I3><324014>. Anti Performed -Skid System Left. Right. Funnion and Emergency Tests <324I0I> Brake Bleed mid Sakti; 424185≥012.4124n <3241i7>. PerforrnedkVbeel Brake and extension. Checked Left and Right NuteraCioi <324I03>.• Norm' AmF-SkJ4 System Pmelion Test Stodes landing gear retraction and <333001>. Saila AdfMameanti26021> <326/32$: Removed auvah fromjacks: . braking An aprimpriately operations need were pilot performed in aircraft Si %animal test and determined that ground handling and satisfactory.. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to . flight item. , , . • aircraft's The effect basic of this weight change on the iireraft's weight and balance watt neglignsfie and no changes west made logic and babnit import. - • • : - No AIMMONaMall, ATTAMIM IND° - ' 0. Additional Slats AreMated • SIDNY_GM_02754154 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFFA_00241076 EFTA01326669 TAA AIRCRAFT REGISTRY CAKERA NO •OZ DATE: - Caa Piety. /US Ctstetat 04~ Ø1O-19% 14:ff2 FI1 GLLFSTREFTI IECH4ICAL CPS TO 916122075353 P.01 I .t, Rie.C.10 OAT{:. • estnnescs.• et rotate ,,,,, ,.. stintiAk AinAlsOm AOMINI STATEMENT OF ION COMPL/ANCE ?NTH THE FEDERAL AVIATION REGULATIONS I / fj: 1. F-- qi *ARC AIRCRAFT OR AIRCRAFT COMPONENT onNintIcAnom 1 • GULFS7RE.A.M 100 V. 11k, • I TY I e (szr. Reel, It...fit...re" AIRPLANE . m as< O • AP"tc no. • GULFSTREAM AEROSPACE CORP. LIST Oit DA TN. «Mil ICATIOW . Tint • thr -q00 L.. Øl40 RENÅ C • å ' `.4 ‘‘LE F1 777 io-6. A s iv M AK) LANDI AJ 61 • i . I 6i EA . ' ...Ina " " "" Is t Dap 12E- 0% u ‘ QC byte ar-r S go cr— tvre14/.) cazum PotvGAJT • . • a•PLICAlllt PIC,IliestilTI ItI« immts• .,.. _ ~SD. FS4Z ZS. 3(33--301 CERTIFICATION al app•iament asiar • V•nle Pan 113 valiant. *Ion vianad Nil& 4ay 'Waal*, .1 tan Adaniavai «I la iteawiaact 'rid naillaira na a, laatia• Aviation' alraltlaws, kne bln isietsti ia"ataiediaci.filititiaaiikei ilia nits.. Jan ad a attacked •Lreis;* ieni --.— aid Iowa 60 c.apir ril aialiiiWi ratrikeis iagatnnega *I tie Silent Aiiataaa Iligaiatial: • I < ' ' 1;pli thra n 'lacteal.. d liarnal •I zbesidaaa (eta .. 1 .. taLAnnin dais diem YOM ', MI OF D'Vens V PtHennialMG atnitairtaTNEs Ins3g.da Tic», miadaiainil ClaSUFICatiOmi - • ' . ØN 1" F:IL1 et!..CA1 s-wirr •-•rc I 4 fl — SDNY_GM Oii54155 - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,15-, and 17 EFTA 00241077 EFTA01326670 - - SDNY GM 02754158 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241078 EFTA01326671 •-serAtait. FAA AIRCRAFT REGISTRY CAREW* NO. 3 DATE: .-o•'t="-':--aR'SPe=n••nam•I0'''"''•...-. r//Y,A>?C— hinelnag OM Ms ittint MAJOR REPAIR AND ALTERATION Pena Ma Os en ?ennoble!, Propeller, mese Mazda ewillIM (Airframe, ame= or Apatite:1i) MOINISNISR lasliteCTIONL 5h. -hoo rem or cove ail amen . See FAR 43.9. FAR 43 Appendix a. and AC 4341 (of subsequent :evasionthereof) lot invitation. ad dispositlen of this form. This moon Is required by law (49 US.0 I421). Failure to report can malt In a civil. Penalty not to exceed S 1000 for each sua violation (Section %l Federal Aviation Act or feel. I. Aireteft Mike GWfstream Aerospace Model Cr-IV Said No. INS . • Nalienably end Regientlion Mart - NSSGA 2. Owner Nemo (Al Soon on tesiarnion outs) Mellon Financial Service Corp 83 lokkess (As town celegiettelion wither) 4444 One Motion Rank Cater Pittsburgh, PA 15253 i For FAA Use Only 4. Vett Idoedibef Una Make 5. Tnie I Motlel I Sabi No. Rea Atarieloa4 X Airframe (As deeratd in Dem I above) ......ae• . Pontplant i--"; ?rood= . Appliance inal beembainer C Cirefemaley Statement A. Amalie LANCE Name A. re MATTESON d A4clom . B. Kant of Many C. Canilkma No. • X U.S. Certificated Meetenie 1660 E. SAN FELIPE DRIVE Foreign Caen/one Mechanic K0175DALE, - AP 1161041 AZ 15251 Catificerted Repair Steffen - • .Manufacturer D. I catty - ham ban that been the made repair In sxordeete mit« aternion yeah made to tha times) identified fahm 4 thaw ee4 deeded on the reverie or etadoneral the reernmette of Pert 0 oft U.S. Pedal! Arians Regalaaacs ma that the infommice feembod hetet= ead cornet Co the beg o my knowledge. .. Due • / 2. ,A......4 //Per • Signature of . bdivickel /2 .4- 2 .----- ' Plasma • .7. Awed Me Remora se Sarin asimisuarit to the of =dairy Misses:el even *visite p0 Attennetranon specified below the int identified is item 4 __impend le the roam poarlst byes and is DE APPROVED 0 REJECTED By FAA fk Swedente Smalls hienufectove . X taspacrion Anon:Lan Ole (394.14) FAA Dnepr, - Ripe Maim I Pesos Approve! by Tramped Nadir Airwoehin!drop Date ottipixovel a Rejection cetese swipe /A6•--.69-526705* 4 IA ......_ .— -.. • --„erg/P 7- r die! _.../ . micbmb onneny • -se! • • :_ is • SDNY_GM_02754157 " 44 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241079 EFTA01326672 c s FAA AIRCRAFT REGISTRY CAM RA NO. j DATE: VAY/ 79 . 7.11101- NOTICE Wel* and balance or operating ilmatslion danger skid be entered in Me appropriate aircraft moon!. An Manton must to campanile mils al previous alientions to assure continued confoemity wish the applicable sizworthiness requiem:Is. S Desciipike rdWork Accomplished Minors sews ti required. meth salmi Ma ism* Mai Sad eatheadity sedregitralan mak and dam wart camplited.) February 8, 1995. Gulfstream Aerospace Corporation (CAC) Model G-IV, Saul Number 1085, N88GA, FAA Aircraft.Type Certificate Data Sheet Al2EA. Aircraft in-service data -- 1881.0 hours & 775 landings. Refer to the following FAA Approved Data: FAA Form 8110-3 date 02-01-95 for Gulfstream Model G-IV identifying Gulfstream Aerospace Corporation drawing numbei 1159SB20470 REV .71 REWORK VERT FIN COVERS - ACCESS - ATTACH FTGS (five ‘. Sheets), as FAA Approved data signed by John G. Wilder Structures DER SO 483; and' Gulfstream Aerospace Corp. {GAC) Aircraft Service Change (ASC) 230 SUBJECT: STABILJZERS (ATA 55) PER77CAL STABILIZER ACCESS COVERS - INSTALL4 77ON OF prototype copy dated January 20, 1994 <CM? CODE 972300> The purpose of this alteration is to install remc\ able access panels on the vertical stabilizer to improve the accessibility for corrosion inspection of the vertical stabilizer/fuselage fitting and attaching hardware (interior of stabilizer). It also provides a means for inspection of the hardware that attaches the tie strap to vertical stabilizer/fu lag. attach fittings (three bolts per side). Modified the aircraft in accordance with the instructions and data contained on the above referred to drawing. Installed parts were furnished in kit form by GAC product support Savannah, GA Recorded compliance with this FAA form 339 in the aircraffs maintenance'records and returned the aircraft to flight status. The effect of this change on the aircraft's weight andisalsfise was igibk. Sind no changes were made to the aircraft's basic weight and balance nsfigitt. .S; • • Zig Jig sans sand tea inopindlir MSS Malty. IMOD - eatil3 Tani NO AIECyCKALIIIIIIIIISAliAITACIIID MOP ' O Addidonil MeAttaebed. • - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _0(1241080 EFTA01326673 r oak. no 0 MAJOR REPAIR AND ALTERATION Fee IAA Ur OS *IAr nn (Airframe, Powerphint, Propeller, or Appliance) um.. ...saga Or aflame 0CSTRUCTONS: Rees se a 130) enserson or bps el slat Sr FM U.I. FAR 43 kart B. as AZ 434-1 a Sawa nab arnerneems as ea nobta (Saba this lam. so llis mon b many by la (a U.S.C. 14213 Fan to mart en rat kt • as way a to nand $11000 ke each FessfslAanak a of 1030). I. Aircra8 Make C.uffstream Aerco Paw Model G-nr Sena] No. 1085 Nations* and Registration Matt NSSGA 7_ Owner Name (As shown on minion ccrolaa) Mellon Financial Service, Corp ff3 Address (As shoal on regamon aniffais) 4444 One Mak. Bank Caner Pittsburgh, PA 15291 3. Tea FAA Do cna, 4. lira Ideatfleadsia S. Trod Unit Make I Model Serial No. Rem Alaska Airframe (As desalcd in Item l above) , - I Powerplant N RopeBa 4. Cathnolty Staleopt A. Amnon Nan ad Alarm B. Bind of Apnoy. C. Osaka No. LANCE A. MATTESON X U.S. Cannoned Machado Ufa E. SAN FELRE DRIVE Fagg, Catifwated Mechanic ' AP Mad SCCITTSDALE.AZ SEMI Cgtifated Rana StaliCa Manitheturer Mao D. I cat* tha tha agar andier anti= made to la Inn) lamina Mama then ad dedaslad on the rent. or attsekmanta Maned have bat tank id axonlanee with the requirentoa east 43 dais U.S. Pea* Astion Ragoaketa ad rat the ictfomtaia area ins ad aerie, to the bee my knovadp. Date . /2- ar-ty sigor{ " 6al ate A - -- 7. Approval kr fan larded Natal tots rho* Sv pans upecillid below. is ma tanifisd in an 4 fa band la do ream Bred by tho Adariadwaarof as Pedal Make tartan at is m APPROVED C/ REJECTED BY •MA ft ante loa , Manufacturer s lag:action Andtaision Ode (Spot) FAA Donlan Papa Swim . Pao Approved by Tmepai Cana Manta Croup Pat of Approval pi-Rejection l - firer Clear* or Dassios ta IA a Aficba DonneBy SDNY_GM_02754159 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024108 I EFTA01326674 7. VAR AIRCRAFT REGTSTIT D - 2. - CAMERA NO. ATE* fPnit .ta. 41' 1 - e• egit i 1 NOTICE Weight and balance or ORcoltnil limilatlen changes shall be entered in the appropriate lime word. An aeration must be compatible with all previous alterations to assize continued conformity with the andiable sicraroithiness requirements 8. Description of Work Accomplished or more spree is sash atittanal theta Wean? with iticral tutonality andointealeis nark ed dew wad complatad) in order to provide contnutly during future inspections, tramenance. and aneratorts a caw of Iris FM Fan 337 Ltaicr. Repair and Alteraton is required to be kept on board the aircraft as long as the alteration remains in coact December 27. 1994. Gulfstrutm Aerospace Corporation (GAC) Model G-IV, Serial Nwnba 1085, N88GA, FAA Musa Type Certificate Data Sheet Al2EA. Aircraft in-service data vi 1856.3 hours & 763 lantings. Refer to the following FAA Approved Data: Grulfetream Aerospace (ASC} 239 SUBJECT: ICE ANDflAN PROTECTION (ATA .30) RINDMIELD IWAT -DUAL CONTROL SWITCHES dated Asyut 25, 1994. s:CMP CODE 972390>; and Gulftrcam Aerospace GIV Airplane Flight Manual Section 5 - SYSTEMS, pne 5- 40 WINDSHIELD HEAT FAA APPROVE) 4 February 1994. The purpose of this alteration is to provide independent windshield heat control for the Id front-right side and right front-left side windows. This service change adds a switch and modifies the windshield heat system wiring. Performed all of ASC-239's modification instructions effective for aircraft SIN 1085 riccit for the folowing minor deviations: (see - figure 2. Page 9) • Wire 2H537A20N was changed to 2H537A22N in ceder to fit into ground block 54 position "S*; •. Was 2.11538A20N was changed to 211538A22N in orda to fit into ground block E2 position 'flr; • Wire 211110822 was Sated into 318A1P10 position -II" because position small "IC was not available; and • Wire 2.134/ 64A22 was inserted inns 3113A1 1)10 position 1st because position small It was not available. Installed parts are listed on page 4 of ASC 239 and were furnished in kit form by GAC product support Savannah, GA. Successfully performed Windshield Heat —Operational Test in accordance with paragraph C. page 3 of ASC- 239's instructions. Recorded compliance with this FAA form 337 in the airerafts maintenance recort and rammed the aircraft to !tight status. Information on the dual switch system will be contained in Section 5 - SYSTEMS of the GPI Airplane Flight Manual, revision dated 12 July 1991 or later issue. • The effect of this change on the aircraft's electrical loading is negligible and no changes uric made to the arcraft's electrical load analysis report. The effect of this change on the aircraft's basic weight and balance was negligible and no changes were made to the airaaft's basic weight and balance report. This a • ecitiptan Reoamod form inspired by Mead Deafly. WORD 6.th 0LO2/95 3A9 Pal NO ADDMONAL SHEETS ARE ATTACHED. *DM* a Additional Sheets Are Attached 4 • ..• • a a. s • a SDNY:Gbl_02754160 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241082 EFTA01326675 FAA AIRCRAFT IIEG/STRT CAMERA WO. DATER 2 - 24 - cM . • . .e...+ q.14 er aser 0 MAJOR REPAIR AND ALTERATION resat Oat OS .. ......= (Airframe, Powerplant, Propel ler, or Appliance) I' alkni i ....ota= abet thateltatise 5»! -elk 54-Th.--nonsprs....,..... 5.. FAR Ca FAA 43 Irarials S. arid AC 4314 (a when*, man ainaf) for taborecta as rispostica crthb fern 111a non le required by Inv (40 U.S.C. 1421). Fenn to next ma resat radii only eat to eared 71 .000 for each at. station (karat 001 Friers arta M*410541. L Aarraft Make , Galan= Aerospace Model G-n, Serial No. 1085 Nancentity and Registration Mark • N88GA 2. Owner Name (As shown on natation cenifiate) Mellon Financial Services Corp #3 Address (As noon on narration cerrilleas) 4444 One Mellon Rank Center Ptttsburgh PA 15253 3. Far FAA Ust Only 4. US Idestillaitke S. Tree Unit Make I Model 1 Sall No. Ink Maim Airframe eon (As detailed in herniae* .' X Powerplat _ Propeller t 1,... —, Appliance TYR* Meaforass 4. CachnedlyStiluemeS A. Aany• Nom ad Aaiun B. Kind or Anna C. Curdles No. LANCE A. MATTESON X U.S. Certificated Mecharde MAL SAN FELIPE DRIVE Foreign Certificated Mechanic AP PUMP SCOTTSDALE. AZ NISI Certificated Remit Station Manufacturer D. lea* dim the mit. =Gs aeration roods IP the wSO) antigen a Wu 4 above and cliecabed on tha mat or thichraente line bass beat malt in secartbace with the naparemnea Mart 43 oF the U.S. Paden% Avarice Regabsfunis aid the the inform= renteted hint Is tree ad coma to the De my knowledge. Des /--- 2 1 -- eV • -4 r t Amoral for Rerun to Service Panama to the sabotity Oven pesos opocifrid below. Ike and identifier S Se 4 WY Mara baths mass pnecaboiby dm Ad:Manna of tba Faded Avalon Administer and ie CO APPROVED 0 REJECTED BY F43Fla Iltmerh brew Mamaciuter x lassos Arabothrelon CemI Preedfin FAA Drips Resit Slides. Paso Approver by Trump's% Cada' Airerombrame amp Date of Approval or Rejection Coaxes.' / - it_re 5---- ! 526705494 IA Sigottose of Autkeizedn , re---e P r Mithael Darnel& FAA Tes (01-14) SDNY_GM_02754161 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241083 EFTA01326676 FAA AIRCRAFT REGISTRY . CAMERA N0, DATE: -2- - NOTICE Weght and balance ar operatam bralterion changes shall be entered in the spiropriate aircraft record. An alnico artist be compliable with all prwitixtt litterOMOS to esame cormoned conformity with the applicable earworthiness xerroxraomti. S. Description d Work Accomplistatel (If mane mice is repay& ma= =Skald =two Woody with =matt emmohly rot 'evasion enszt sad data wort caresteied.) December 28, 1994. Gutfetrcam Aerospace Corporation (GAC) Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Cakficate Data Shea AI2EA. Aircraft in-service data = 1856.3 hours At 763 landing.- 'Refer to the following FAA Approved Data: Gulfaresm Aerospace Corp. {GAC) Aircraft Service Change , (ABC) 263 SUBJECT: PLIGHT CONTROLS (An 27) FIR VATOR BALLAST WEIGHT COVER - 'it: REYOVAL dated May 11, 1994 clalP CODE 97239th; GAC ASC-263AM1 SUBJECT: PLIGHT CONTROLS (ATA 27)21,11VATOR BALLAST WRIGHT COVES - REVOYAL dated July 15, 1994 <CMP CODE 972391)1 aid GAC ASC-263AM2 SUBJECT: PLIGHT COIVTROLS (4M 27) ELEVAPOR BALLAST WEIGHT COVER - REVOVAL dated August 26, 1994 <CMP CODE 9779yz>. Note: ASC263 Abe cancels and suPenedea ASC-263 AM1. The purpose of this Aircraft Service Change(s) is to remove ballast weight covers from the left and right elevators and rework the existing ballast weights. Removal of these Coven will provide easier access to the ballast weights for impaction purposes• thereby helping to detect and prevail the chance of corrosion in the Mire Removed left and right elevators from the aircraft in accordance with the GAC Computaized Maintenance Program (CMPI work codes 273007 and 273008. respectively. I.E.FT ELEVATOR RI El EVATOR DATE CODE 11-88 11.88 old PART No. 1159C820002-S9 1159CS10001-SIO new PART No. 1159SB40518-1 11595B40518-2 SERIAL No. 1086 1086 BALANCE DATA BEFORE ASC-243 AFTER ASC-263 0.01N/LBS NOSE HEAVY 0.0 INXISS NOSE HEAVY 17.6 INIBSNOSE HEAVY 14.6 BULBS NOSE HEAVY Performed all of ASC-203's modification instruction effective for secret S/N 1085. Installed parts are listed in ASC 263 pages 8 and 9 for Kit 1 end were furnished by GAC product support Savannah GA Performed required inaPection of both elevators end did ma fmd any conteloi Checked and balanced both clews:es in scardance with instruction Gpry Maintenance Manual Chapter 27. Installed the left and right elevators in accordance with GAC CMP codes 273007 and 273008 to tbeir proper positions on the aircraft Performed elevator control rigging check in accordance with GAC CM? code 273005 and performed gust lock system function ter in accordance with GAC Cliff code 277015. Recorded compliance with this FAA form 337 in the sixtraffs maintenance records and maenad the aircraft to flight status. • A weight change of + 10.0 pounds st horizontal arm 939 was made to the aircraft's Iconic weight and balance repot. 1= bats preyed fin "wind by: a Deadly =MD La% (WOW= 3S0 PM NO ADDITONAL MN= all ATTACHED. MOW 0 Additional Sheets Axe Attache] ‘4011116; t, • - SON Y_Gi.1 _02754162 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241084 EFTA01326677 lAA AIRCRAFT REGISTRY CAMERA NO. DATE, -2 - 3— 0 MAJOR REPAIR AND ALTERATION d ins (Airrinilei Powerplast. Pc0PcileT, Of APPIlloce) na...u.... aearem. gas a. ii Baia T. /mule oat, otrat mts. 5 1- .... -If) 6.2 baSTRUCTIONS: Pitacetypa al mod. SA* FAR 43.9. FM 43 Mose B. ind AC 43 SI de ditampara naiads bad) for norm= era dmoseto of die toed Ills roxet is WS by law (49 U.S.C. 1421). Fein to report on road Medd PIMPLY net to 077.01 /I .000 b men add doted. (Soden 90i Federal Malian Ad ofNMI I. Airasfr Make Gul (stream Aerospace Modal G-IV Saul No. INS Nabonabty and Reparation Mark NSSGA ' 2. Owns Name (Pd i/OWII on reparrabon batiks'.) Mann Financial Services Corp 03 Address (As shown on nigkitnnon terofinee) 4444 Om Menem Bank Ceiter Pbaaborgb. PA 15258 3. For FAA ties Only 4. US Idacolecalko 5. Tote Unit Make I Mudd I . Soial No. •.... RADS I allege Aidruld (As deaczthed in Item I above) nann•• ••••""n" X PowaVant Propeller APPMeco TS,* abotaatarer • -' 6. Cahn* MatemaP - A. Allays Mars ad Sao B. KIM of May I C. Cobb:m14o. LANCE A. MATTESON X U.S. Certificated Mechanic 8560 E. SAN FELIPE DRIVE Foreign Certificated Malunie AP 1864049 SCOTTSDALE. AZ ansr- Catficesed Repair Station Maitufichner D. Reify dal dta cm* wird Merton mods to Oa SION idadiRad lb item 4 toys and daienbod m Wa maw a madam= Sao in teas mai la accordmea with We againeams of Put 43 of iba U.3. Folded Masan Raplaixo ad datOretefomsodon Rostatod halm is trot and mom to the be of kacodatip. Dale ' • /i - Ze fiv o, 7. AMOS ke Ran to Santos Pam tots dadaddy zWa. yam.' apocified Maw. S a lanai:din in 4 Will ibly4dAd al Ih• =MIN pluccibid by the Adaddausor °fed hard At Aelnsieldnom and is ID APPROVED C REJECTED BY - FAA Ma Rimini. later Alddllbalset z IM*4646 ARIlltpliba ober (5pACY) . ' YAADalipab Rapt Dem Pawn Approvad bj 'troupe CS Airoottbssa Orme Date otApprovd a Itcitebon i - if- fr . cetera, *t seemboNo 526105894 IA - ' Spume of ' " ' ' Malmel DalndllY FAA In /37 (03.94) 9 - 111‘ 141/ A.: .. i1/4,44S,,,ak" .19 learela2kack-s,%.. : SDNY_GM_02754183 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241085 EFTA01326678 FAA AIRCRAFT RICERS'S CAMERA NO. DATES December 28, 1994. Gu&tram Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data 1856.3 hours & 763 bindle. Refer to the following FAA Approved Data: FAA Form 8110-3 date 12-3-93 for Gulfstream Model G-1V identifying Gulfstream Aerospace Corporation drawing number SE25201105 REPAIR, BLUED F5793.75 Rff (MAJOR) including E.O. Al dated 12/2/93, as FAA Approved data signed by John G. Wilder Structures DER SO-483. The purpose of this project is to repair damage to the Fuselage Station 793.75 bulkhead that was caused by improper engagement of the GUST LOCK system. Repaired the "-901 BLKHEAD" FS 793.75 to conform with the above listed drawing. Replaced GAC 1159C20509-26 bracket (located at Water Line 110) using MS20470AD5 rivets and optional HL18-5 hylock fasteners as required. Performed gust lock system function test in accordance with GAC CMP code 277015. Recorded compliance with this FAA form 337 in the aircraffs maintenance records and returned the aircraft to flight status. The effect of this change on the aircraft's weight and balance is negligible and no changes were made to aircraft's basic weight and balance report This is • compute mauled foon prepend by. Michael Donn*. . WORD 6.04; 01/02/95134 PM NO ADDITIONAL SHEETS ARE ATTACHED. gams D. Additional Sb:eis Are Attached • „ -airs ‘1.,;SNiertpkz., SDNY GA4 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,_02754164 and 17 EFTA_002410116 EFTA01326679 el MAJOR REPAIR AND ALTERATION 0 ii Dgaris• (Airframe, PowerpLant, Propeller, or Appliance) d Triniermim riSd 'slim Adam/40•••• a.... a 4. onacid I* FAA ow Owls Ma Ilearthasiot 5)4. eCS 0 INSTRUCTIONS Frts wtat* ad 4,117109 5MFAR 43.9. FM 43 APlakt 8. arid AC 43 9.1 (or Man aka tot) for drat rind dsposliced of ahem. Ilia report 4 oanid by WA (49 ll S.C. 1421). Faa to ran as an 4 SF MIMS nal tomad SEWS Rs wa ad. at, (Sadon 901 Federal At Ad of 1958) I. Aircraft Make Gultstream Aerospace Modal C -IV Sand No. 1085 Nationality and Registration Mark MEGA 2. Owner Name (As shown on reargion =drama) Mellon Financial Services Corp lO Address (As shown on registration mite) 4444 One Mellon Bask Calder Mahwah. PA 15258 3. For FAA Use On) • R I DS Ideadaikation S. Too Unit Make . Model Scrod No. Reps Sage Airfhme (As descobed in Imo I above) X Powerplant • PropeDer . Apphanee The Materszr 8. Cadernall7 Mallernme • A. Agiall It ad Mare . B. Sled of Agency C. Coles No. LANCE A. MATTESON 150 L SAN FELIPE DRIVE SCOTTSDALE, Al. MSS X U.S Certificated Median° FONIAP Certificated Mechanic AP 1864049 Certificated Repair Station Mandamus D. I comfy Rs the reps atm shams made to the °nth) toned ea seen 4 above ad dmatted tette more or arm= bum We tom made in empress SA the sequireinexes of Pat 43 of the US Faded At Regahaims mid din We inf=oncm fornislutl hennas trot ad cooed radiate of_m, knowledge. _ Dent Snymuie g -' •2 54- tY Ce 7. Approval for %Moro to Bona Pursuant's, WKS Om person specified bdow, the nail Sated is km 4 seerisiqoaad laths ems proositod by dis A na albs Pedant Arledge Athrdsdansion ode T APPROVED O REJECTED BY MARL DES* Rymer Minufactuter inapiciice Anaolizstkei COS (Spa) , FAA Doormat Reps Swim pan Approved by fl agon Clear Mrworthlas 0roop Date of Approval a Rejection I .7k . it Coolies et ClagmlitS146. - 52670504 IA Aril= Or . . . . ..... .....--.. Weasel balmily NI* .:+a 40 111S 110 1.%t-t.s. A EDIritaM_0275416 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241087 EFTA01326680 FAA AIRCRAFT REGISTRY CAMERA NO. 3111 DATES - 2-9 (145 NOTICE Wright and balance or operating honttoon charms shall be entered in the appropriate eirmen record. An skeleton roust be compatible with all previous alterations to assure conimued conformity with the applicable Swarthiness requirements Dnatptko of Work Accomplished Of mon sax is required. tech addctional glues Identify wish &mart ratiorckty red mom= mat end Si work completed.) November 30, 1994 Goats= Aerospace Corporation ic.Aci Model G-IV. Serial Number l06S, I.O3BGA, FAA Aircraft Type Cediticate Data Sheet AI 2EA. Aircraft in-service des - 1856.3 hours and 763 landings. Refer to the following FAA Approved Data. FAA Form 8110-3 date 12-22-93 for Gulfstreant Model G-IV identifying Gulfstream Aerospace Corp drawing number SE05813101 CORROSION REPAIR BALANCE WEIGHT INSTL AILERON as FAA Appruvcd data signed by John G. Wilder, Structures DER SO-483. The purpose of this project is to inspect and (if necessary) repair all balance weights and holding straps of the LH and RH ailerons. This inspection/repair involves: A. The removal of the left and right aileron from the aircraft B. Removing and identifying the straps and ballast weights to gain access to the balance beam assembly; C. Inspecting the weights, straps, balance beam, and attaching hardware for corrosion; D. If corrosion is found, the removal, preparation and/or treatment of the affected areas; and E. The proper. re￾assembly, balancing, and attachment of the aileron control surfaces to the aircraft. In accordance with the GAC Computerized Maintenance Program (CMP} coda 271013 and 271014 removed left and right ailerons from the aircraft Removed the 1159=0602 straps and balance weights from both Maus. Identified all taps and ballast weights for proper re-assembly and inspected balance bans assemblies. Paformal inspection of both aileron assemblies and attaching parts in accordance with the above referral to GAC Repair Dwg The inspection revealed: balance weight straps had no corrosion and Wand weights had corrosion. Performed REPAIR PROCEDURES of above relayed GAC Repair Ds% step 4. for BALANCE WEIGHTS, including um:ructions contained at Engineering Order Al for the drawing SE05813101, dated 11/21/94. Using the original I I59CS20602 straps. installed the treated aileron ballast weights to their original position with new attaching hardware. In accordance with the GAC Maintenance Manual Chapter 27-0, Flight Control Symms, check the balance of both ailerons; LH aileron 20.05 inAbs. NOSE HEAVY and RH aileron 21.89 in-Abs. NOSE HEAVY (tolawice 0-32 in/lbs ) In accordance with GAC CMP codes 271013 and 271014 re-installed the left and right ailerons to their tipper positions on the aircraft. Patterned aileron control rigging check in accordance with GAC CMP code 271005, Performed aileron manual and power system operational tests in accordance with GAC CMP coda 271001 and 271002 respectively. and performed gist lock system (erosion test in woad:ma with GAC O3.(P cede 277015. The aircraft was tan Down by two appropriately rated pilots and it was determined that the repair did not change the flight charadaistics or substantially affect the flight operation of the aircraft Recorded compliance with this FM form 337 in the aircraft's enaidenance records and =mudd the aircraft to flight status. No changes to the aintraffs weight and balance resulted from this repair. This I • mews. sad fen wpm.] by flits I Daselly. Mord t Oc OVUM 31/ fie NO ADDITICROL StIEETS AM ATTACHED. IND. Adektional Sheets Are Amidst .v?..Crta. i • SDN Y_GM_02754 166 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241088 EFTA01326681 1‘ 1431 bar --3r AA AIRC CAMERA NO. DATn 12-7-94 0 MA.JORREPAIR ADO Alin RATION us tn... - 4 ....... (Airframe, Pan-plant Propeller, or Appliance) 7444A4... - . . Mialens.• WIN. 2115013) Twat Use Ody OSC• 1416thalit* 9c - e :.il 1 inSTRuCT0NS Print or type all entries. See FAR 43.9. FAR 43 Append:A O. and AC 43.9-1 or subsequent IVYS len thereof) for illitIlaCti011S and dispootion of this form. This report is required by law (49 U.S C. 1421). Fain to report can result Ina civil penalty not to used $1000 lot each such violation (Section 901 federal Aviation Act of 19583 I. Airmail Make Gull-stream Aerospace SciaLNo. VMS Model' -IV G Nationality and Registration Mark PIMA 2. Owner Name (As shown on remotion caufiate) . MELLON FINANCIAL SERVICES CORI' 1O Address (As shown on zegimmian certalost0 4444 ONE MELLON BANK CENTER PITTSBURQL PA 157.31 3. For FAA U se (My A Don Ideonfkaaloo 5. Type Unit Make Model I Serial No. Repair I Minion Airframe .1 (As demated in Item I above) . z. . X Powerplard . . . - PropcDer • Apphance - Type. bbnatenner - IA Geothermal, Statement - _ .. A. AnneysI4aee i mad Addnea B. X Kind of Agency C. Cenifecets No. LANCE A. MATTFSON 1560 F.SAN FELIPE DRIVE SCOTTSDALE, AZ 8.5291 U.S. Certificated Mechanic - 1164049 - - Fenian Catenated Mechanic AP Coat:mated Repair Station . *Mainifactitta i D. I certify that the repast Sot Samoa made to the atri(a) identified in hem a above eat chanalied on the reverse or anectnnetas henna have been made in err:edam" with the rocrairesomus of Pin 43 of the US. Federal Aiitin Ripsistions and dim the biformoon forrisbed herein is mu and correct to the bat of isiknowlecbtA Dust 06 2 7- fly Signana c}sjit i utbonzed ' T. Approval to Rem te Servke Parsee* .1dmithansits BY the amhority given pants specified ban. the well idsmified in item 4 ow nmpened M the manna presmbed by the of the Federal Ablation Adenainion god is LEI APPROVED O REJECTED - FAA 111- S:Ndsd, bspeaer 'manufacturer r ile/peon= Ainhonation . I Other (Spsify) FAA Dengue Rept Station Palos Approved by Tramport Cards Airwatlainam Orono Dale of Amcor' or Rejection centhno• • . . Slipmtne of Authorized • ' "IPS". - . ICrIs r i Miami Dino* . FAA Perm III (9144) -- " 4 •442C4k }RFC"-rilrat - . lane SDNY GM_02754167 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241089 EFTA01326682 sells743144Wfisan661opiaafte„. eszro- 2,1 : NOTICE Wright and balance or operating !mutton changes than be entered in the appnapide aircraft record An alteration must be compatible with all previous Litt:canons to assure continued callow* with the apphcable airworthiness remonements. _ I. Desertptlen °Mork Accomplished (If mat spere is reman& mach eictitiocim slaws Wen* coat aircraft =Monate,' ad resisinsion mark en4 etas work completed) In older fp provide continuity during &Rule inspection;, maintenance. and alterations a true copy of this FM Emil 337 is fecund to be kept on board the Smart as Song as the alteration remain in effect. AUGUST 26, 1994. Gulfstreare Aerospace Corporation 'CAC} Model Cr-IV, Serial Number 1085, NM& FAA - Aircraft (Type Certificate Data Sheet Al2EA Aircraft ill-Set data - 17116.6 hours & 736 landinp. • Refer to the Mowing FAA Approved Data:- FAA Fonn 8110-3 DATE 7-1R-94, MAKE Crulfstrearn, MODEL GIV TYPE Airplane, NAME OF APPLICANT Cruftgream Aerospace Corporation, LIST OF DATA IDENTIFICATION 115%841296 (Engineering Order Al), TALE BRAKE ENHANCEMENTS, DER- R. IPESSON- SO761, SYSTEMS & EQUIP, and GAO Aircraft Seniee Change 296, Part 12 Drawing 11591430036 BO 63 Ground Spoiler Reanictor and PartM Drawing 1159SB40560 Bnkc Bungee. The purpose of this alteration is to improve `brake-by-wire ' operation by installing restrictors in series with the ground spoiler actuator input pressure ports to alleviate hydraulic demand mid modifying the brake pedal bungee's to obtain increased tension. Performed an of modification istmuctions for Part 11 and Pert Dl orGIV ASC 296 <OAP 977960>. AD pas were instaBed new and obtained from Gullet:cam Mosinee Product Support, Savannah, GA. - Removed four each Pal MS21916164 union &tato from the press= input ports (PI and P2) of the two ground spode( actuators and installed four each PM MHX031590013A R.estrictor &Pap with new "0" ring pickings, 1159020011-06let accotdance wit the instructions contained on GAC Drawing /1550430036. Reworked d each GAC P/N 1139CA0040-x Brake Pedal Butte's to P/N 11595B40560-x confagurabon in accordance with the insbuctions contained on CACThawing 11398B40503, 0W8RACEPETtea, BlthiGEE BIUKEOUT &KNEE FORCE .ADJUSTMENT Sheets 1, 2, & 3 34•3. Installed the Bake Pedal Bonne's as follows: poonort • • P/N - .WMALMNSIOti Pia MINE ccer coog Pilot's Left 1159%40360-1 0211 241 LBS. 43S LBS: 324171 Pilot's Right 1/39SB40360-2 C039 . 24.2 LBS. 43.6 LBS. 324172 Co-pilot's Lel 1159313405601 03197: ,..- 244 LBS. 433 LB& 324173 Co-plot's Right 1139SB40360-2 0337 243 LBS. 43.4 LBS. 324174 Successfully performed GAC <CMP 276001>'Caound Spodet Sittet Operatiag:fort enentiot> Whed Brake Systais￾Panaion Test and <CAW 324103> AntiSkid System-Fonction Test. • • . A Cammd Taxi operational test was conducted by two appropiately tided pilots: The pilots tested for ptoper blue response at =Ma taxi speeds from plot and copilot positions while opaaring wing flaps, goad spotless, and nose wheal steainq. No ainVI620 409 600t”cFenwitcti • Recorded compliance with this FAA form 337 in the aireratts trtailnalat/Ct to:aidsend retuned the aircraft to digit status The ef&et of this dense on the ant:ars basic weight end balance wait neftlagTh-ble end no Merges were made to the a “ad's base 'stied end baba= report. Ns hese/Poe named kiwi senewirs by. Wood bcaially. watt) ass. 01024,1;43 tai - _ NO ADDITIONAL MIMS AiLL AITAOIED. -O -Additional Shall NeAtiebat ' --7a•IrTvik SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8 SONY G , 9, 10, 15, and 17 G502754168 EFTA ornai non EFTA01326683 toured OIOD ... oda C MAJOR REPAIR AND ALTERATION ler FAA Theo oyes (Althaver, Powerplant, Propeller, or Appliance) ,............ . .... Oen 14eadmiee .0 C- r -510 evSTRUCTIONT Print Or type all entries. See FM 43.9, FM 43 Appendix 9. and AC 41.9.1 (or subsequent revision thereof) for instructiOrn and disposition of this form. This report is required by Imo (49 USG 1421). Failure t0 report can result In a cUll Penalty not to need 51.000 for each such violation (Section 90l federal Aviation Act of 1954). I. Aircraft Make Colrain:P.M Aerospace ,Model G-IV Sail No. 1085 Nationality and Registration Mark NSSGA 2. Owna Name (As aberion on repatrwion arrtificata) MELLON FINANCIAL SERVICES CORP BD Address (As thorn on reamine,n cen.Lime) 4444 ONE MELLON BANK CENTER PITTSBURGH. PA 15153 3 For FAA Vieth* .4. Uole Ideal/Ratko - - Line Unt Make I Model I Sall No. • Repair Ann Airframe (Ai described in Item I above) X . • Powaplant , \ ... Propeller Anoltance TYPe Mmttfattarer - a. Cadermay Matemeor A. Matey, Sc. end Addreas .. • A. KW of Niamey . C. Octilkela No. LANCE A. MATTESON X U.S. Catifaceled Weber& 8548 E. SAN FELIPE DRIVE port Lea ca4theatal Mechanic AP 1864149 SCOTTSDALE, AZ ISM Catfitated Rata &Mae I Martufaataa D. I ratify t the repair mar Mention node to the onn(s) identified m non 4 stow and &Shed oa the muse or gtschwints hem have two made in r.conLince wilt the napineemm of Pan 43 of ths US. Faded ArketooltecoMions me that the incantation furnished hem" is true nod coned to thebera 0 my lascrwiedge Owe g 7- ft( friPernrefirralrifrldrE. -----.7.C„ e C, 7. Approval for Reran le awake Ps MIS wrap &V pemommacifiM below. the unit HSU! la item 4 was torplaae ha the mew prescolve by the . Ahead. Attie Petted Avilioe Adoiron and S 0 APPROVED 0 REJECTED BY FAA Pk Or WS taps Mandictura x lxvictica AildiCS31% .0her(Srpeci(y) . I : FAA Dmipm Rise; 48691. . .. . Pawn Approved by Tnospxt CisinAtecedirsettittop . Dale plApprova or Rejection .8 — Z9' -s V °AIM. IF " , DeOritialt.- SISM5491 Lt gpaRpm Of Michael Donnefry • I M-4.D.O/I0/4..",.. • •••• • ••••• SONY GM_02754169 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00241091 EFTA01326684 FM AIRCRAFT CAMTRA NO. ISIKY DATE: 12 -9- 74 • NOTICE Weight and balance or operating thretabon changes shall be entered in the appropriate airerae reconi An alteration must be cons pa olge with all previous alterations to ass= continued cantos:miry with the applicable airworthiness 11881801:Mall3. 8. Dvscriptlec of Work Accomplished of more spice is remand. each adduiciutl them. thmtity with that mdonally and mist mark and dee work completed.) in order to provide cordhurty during future inspections, maintenance, and alterations a true copy of this FAA Form 337 is required to be kept on board the aircraft as long as the alteration remain in effect AUGUST:26. 1994. Gulhtream Aerospace Corporation (GAC) Model G-IV. Said Number 1085, N880A, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-savice data ••• 1786.6 hours. & 736 landings. Refs to the following FAA Approved Dalt GAC Aircraft Service Change (MC} 232, SUBJECT: ICE AND RAIN PROTECTION (ATA 30) WING TEMPERAWRE LOW MESSAGE — PROVISIONS, dated December 17, 1993. The purpose of this alteration is to activate the "WING TEMP LOW" message (Amber) on the Engine Instruments Crew Alerting System (EICAS) and mask alert if the wing has not reached 100 &tors Fahrenheit after two minutes from being selected ON. Performed all of ASC 232's modification instructions effective fOr A/C 1085 except for the following minor dm.iations: • Coacplt Overhead Panel: Existing wires1H151D20, IFINA20, 2H151C20, and 2E126A20 were replaced with new NSW. 22759116-17 to ft GA0335)4L22DS contacts provided with new wing anti-ice:wit. Avioniat Shelf Assemblies: Al added wire connections to the Fault Warning Computer(s) and Data Acquisition Diggs) 'Mt made directly to the rack <on:tenons) Stead or through the shelf disconnects. Main Junction and Relay Panel: Wets IH152F22 and I.H152X22 was remove from T113M positions If and G respectively and spliced together. Win 2H152.1G2 and 2H152F22 way rand from T720 position G and K respectively and spliced Wither. Wire H9076B22 was spike to wire 1H1S2Y22 near Data Acquisition US MI, 95A4PIB pia, 17. Wire H9071322 was spliced to wire 211i 32T22 near Dan Acquisition Und 12, 95A5FIB pin 17. Wen /49078A22 and H9078AA22 were spliced bribe( with wire I HI87D22 nor connector NAINC pin 89. Wires k19079A22 and 119079AA22 were spliced togetha with wire 2H1I37Dn near connector Nmptc pin 91. . AU of the deviations that wire made to the apprerred design %Senecessary to provide for compatibility with existing approved configurations: It has been determined that the deviation made did no after the intent or operation of the approved eiraeft savice change, • • -- - • • All parts were provided in kit fotro and obtained from Gulf:strain Arrospece Produh Ruppert, Savannah, GA Sucossfully performed ASC 732's operational lest. Recorded compliance with this FAA loon 337 in the aircraft's rneintenan ce records and reigned the aircraft to flight . . _ The effort of thirchange at the aircraft's basic weight and balance was negligible and no changes sect rna..te to the aircraft's hthic weight and balance mon. lli.as =war romiud fonaprrmul br. aOdsI Omani,' WOAD 6 Oa 01/2691Strt PY NO ADDMONAL stores AtEMTACIIED •E`te 0 Additional Sheets Are Atractu:d • • ST-,- .• • ....atejalate-, J . • 4 . .klietialHAPP4 1 7:7- -.7 ••• ' -1;4 • • • • SDNY GM_02754170 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241092 EFTA01326685 P =nth • CA1CRA SO. I DATE: I 2 _ 7_ 94 ram Cow :If On I2 MAJOR REPAIR AND ALTERATION Fiera manse us tarown en ' -- - (Airframe, Powerplatot, Plojoeller, Or Appliance) sr...seer ..... Me kleatifisetian 2e (,- ics4 O INSTRUCTIONS: Mot of type an entries. See FAR 41% FAA 43 Appendix U. and AC 43.91 (or subsequent revision !Steen for insqintions and disposition of this form. This report Is required by Una (49 US C. 1421K Failure t report Can result Is a civil mobil, not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1950). 1. Aircraft Mats Gulfstream Aerospace￾Model ' G-IV Said No. 1085 Nae003MY DM Rogistsation Matt NSSGA 2. Owner Name (As Amen on Illtalle01/ califlone) ' MELLON FINANCIAL SERVICES CORP ICI Address (As shown onDOS:Sion Patina.) 4444 ONE MELLON BANK CENTER PITTSBURGH. PA 15253 3—For FAA Uwe Ott A Unit Mead:Sena= Unit Make 5. Tne • ' . I Model I Sail No. papa Minion Airttame *r n :••••••••••"'• (As desenled in Item:above) X Pow*** Propeller TYPe hernefieraree 6. ConterenttY Swetweseed A. AP:00 9Tleme and Address B. Rind of Amoy C. Cctk*s No. LANCE A. MATTESON X US. Certificated Mechanic. A - 856$ E. SAN FELIPE DRIVE FeeWen Catifioded Mechmic ' AP 1364049 SCOTTSDALE, AZ 332.58 Certificated Rosa SUM* Manufacturer : D. I certify that the rep* endior ekeraion male to the noi(e) identified in item 4 tow end detailed on the &vav or enachmenu lino have tem male hi leatednoce with the :Neiman= *Pr 43 of the U.S. Fedenl Avisean Replaeom and via the infixivenon fornithed her* earn wad coma to the bed of my Dunned* 9 -,77 rr G. 7.' Apart:9M for Return to Savke Patio the ember* given moons specified Mk* the ant identified in son 4 win hopeaed in the wanner tresedbed by the Aflisizeloratthe Fail Avid= Admlainice and IF OD APPROVED 0 REJECTED BY FAA De an* Menu:Setae* X **Mon Awhothation Other (speedy) FAA Nips Rep& Station I Paton Approved by Troop* CUBIC" MIWOOkillall. Cecesp Date of Apperef or RMection • - 9 — a9-- IY comma., Brit= of Deeps* we . 526705494 IA' • Michael Dcamay SDNY GM 02754171 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241093 EFTA01326686 -=.;,17.17...-4.-fttrftralle„wPnenaNCeinwinvan'7"-'7, IM Allts.RAnlatTgr - - CAHEPA NO. DATE: 1 2_ 7_ 94 NOTICE • Wright and balance or operating limitation changes shall be entered in the amperage aircraft record. An alteration tut be compatible with all previous aluranons to assure continued conformity with the applicable airworthiness re:pit-tents. I. Desaiptien el Work Accomplished (if more span b required, attach addeacual sheet identify wida entry and regnewrion mark rid der a work compleuct.) In order to provide continuity during future inspections, maintenance, and alterations a true copy of this FAA Fame 3371$ required to be kept on boird the aircraft as king as the alteration remain in effect. AUGUST 26, 1990. Gulfstream Aerospace Corporation (GAC} Model O-1V. Serial Number 1085, N886A, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 1786.6 hours & 736 landings. Refer to the following FAA Approved Data GAC Aircraft Sent Change (5C) 255,.SUIEUECT: INSTRUMENTS (ATA 31) SNAPSHOT SWITCH INSTALLATION, dated May 5, 1994. - The purpose of this alteration is to provide thc crew with a switch that recants engine parameten in both Fault Warning Computer's (FWC) non VI)Litilc memory. Paformcd all of ASC 255's modification instmcdons effective for A/C 1085 except for the following minor deviations: • • Cockpit Overhead Panel: Installed - SNAPSHOT- switch ASC255DSI on overhead panel in the spare vacant position adjacent to APU fire test switch. Comucted ASC2.55XDSI switch tin wiring as follows: Pint...are FD9030A22N to ground block E2 pin W; in 2 wire FD90213A22 to 318A1P7 pin small U; no why Jumper 22 to Pin IT,all wire FD9030B12 to ground block E2 pint Pins 5 79 All no connections: MA wire W5281.022 to172N Pin D: punBwcc FD9029A22 to ocancrior 31ILAIP7 pin small V; and pin 1p wire FD9031A22 to commenter 318A1P7* small W. • Avionics Shelf Assemblies: Connected wins from 318A1P7J1 ai follows: pin small U wire F09028B22 to Annannator tights Dim and Test Box- 29AIP2C pat 11; pin small V wise Fusvats/2 spliced to wires FD9029C22 and FC9029D22connected to FWC I I •95A IPIA pin 81 and FWC a 2 95A2P1A pin 81, respectively, and pm tan W wire FD9031B22 to Annunciator Dan and Test Box-29AIP2C pin 64. All added wire connections to the Fault Warning Computer(s) and Annunciator Lights Dim ted Test Box were made directly to the rack conneenx(s) instead of through the shelf diatom:Cs. All of the deviations that were made to the appnived design Were necessary to provide for compatibility with aiding approved eccfignaticra and allow both pilots access to the - SNAPSHOT" switch. It has been determined that the deviations made did not alter the intent or operation of the appoval aircraft service change. . • .. • - All parts were ptirdiased from GulfstrearnAaraiiiiiiProdurit finning. Sawing, GA. Successfully_perfamed ASC 255'S nperational test Recorded compliance witlithis FAA form 337 in the aircraft matte reteds and retuned the aircraft to flight stains. • • The effect of ibis their 'dotal load =WW2's %alibi =abaft. Fair fair t eNAFSHOr swath indieaas, is from the o' HEAD LTS PWR 02 aieuit breaker -8HAPRHOr Sint lamp mane &ow (When snapshot switch is prayed or during wanting fights tesOkssthan 02 ats in tnighit10.05 till in . . . The effect of this change on the aircraft's basic weight aid balance w® negligible wid charges were made to the ainitaft's basic weight and balance report • - . NO ADDMONAL man, An AlTACRED •19-496 a Pidmonal MO= Are Attached z..s. - •yrv.ne!-I;+wfrr￾ti ' I • -en h •-J-h 4i l % SDNY_GM_02754172 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241094 EFTA01326687 Fe .... csa X. norm 0 MAJOR REPAIR AND ALTERATION r 1 r nAth•oute (Airframe, Powerplant, Propeller, or Appliance) terns tilat••••• des,, siScarica 4 ts c ,. / .0 " iRSTRuCTIONS: Print or type all entries. See FAR 43.9: FAR 43 Appendix El. and AC 43.91 (or subsequehe revision thereat for instructions an disposition of this lone. This report ts required by Ire (49 US C. I421). Falun to report can result loaded penalty not to exceed 51,000 for each s Leh 'violation (Section 901 Federal Artaterin Act of 1950). I. Aircraft Make CulTstream Aerospace Model G-IV Said No. 1085 Natisnably aid Reettalion Mack MISGA 2. Owner Name (A. shown on repartee enflame) MELLON FINANCIAL SERVICES CORE' SS Address (As town orimgetricion eatiame) 4441 ONE MELLON BANK CENTER ' PITTSBURGH, PA 15253 1 For FAA Us• °ray 4. Unk Ideonacetke 5. Tmee LIM Mt Model I Sail No. Repro APCIelon Mfrs (As dosentedis It •••••••••• ... . X Pomp= Proper -.. , Appellate TYPe Mamba= 6. CaMormity Staley= - ... - A. Aspera Nine and Addis B. Kind of Apnc C COMPlitlo: ' LANCE A. MATTESON X U.S. Caicos Mecksinic , 1360 E. SAN FELIPE DRIVE. Foram Catifteatesi Med= AP ISSN= SCOTTSDALE, AZ ISISS Catificated Repair Stag m —Manufsetura D. I catty Mt the rep & and/or aced= rude to the asps) idatitud ict item 4 above ad deaMed on the mime or metements hereto bevy been made m read= wilt the repherrenta of Pert 43 of the U.S. Pedant Let Replalems end dm the informar forentiest hicas is troe and cord to the Mom knowledge. , Date V /eV ------- r r 7. Approval for Remo to Sas Pmassatw the =MeV given ponces specified below the MI Acidified to dome me impeded SS razor preembest by dm Methstamor calm Federal Awallcm Adrolestralice ands 02 APPROVED O REJECTED BY FAA SR palm& ars Nasseactunr x thapciSionAtabodation c ater(Spedy) , FAADeepene . t Peprix &Rion Pawn Approved by Trietsgoet Casts Airouthiosse cheap Dine of Approve( or Rejection 8 —/s--- 5° se Ccormft.w N .' Desiengtee .526" M S IA • Signature of Assatotized ' - r SDNY_CM_027541T3 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241095 EFTA01326688 NOTICE Weals and balance or operating limitation changes shall be entered in the appropiate aircraft record. An alteration must be • compatible with all previous alterations to asnre continued conformity with the applicable airworthiness requirements. & Dentriptlea of Work Accompllthed - at more epee is required. each deuced Mesta dairy web secret ciacualny and minion mat and die work peefeiseet.) In order to provide continuity during future inspections, maintenance. and alterationfsv anlioopy of this FM Finn 337 is required to be kept on board the aircraft as long as the alteration ' in effect. AUGUST 14. 1994. Galant:am Aerospace Corporation (CAC) Model O.1V, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet AI 2EA. Aircraft in-snee data = 1786.6 hours & 736 landioid.' Refer to the following FAA Approved Data: Gulfstrcam Aerospace Corporation Aircraft Service Change (ASC} 295 SUBJECT: AIR CONDIT7010110 (ATA 21) CABIN PRESSURE* MANUAL CONTROL DVS7'ALLA77ON dated JULY 22, 1994. <CM? CODE 972950> The purpose of this alteration is to allow the cabin 'air pressure control to revert to snuff operation in the event 115 VAC power to the pressurization system is lost. Presently, if 115 VAC power is lost, the air pressure transducer and the outflow valve will fat - 32.5AI KI 0 MODIFICATION: Price to preforming ASC-295's modification instantiate modified the eating mita Ray & lunction pond to provide for expansion Removed 8, discarded Sating May 315A1K10, Deutsch P/N E4104 385; Exacted all of the wires from socket 315AI XXI°, and Removed te discarded relay socket 315A1XKIO, Damsels P/N 65009004.513. Installed a new Deutsch P/N 65009001.513 relay soda at eft position 32.5AIXKI0 & connected existing wires as follows: WI33D22 • A1; W132F22 - A2; H9014A20 - B1; H9015A2ON - 82; H9013A20 - B3; 09056A20 XI; & G52A2ON - XL ASC 295 DEVIATIONS: Instant:dancer Deutsch P/N 65039-008-513 relay socket adjacent to nil position 325A DOC 10 (see above) and identified as ASC295XKI instead of the relay, socket and bit listed in ASC 295. Perforated all of the wising changes shown on Figure 4 of ASC 295's irectructiont amp wires DU/113B20V and DIOICC2OV wee asserted into 326A I P200 and 326A112.00 (espectively) potation P instead of era T. After completing edam and ring out. installed a new Leach P/N 1A-W4F-005 (aka GA11335590 unto socket ASC295XX1. All of the entailed pasts were purchased from GAC Product Support Savannah, GA. Successfully pained the installation checkout listed in Paragraph B pages 4, 5. and 6 of ASC 295 instructions. Recanted =Same with the FAA font 337th thitherafrs maintenance records and returned the aircraft to flight sums. It has been detennined that the intarebaimehip between this dungy and any previously approved cooftpration will not introduce any adverse effect upon the arworthinionfthe aircraft This deemxinalion includes, but is not boded to. My modifications or deviations made did not atter Pa EMI of the approved ancralt service change; Mum performing its maided functions the operation is augment; No %at manual smedameras are require& and the installation is compatible at all previous therations assuring continuous conformity with the appleable ithWOOthilleSS requiremmts. The effect of this change on the airgartelicititial lee4ing twill be 0.03 amps added to the CABIN PRESS 115V thieuit breaker, essential 115 VACIstes:j...s, _ • ... She act of this change on the airtisfei basic weight and bitten— negligible and no changes were made to the aircraft's busk weight and balancereport • - . . .. • aercaor pared En nal by. Itdst 'Decal WOIUM ON - tandem SAMS - NO ADDMONAL !MEM All Ansium tat 0 Additional Sheets Art Attached • "fr,,'. _ st: .e' • -a • _art....c-s,--?entifilsaselleSill*Pere7 . . • . .t • -44, :•••• SDNY_GM_02754 1 74 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241096 EFTA01326689 0 MAJOR REPAIR AND ALTERATION ,.....",4 MOM tine= /It IAA Ono Oily Oilkelocoirsaise . 4-ec - t's % fnoea (Airframe, Powerplant, Propeller, or Appliance) ,..SAME 'Simla MIR insminions and penalty not to Print or type anentries. See FAR 43.9. FAR 43 Appendix It and AC 43.9.1 (or subse trent revision thew!) for disposition of thks form. This report is required by law (49 uS.C. 1421). failure to report no result Ina clod weed 51,000 foe taco such violation (Section 901 federal Aviation Act of 19S 0). I. Antraft Mae Gulfstream Aerospace Model G-IV No. 1085 Nationalny and Registration Matt NSSGA 2. Owned Name (As thorn on niftstraticat arena) MELLON FINANCIAL SERVICES CORPUS Addams (AS IbOVIa 011ttOttri011 OlitiliCOW) 4444 ONE MELLON BANK CENTER ' PITTSBURGH, PA 152.58 3.. For FAA Use Thdl 4. US IdeollIcanon S. Type Unit Mae Repair Aturadon Akers (At da 1. miadin Itmn I Mon) "'in n " ********** X Powaplant Practise .. Ng Msarthamer • . — fa Coneamily Surat A. Aisayb Nine and Addreee IS KIM Mir C. Caeca No. LANCE A. MATTESON $560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 11525$ X US. Certificated Mechanic Patio Catificared Mechanic AP MOMS Cation& Pamir Station Minobetatex D. I nary IS me rapt and/or anion made to the imiaNdaithed in Eno 4 Mon and deeedbed on the myna or inedanento beneo have boa wade in sem= nth the requiems= of Put 43 of the U.S-Fedeni MIS= Rem and that the informetioo fandsbad tonin is tree =ad =tett° the bac my lamededid Dan )—ts,-5,y SiPar 418 d 7. Anomalies Rearm to Scoriae Parent to the ..homy given perms specified barer. W non Modified an in 4 misspend Isi dome= preamlied by the Azteanmeor ate Facet minion Adman:aim =dal Ila APPROVED 0 REJECTED .. BY AAA Ft Semd•d• boon Memitactunar I Inspechou Ambocintion 9!1, 1(3$410 Empalme* Rent Mann Person wawa by Daemon • • • Camila Anwortkbas Oran Data of Approval ar Rejection efrr/95 1 mama. or - RearefiaaM . ST 6703494 IA Sipoovre of _... 7 .-otti ,„,," MichaelDonndly tareen511(0.494) • SIJNY' brA 0175417r • teces_1-•• • ...-.:Atalusa.: • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241097 EFTA01326690 • - • Icis,vksoi.:,:;1 AttarrAfgYegir,it M AIRC CA KERA NO. i • 12-7-94 -• • Wei Nana ght and balance or compatible with all previous °Mating Limitation changes dun be altered in the appropriate atrcraR reo,rd. An alteration must be alterations to assure continued conformity with the applicable throcorthiness ro:ryercmcnts. S. tamertyttea of Week Accomplished (If more apaar a main& math %attired thects. Itlesity with siren& nsionatity and "misuse= an and claw wed cors[plaied.) FAA in older ram to 337 provide continuity during Mute inspections, maintenance, and altmations a true copy of this is requited to be kept on baud the aircraft as bog as the alteration tetnain in effect . Aircraft AUGUST Type 14, Certificate 1994. Gulf:ream Aerospace Cbrporation (GAC) Model G-1V, Serial Number 1085, P/88GA, FAA Data Sheet Al 2EA Artraft in-service data - 1786.6 hours & 736 hmdings. Refer to the following FAA Appired Data: Gulfstrcam Aerospace Corporation Aircraft Service Change DECEMBER fASC) 313 SUBJECT: P 4TICS (4E4 3e9 OWN PRESSURI Z477QMSTABILIZaj77ON dged 17, 1994. aCODE ••• 973130> - 7 The purpose of this alteration is to reduce the cabin pressure rate changes that cocoa dicing rapid power lever 18 reductions PSIG at high altitude. This alteration provides an electrical circuit to reset bleed air pressure regulation from descent. without to 30 PSIG ANTI when the power levers are retarded below pedestal quadrant angle In • retarded power lever -ICE oft manifold pressure is maintained above 20 FS1G. This circuit is routed 2500 FT AGL horn mute through the relay, disabling the circuit when this relay is activated Selection of any AN1T-ICE function also disables this circuit. ASC 313 INSTALLATION AND DEVIATIONS: position near 32.3AIXKS8 and Installed • new Death P/N 65009-001.513 relay socket into a vacant tad Performed all of identified the socket as ASC31350: I instead of the relay, socket end thicket hued m ASC 313. Wires D0002820 the and wiring changes shown on Figures 3 and 6 of ASC 31Ts ismachons. wept for the following deviations: 09002A20 were insetted into 326AI P200 and 326A11200 (respectively) positions Warm D9004A20 instead of maga; Vises D9004820.139004C20. and D9004B20 were inserted into 326AIP2OP and 326A11200 (respectively) position It instead of small/ D9007A22N was and H428C20 was inserted into 326AIT/16 M positions K. L, & AI Despettively)-, Wire installed a new emoted into ground block El position/AMOS of El 1 positio' n lit After completing weirs and rigout, parbased from leach GAC P/N Prod= .1-W4N005 relay (aka. OAR833NRI) Ito socket ASC313XK1. AD of the installed pars were Support Swainish. GA. SurionsfullY Performed Service Basin Numbs the 3399022-36-1646 instatheion checkout hated mEaragnph E pee 3 of ASC 313's instructiess. Note-Athed Signal • removing UPPER pylon panel has ban previously comPled wild Valves 541.1 and Sala we accessible by 2 on the impactive side. Recorded compliance with this FAA form 337 in the Scat's roShmance records and returned the aircraft to flight status. It has been determined that the intentiarionslths between this change rd any pthiously approved configuration , fla not modifications /misdate any or adverse deviations effect made upon the airworthiness of the aircraft This determination indudes, but is not limited to: My fime5orts the operation a did not aka the intimt of the approved aircraft service Mange, What performing Its intended previous durations assuring automatic continuous No flight manual supplement! are required; and the instillation is compotthle with al • cont.:achy with the applicabk airworthiness requarements. SPEED The effect BRAKEFLAP of this change ALARM en the airmars dectried le:dinged] be 1.7 crops added to the etseraid de bid (0.1t7•5 apgsb CB 242 and 0225 to CB 262 SINGLE PACK). " basic The effect wthda of and this balance change on the aimata basic Weigth and botanic was regfigilde and no changes were made to aiseraft's repth. nit • sthow wens twos w4nNel . . woometiiiitareniAsAgraiatcr'laar 0 Addi6ortal Meets 4r6 Matited 1 • SDNY_GM_02754176 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00741098 EFTA01326691 MIMMIUME CAA A J. *WRAF I ELGISIR ' • • _ SSW Cif -LI__ • - - 410 MAJOR REPAIR AND ALTERATION I......... 010 Wm IFeC Yet IAA CM OM con anasnaaos -k -elio (Alston., Prewarplant, Propeller, at Appliance) .17nme•••• n....... =IONS: Mat at .5 type as autos. St• FAA 43.9. FAA 43 APMMix F. and inunations and disposition of tint fn. This report's swim! by Lt. (49 U. penalty me 10 o(4•4 SI.000 N4 atell such Sanaa Manion SO I NOM' Avi9 AC 43.9.1 lot subsequitot nation thentoh for C. 14214 Nan to report tan rank initial. Ion Act of 195t. I. Mud Mac • Gal Wean Aerospace Model GEV Saul No. IOU ?humbly and Registration Nick NRSGA 2. Ouns ;we on nentenatai cenifcia) MIANCIAL SERVICES CORP CI Address (Ai shorn on nista= catalog') 4444 ONE MELLON RANK CENTER PITTSBURGH, PA Ina 1 VAR rm Use 0.1, i Ts US Nib Met ( Sod No Ramat Alan -...• . I Airtnans ii hem I 'bow) ••••••••••••••"*" Amanita • • Propsila Aglow • / - Paseasst ik• clear hA. mows to el Mira 1 a Kad of Any C. Lea A. MA11111074 I U.S Catiticated Metric • BMA E. RAN MAT Darn Foreign Cated Modal* 3COTTSDALE. AZ MSS Cataloged Raw Stet MCGLaktita D. I amity Os ma ncnr Sas alma en ion. tint(s) tataitt iii le 4 eon mod dtecolect asactinata bona Monad bap on ends a .ccida• Ina the rapzirentan of Pot 43 of as Us Feint Nat dr adeassecc bac A Cup isl carat to ths falconry teowk4Alt Drs e- 1 7- f y sis ottaiis . . r7 4"1C.S. 2 7. Afarenitse Rani liana Mfluml IF 41* 4411A4sY lima A MASS Sow. tap ana itathid ia Ilmi 4 Me arapiard a is !me pandasa ages Aiwa of tht Fadden Avalon Asa•tatfon ad in IS APPROVED 0 REJECTED . BY " IA A. goon sir c bon ltscan z talon Acarsige . . IFAA Dagen taps Oro- PO= Ascend by halm dadamworttrnan Oro. Du of Approni a Rejection I . - ? ta -sr O..§...- osem...N. OWNS M -:- • sone of Alameda 41;iC: II 01 edictal Donnelly Sigiczaldifida;a ss SDNY_GPA_02754 177 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241099 EFTA01326692 -,› -."- 1•1~ ""4- • .iii;!~~1h‘4 - ir> NOTICE 0'i:imperilla Weght and wØ balance al or opetalang I/sic:ion chars& shell be as in the approrrale sacral mooed M alteration must be previous iheriaoniiii aware ~cod conformity mA the applicable erwarchiness requirements. . IL Deeertentia at week AconaplIdad (If mon spice ie required. such Slams Mesta Idera4 tab meal ~ay tad ~es mat wad ear wort complated3 In FM ceder Form to provide 337 conanurty during Mure Inspections. manteranoe. and Wistaria:a a true copy of this is requited to In kept on board the aircraft as king as the alteration remain in effect. Aircraft AUGUST Type 26, I Amapa Corporation (CAC) Model G-IV. Serial Number 1085. N88GA, FAA Sheet Al 2EA. Aircraft ia-testcc der. - 1786.6 bows & 736 landings. MODEL Refer to the GIV, f Approved Da FAA Fin 8110-3 DATE 7-18-94, MAICE Gudaream. DATA NAME OF APPLICANT Glace= Aerospace Corporal" LIST OF DER￾IDE N 11595B41296 (Er#coring Order Al), TITLE BRAKE ENHANCEMENTS, 11391130036 R. 1 761, SYSTEMS & EQUIP; and GAC Aireraft Service Change 296, part II Drawing EO Spoiler Restrica and Pal III Drawing 1159SH40560 Brake Beppu The purpose of this alteration t ss ve 'brake-by-wire' operation by inctalling i • restrictors in series with the actuator input pressure ports to alkriate hydraulic demand and mod e pedal bungec's to obtain increased tension. Removed fox each P/N 14521916164 union the prom= and ~led four tech P/N 1111X0515900BA Pernietor anew with new the inetructims oanlainal on GAC Draw" 1159H30036 Rorocked 4 each GAC PJN 1159C40040-x Bake PØ Bunsee's to P/N in:new-tiros contal on GAC Gnaws-113951340503 GIV BRAKE P ADJUSTMENT Shea 1,2, d 3 of 3 installed the large Pedal Sungois POQITION PM Noes Left 11395B405c0-1 Plot's RIP! 1159584)540-2 Co-plot's Led 115958405681 Co-pkit's Pistil 115958405682 ~ton Soccaufully Tat performed w GAC <CUP 226001> Gromid Spot System Operaliaral-TaL <CUP 3241 CUP 324103> Araararl Syslan-Fonetion Test A Ground Ttn operator* ten toes conducted by two mar* need pion. The pion tested normal tam speeds rap:sued from pilot and copilot par vitae apaazo wars 6W, ground galas, and nom wheel mama No Randal omsprnrice with am FAA km 337 oM acerbailiess ~is allleallhe Smart to tit& tar: The weight effect and of laince eta Sir report ante cafes be ale ett ben sup ~sit and es Saw we :irk b the as at, taus main emsear mews as ornedby MSS De* rap 911 182 ArlaaeaL fl An ardzsan • O Adderana Shaft An Attached SDNY GM_027541 78 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241100 EFTA01326693 4 4.1MV:4-. - " COS4Ir SDNY GM 02754179. r........d PO. 1 . zsara 0 MAJOR REPAIR AND ALTERATION for'AA UM 0ST of trmiore (Alsfrome, Power',lant, Propeller, or Appliance) odes sort= ••••••• - • • once stem. .OC -Tc9o. INSTRUCTIONS Rant Of (We ap hisries. Sae FAR 43.9, FM 43 rsIMehdit I, and AC 43.9.1 for subsequent revision thereof) for instructions and dhposirion of t tons. This repott Is rrpoinKI in law 09 U.S.C. 14213 Fare t report can nook in a civil ONINNY nor to xreed 51,04:* for sigh sigh violation (Section al lederld knal_Kin MI Or 195 M. I. Airettit Stake • Gulfstresin Aerospace Mudd G -IV &coal No 1085 Netionthrysnd Repstntion Dar NM IGA 2. Owner on mama astfaa FINANCIAL SERVICES CORP ID Address (As am on tearoom merwast 4444 ONE MELLON BANE CENTER ' PITIIISURGM PA 15153 • . re FAA Us Or V( ern ..... ..,.... 3 --e—r tin. Unr bake E. ' z Model i Sala No. Roar ARM Aillinne 3.z. r in Ilan I MOM) .""nnann....4) X Power*/ Pads Appian. TYP4 leadmin -.. • - . 46 Carlear ii A. Adencys ram ad Addams ' B. lad of Apia C W. e• LANCE A. RIATTEXPI X C 5. Calthairod - ass L SAN nun DRIVE Foam Cat&ad Manic . sco th at's.. AZ suss Cantina Rani St . Monufocturcr - D. I cettifytho the repel Sot nemoott may to 1b ads) identad Sao 4 toe. .4 a: Ma andsnato tonso lim Oa easy is exordia ea a mamas of Put 41010o U.S. Total Aviata the leforrace fined ems a vois a coma to IS aro amass. . ig- 7T PV - • -........ , - t the to ocaerete Pm to tat =dairy pat pima spaled tolom the Ens tarifa bar 4 am lacral Idea m presinal by Oa Ariziammos ads Federal Mince Abollstrean rod I le APPROVED CI REJECTED • ... BY rna no nem . bent I gessax r z moon Ammo I Dan Oran . FAA D*We , Ferep in . • Peen Aparmay Tampa Can oinnerdos thump 1 DSc of Amaral or ROMS . • . 8 - it -1 ef . • Dolblia' 130". to copsol• Spaof .--- . -laicbod Dandy SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 00241101 EFTA01326694 • . - ..••••••=0,C-- S. Discerns el Week AoremplIsbal Of more smog is rent& cab elation& ass. Mandy anni vane neanaley and memo. ant sad ids work complseed.) In FAA order Form to provide 337 continuity during future inspecans, maintenance, and Mashers a true copy of thri. is isduesd to be kept an board the ant at long es the effetattan remain rn effect. AUGUST Aircraft Type 26, Catifi 1994. dulfstraan Aerospace Corporation (GACI Mole 0-IV. Sant Number 1085, NIOIGA, FAA Al2EA. Aircraft iirt,irdas - 1786.6 hours 736 ender Refer to the Ze.t b L / GAC Aircraft Service One {ASO S. SUBJECT': ICE AND RAIN 14/9EltATURE LOW MESSACiE - PAW/MONS. dead Dextriba 17, 1993. Thu pnapose of this n to activate the "WING TEMP LOW" message (Amber) on the &tax Fahrcmhrit (EICAS) and await ahartinse W4 ha net reached 100 degree' of err two ".:,: from bean selected ON. Main Junction and Relay Punt Wires I/4152222 and 1H1525C2 was and spliced together. Wires 2/4151202 and 2/1152922 wee removed from spaced together to win Wee 211I321'22 49076W vas salsa trifle IH152Y22 near Data Accpsisibm 1, 95MPIB pm 17. Rive 1{907-E 22 wr rear Data acepaintion Unit al, 95A5PIEI pia 17. VT together yeah win 1H IIDDI2 rear connseur Z9A !PIC pa 29. The MN 2H127021 near armada 29A1P1C pa 91. All of the devatiorn tint were mode to the approved design were prinide for append configundiens rotting approved strain hint been dreamt:bad tic the dentin neck did not alts the of the service dew All parts were prodded in kit form ad obtained from Galina Aerospace Predict Support. Staessfolly performed ASC 232's operatieral test • Reorded compliance with thin FAA Co® 337 m the Irate essantermai meads aid maned Altus to night surcrafra The etTect name of this weight chaise on the wen& a basic weir sod beamed we saaphigaiie sod no dames were made to the and balm report .• sew. gene eine pnind kbanal Deal, WOW it Sam 12i MI ACIDECENALSts a MLLE* Vla, - . - - - igui.ake'S • - .42 : - cre,triLl MbNyfiM_ 02764180 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241102 EFTA01326695 .Nragitr • Agt5,O3c-stki-: •PJAU• giCa • • .•IrrnAr ican ft.. - O MAJOR REPAIR AND ALTERATION tart* Ms Ody karat strnmoorma (Aldine. Powerplant. Propeller, or Appliance) " SIIIISSIL caw ension <SC-IC:SO a INSTRUCTIONS: Print or type all entries. See FM 43 43. fah 43 Appendix B. and irstructiom and disposition of this form. Thin report is required be a (49 U S renal' not to $1,000 for each such violation (Section 901 reclitral Arial lon AC 43.94 lot subsequent revision thereon for C. 1421) Failure to report can result inst.& Act o119$8), ...tfted I. Arad Make . . Gullatreasa Aerospace - Mood . &Iv • i Sol No. f I i.: . - - Nerionelity mid Registration Meek • NIIIIGA 2. Owner N •• . ; 2%9. (WPM awakes) ?....,.. ME r • N . - ANCIAL SERVICES CORP Ni Address (Astor' on regltrIDOTI rands.) 4444 ONE MELLON BANK CENTER - PITTSBURGH, PA 13251 IA Li!, 3. Fee IAA Use OWE •.• . id. . 4. 4 Mee Make . '3. Eno I I - MOM No. • Riper Monies Airbag • . . • ..................... • kem I above) ""•• •••44'.•••5•••• I ' Parepleat 4? Panels -'' • Afars rAlle - e Wein. ne , • A. ava . C soil A lean Ned Adana , B. KIM essay - C. Cedar LANCE A. nunnot4 . L U.S. CerOficated Meekest - IMO E. SAN FILM DRIVE Foreits Catibrated Mecheltie AP iCOTTSOA&S, AZ CUSS .... Caticated Repast &Mx° •• D.' I ready OM ' Lain hew bee the =do rep* gator Swami sea to Os moo) itateed is lea 4 Move al dessolool as Ike• is ecconlosse wee Oa loam of Pen 43 of dr U.3. Feast Avalon Repletion fniskett Owe haat Simi ad eat MS toe ofem keesderce i i~ • 8-27 Tr' • - 7. Antwel lar Rents MUM= Pecom Admeriersor la Ms of MilmaY do Peeing Pva Minion PKocia Adiseserneas vides Wow. die me ideemilotbea 4 rt e sweat S a pemobel by the ode IC APPIIOVED CI REJECTED FAA Pril .. lo lawn Meoutectusu x tropecocei Aatkorabos COM BY (MediY) .•: e. FAA Cram . a Repot Meioa Puma Approved by Ira,* . Clesdeknortkixo. arose- .• f . Due olApprorel Or Rqsdion ' . • . , .0-/P: ety ,: claienencle BiOriYe of. a , is--- UMW li .. Milton Domani),e aunt ••••••C A 401 _ 14/ ,1V12/4 r a . / i SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241103 EFTA01326696 ran. OncirlIV•Cilttlil "Mr Or S. Eleserlptha of Aoosatellead Of more spa is walks& wrack alatione then karata Mm acre carnally wet regent= ®t ins dee wort completed.) In order to provide continuity dung future inspections mainteranCe. and atterabons a true copy of MIA FAA Form 337 m requited to be kept on board the aircraft as long as the alteration remain 07 effect. AUGUST 26, 1994. Gulfs-bozo Aerospace Corporation (GAC) Mryfrl G.W. Serial Number 1085. N88GA. FAA Aircraft Type Sheet A 12EA Allyn* in-urn= deta - 1786.6 holm 4 736 Landings • GAC Aetna Sense Chace IAJC1 255. SUBJECT. INSIROMENTSCATASI). SNAPSHOT TION, dead May 5, 1924 The putpae of a to provide the an wattles/rich that meta engine parameters in both Fait Wunmg C) tita What memory • swath ASC2.55DSI on overhead penal in the spot Watt position 1 nvitch socket wince se fakers: bid want FD9030AZ/N to groutal small U; an,2 wee Jumper 72 totall bp..! wire P090)0822 to bred SII521041022 to Dv Pn D pia wire FD9029A22 to CODDSCIDI 31/A1111 On ail W. Avkaske Shelf Asa/sales: Connected • 31/A1P7.11 Who Dim and Tee Box - VA1F2C pit 11; pasmall V win FD90298 to F9/C a 1 -95A1FIA pm 81 tad riVC 12 - 95A2F1A pin SI, rospece Dim sod Tat Scot - 29A1P2C pit 64. AD added wee oomeetara to th and Toe Box were trade deo* to the rack con:to(s) instead ofthn All of the &viatica, die was made to the spermod Jess was approved ocinftgurations aid allow both pilots soca, to the deviations mode did is alter the intent or %cram of the The effect of this chapati& brash'. decd load imelya, ml be cesais. Poser it the 01- switch macaw! b from the O'HEAD LTS MR 12 an totter. -SNAPSHOT* Slaw Sop ONUS doe (when snaphot math a pressed or dorms amnia haws tea) a kas than 0.1 amps in hoe/ wid 9.05 amp 4 dia. The e ffeet of this Mange on the turaaft's basic triad rat Saes wee timalaiat Sat orb Ohara were made to the ureraft's belie weight and balance report. Tao Ammar swired Da 'mond Y. ISSN Dear. VOIDGAD - - -araftavarvit. - " SDNY_GM_02754182 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 164 EFTA01326697 -"finar. f 4"0 17, 4/ MLFTM t pilsesal MO ii• 'MO 0 • MAJOR REPAIR AND ALTERATION """Oi°" album...N. (Metros, Poweeplawf, Propeller, et Appilmmt) I ol l Sulam . oats iiaftaa Ps C. cit) -' IMSTaut. lama Print or type a atria. Sera FAA 43.9. ma 43 hofaCilY I. and C.0 .04 (Co 7 revision thereof) for Mar imtnakon and disposition of tiro fora. This report b Cro a (49 US C. 1421). Foam to mart can result Mocha nbc to flied $ 1 000 for each such Vaal (Socha a I Fedora Avalon Act of Phi A. Mahe I. Aland • Cantinas AerospaCe Modd C-IV Seril No IOW lalicaity tad Regiongan Mach MEGA Name (A• than on raposica calicia) 2. Ow= FINANCIAL SERVICES CORP ID Address (As Sm on ropengeo cseakos) 4444 ONZ MELLON BANK ONTER ' PITTSBURGH. PA IS= K Fe FAA Moamar 3. T • Use MIS MOOd i TO No. Ems Aberaton Aflame ii lam I above) • X Powniot Nopio Appleton TIPP ear & Calliallif A hag, as al Adam B. Cad of Aorta C Oaks Na. LANCE A. MATTLIOPI I U.S. Colligated ISM L SAN MAIM DRIVE Fonda Catificaled ' SCOTTSDALE. AZ na Certificated Rept Swim Mamba= D. I catty Oa the ea* aka dna ads to ra sa(4) trassad in tan4 tow a chicasd atachtsas tea ay Ear aide is oxonlatat a sk a taantats of PEI 43 of the U.S. Falai Arta a Cam toad area a free ad coma to a toot of ley ardatap Dia g/i 574V Seam of - r 7. Manna he Rao an Serb Palacio a sakarysia pa= sada bast ink madled nes 4 es saidai ia r as pada by is AtIsmanta arch' Fad At Adamant:a ad a NI APPROVED 0 REJECTED BY arta aria ~ oar Maatiams i havato• Athcastaa Car (acity) FAA lawn Emir San Pm Amara by Tim - A•liall= Croup Dub MN:rani or Rooftop <9 —/s---tre (Noises toosumato SWOON IA Sessen of Aabooad .ti LadDcrttny :440;; .• SDNY_GM_027S4183 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241105 EFTA01326698 • ••••••laellWat 0-AL--tzww f - SDNY GM_02754184 L Osseripliso tifWarkAcomplishwl (r moo specs is ropiest. WI adorned raw teisaelip sin secret swot wit rssinormo mR wet de week completed) In ader to provide contmudy during Uwe inspections, maintenance. and alterations a bus copy a this FM Fare 337 is' raptured tote kept on bored the acre as en; as the alteration remain m effect. AUGUST 14, 1994. Gukstrean Aerospace Corporation (GACI Model G-N, Serial Number 1085, NSSGA, FAA Ain:raft Type Grams. Dm Sheet AMA. Attest in-ten-ice dots 1716.6 Ian & 736 Labs", Rr1aW the f• Approved Data: Gulfs:ram Aerospace Corporation Aircraft Service Change (MC) ECT: AIR CONDITIONING (4 TA 21) CABIN PRESSURE MANUAL 27ON dated JULY 22, 1994. <CKI3CODE 972930> is to agow the cabin a prams control 10 mat to manual operation in the the Pronorialace sYllao s lot Pow*, d l l s VAC power is lost, the prance trordocu'' the outflow 1. fast Gre -295's modification irstractesas aiodified the existing 325AI Relay & Skins relay 3.25AIK10, Datoch P/N E4161383; Waded .1 relay socket 325A 'XXI°, Dana& P/N 65009-004513, nil position 325AI X1(10 a connected miens wires es folows ON - ft2, HS0BA20 83; GPOSSA20 - XI; tG52A2ON - JCL A3C 795 DEVIATIONS: binged& new tort Wee) 500O421.513 Sty socket .4—S to tad position 325A DO(IO (see and identical as ASC295)3C I instead , socket sod chops shown on Papa 4 of ASC 295's outruceons, orator wets DI01 306AI P200 Grid 326A11200 (vispectrody) pontoon P 'mead of ma/ Leecii P/N )A-W4P-005 fake GASSUSV I) Sao wicket ASC295XILL Proctoo Support Saverrsh. Safully performed the installation cluck= lined in It has been determined that the intentimonship between this Mere and my previa.* approved introduce my adverse effect upon the sinvotainess of Ur sacral Thu dconeznation includes, tea modifications or damsons made did not aka tee ouent of a y e approved acrid Sat comae, finis the operation n cal-WC; No .y..anal Illadat. an Ian. al a instslistion mynas thereon wwiame comnisous conframsy with the applicable lindens requittrena The effect of this change on the turcists electrical leading sill be 0.03 ads .dried to the circuit breaker. mental 115 VAC bus, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241106 EFTA01326699 CAPTLl AVE CIE* t I I tit'ArWli 0 MAJOR REPAIR AND ALTERATION dit...p.om, si... sea QUrfreeee, Poweeplant, Propeller, or Appliance) eassem ISseeecimi Per >Maw - fa /AA CS 0.7 Ma Swedes Oc - r'5 N: rPISTRUCT1ONS: Print a type all *Win See FAR • 3.9. FM 43 Appendix 8. and AC 43.91 (or subsequent revision Immo for 1miructions and disposition or this tom. Tile report a required by La (49 U.S C. 1421). Failure to tenon can Mule In a dull penally nor to ineetlyi)00 for each wan violation (Section 901 federal Aviation Art of 19$03 I. Ararat Mat! . GUItlatItOl Aerostat Model G-IV Said No. INS Neicasfaty ad Repose= Me& NESGA Name (As eon • on reqiernlion ainifiese) 2 On, FINANCIAL SERVICES CORP 83 Address (Moot oe spite CM/OW 4444 ONE MELLON BANK CEYTtE ' PITTSBURGH, PA ln,5$ 3. Per FAA Da OAF 1441180:alleei lat Sin. IM .1,4. Model I Sal No Ian Alan Aida in IC I non •4•4••••••••••••••• X Pollan Ropier Awing A. las Hafaa ...... tr ad Ada B. InSof th Ceedweein Ma L LANCE A. MATIII3ON C Cant No. la L. SAN PXLI72 DRIVE SCDITSDALL AZ I52 X U.S. Cancan M Fora Carnicated oda Coat:aged Recta Stilton Meaufectura D. I catty Os LS Mai laSS Ca =an COI Sant a is 4 non ad Cad sac Into a Co ton ta nora wit In intonate of Put 43 of the U.S. Feta Annia dr ietosaina rand balsa ad correa to tbr On of dry Inntolda. De sr?" , n r Panto 7. Anent Ihir Roan 14 Sinn Athreirrair BY S. of aciry the Foal wee Avan roan Ack•irrairs speccese Wort d at at an and ma 4 we spa al as clad by dit PA* Ft Vine sad if TH APPROVED 0 REJECTED ales Ineadlacera x Cocoon tontonan C84(39 442) FAADonate Rata Ca Pa Apron by Tact Coda AnOrda Group IC of Awron or Ration eln-A7 Catama a' eW s Dia SWAM% IA f - - ad.." Mai Dan! SDNY_GM_02754 185 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241107 EFTA01326700 cmam knout? itionike - 7st NOTICE • Weight and balance or operating Enutation change shall • compete with all be eared in to appropriate aircraft mead An ateranon must be previous alterations to assure continued confonsity with the triable Sworthiness reqtarments. & Dratelpelir fl ak Asearlabed at mole Nee a Molted and elationst tees Ids* wan at Mosley ad mite= eark ed des wart scallt&) In FAA order Form to 337 provide continuity dunng future inspections. marrtenenoe, and alterations a true copy of Ss is' required to be kept on board the amnia as by as the alteration remain in t. Aims& AUGUST Type 14, 1594. Chaste= Aerospace Corporation (CAC) Model G-1V, Serial Number 1085, N8SGA, FAA Certificate Dsta Sheet Al2EA. Auctift meertia Si - 3736.6 hors & 736 landuigs. Rder to the f (ASC) 313 S DECEMBER 1 Approved Data: Whitman Aaospace Corporation Aircraft Service Change NEUM,477CS (ATA 36) CABIN PRESSURIZ427ONSTABIILZa71ON dated <-CMP CODE 973130> The ptirpose of on is to reduce the cabin prelate rite changes thud occur during maid power lever reductions at high This situation provides/selected came to reset bleed air pressure regulation 18 PSIG from descent, without to 30 PSI the power leen at retard below pedestal guide= angle. Ina retarded power Ice ont manifold 2.500 FT Ala is saintsical above 20 PSIG. This cured is tuned through the ban mute relay, nen this relay is sciarded. Selection of any Awn-ICE function also disables this camas. ASC 313 PLSTALLATICAN AND portion near 315AIRKSB and idattified Performed all of the wiring changes shown • new Deulach PIN 65009-001-513 relay socket ins a scant veil 13XK1 indeed of the relay, scar and basket listed in ASC 313. Wan D9002B20 and D9002A30 6 of ASC 313's insertions, except fir the following deviriena Wee D9004A20 ad iltre - P200 sod 326A11203 (rospectivdy) potion S Used ofd: D9004820 were Woes D9004820, D9061C20. I F200 and 326A (reepectiwely) position R hued of nag D9007A22N was Seated ad H4D3C20 we anted into 326A1T/1 R. L. & ht (respectivdy); Ws insad a new Leh P/N Son Wound 1110& E2 Parton M Sued of El a Ala completer war and erg a µnehued from GAC Pet 1-W4N-005 Dawn relay (aka GAR835NRI) into 13XK1. Al of the staled pats wee Savannah, GA Service Suocessfuly Bolen performed Number the szatim checkout toted in Pesegark E p ASC 311's weruchons Note- Athed Signal remota UPPER pylon pod 3395012-36-1646 hie been ;mks* complied Veins 54/1 and 5412 ire accesuble by I on be reapers stele Recorded complasoce at. this FAA loan 137 n the masts so elmave rant end tamed the It has been daermerad that the ersernelstionstup beta= this damps and say previolaty appeared introduce any 'draw act upon the *wartime* dee Sat 7Ls debaxeration artudes, but incekfrations or ember reide did not aka the thank athe approval swath service change, fimetems the opcestion es automata; No Oar m.mdagWbmno are nescirot, and the instance prrnous allenziors estanng tie ceakanity Mt tie sppwatietimatticest rearms. - . • bar The act °Ishii chore on the saszar's SAMS lotd.. will be 1.75sssd as the sate SPEED BRAKETLAP ALA1Ud ad 0275 ki CB 20 44.014 Pa . . status. Any its intended at an S imps to CB 2C The as of els charge on the raarabatMasi✓tetalSSekgR bre wage and Slam apart . selidre are was ode to the .Stmt's Ths • • aria 'seal in needale INSI9TiS TARDY% ,.a. .imismiscrion. ocAddikvo.kkensAs!. - • . etlt raintsgtiatoaarief irarstirrz _n--zi j* • 2:40vjz;,: .c.,.2 • Geo:4_027541R SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 I 08 EFTA01326701 lntar ' eV' FAA AIRCRAFT REGISTRY nien,,, CAMERA NO. / DATE: 5' - /7 - MAJOR REPAIR AND ALTEEATION - Cracow= (Airframe, Powerplant, Propeller, or trace) .......... re..... .. ".......... own. Ila4a . ....AA visor, • OM. Mereneeriaa - - ra4,,, 0L - 63° INSIRuODONS: Prat or type el flies. See FM .3.9. FM 43 Appease 8. sed AC 43 9-I (aassns! Mann Mt banlanns ad trnensmen a this lam 1S read is rebind by lav (MI U.S.C. t421! Fates to typal as real Ins di pasty not to eragied SLOW breath Bah seam (Seem. 901 Federal Melton Ns of MM. • I. Aircraft Mike Collette= Aertasptce Modd - C-IV Serial No. 1085 Nalionsbly and Reese:Woo Mark NMIGA 2. Ovals Name (As show a reparation an -am) ACFIUM LEASING CORP Adam (As sawn on remake certacas) FOUR EMBARCADERO CTR SAN FRANCISCO, CA 94111 3. For FAA Fry Only 4. Volt Ithogaleadoe 5.Type Ural Ma I Modd I &dal No. Repair Mat= Airframe • 4•••••••••••••••• (As dosed:4d in 11 I above) see...... X Powaplant Propeller - Appiamca 1 '. Alsobtrans • A Cakemilly Stien=8/1 • 'A Stilt and Address B. Kind of Away C Cantata No. LANCE A MATEESON • . 9560 E. SAN FELIPE DRIVE SCOMDALE, AZ MSS X U.S. Caticated Me trans .,-• F044881Cartthesleil Medmmic AP.1164049 CatSated Emma Station liamaimturer D. Inesty Math/mak wellor Mormon waft so the eat(s) identified mama above and 6nenlad m the rasa a ancesawn kneto an lam mens in acerdiace Caul nquiteemas or Pat 43 of Ma at Fare ' Itagalskaw aid tha the informs:on forawhorl baron is mu ad coma lo the beet o my lambda& Date .1-ff-ty . .&gitatal f ri f - 7. Anneal for Rearm *Arles Persosot to the antharty given peon specified below. Me onit idatiEsd in be4 vs Spa mare Ana pass wad by the Mitnineracer of the Federal Ariake talon and is XI APPROVED C EMCEED BY FAA Ft ausbrei twat Mandato= ' x laspecOmMahceimicas . sons (Spicily) FAA Dadposa Rep* Station Pam Approve! by Tr dada Afrwarthinea Oroap Den Approval or Ftewtoon --- WO V - . eat Dmielam am 3267950% IA MbNYCM 027541g7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241109 EFTA01326702 "ra￾t eflitigf rY FAA AIRCRAFT REGISTRY a y CAMERA NO. / DATE: 4 NOTICE WM& and bolus a °Paging limilabon dears ant be :raced in the sisnipsu lir alf LIMOS. An austionroust be compeale with a0 previous altastiont to assure continued conformity with the applicable airwortbineas remoraocnts. & Desoiptke of Work Aromapllabed (rm= apace b oppoired. cad: eddtionet aka Ida* with &ad rsiterty act ranmaion mart ad de wort _.plead.) March 18, 1994. Gotham-am Aerospace Corporation {GAC} Model G-IV, Saul Number 1085, NUGA, FAA Aircraft Type Catificate Data Sherd AMA.. Aircraft ea-service data = 1629.9 hours & 669 landinp. Refer to the following FAA Approved Data: Oulfstream Aerospace Corporation Aircraft Service Change {ASC} 298 SUBJECT: PNEUMATICS (ATA 36) BLEED AIR ISOLATION VALVE RELAY- POWER SOURCE MODIFICATION dated February 16, 1994. <CMP CODE 972980> • The purpose of this alters\ on is to separate the power source fete bleed air isolation valve control relay from the bleed air isolation valve relay. Presently, both relays are powered from the same 28 VDC circuit breaker. This ASC installs an 'AC' control relay for the valve control relay which will eliminate the possibility of a single fault causing a false cockpit indication. Performed all of ASC-298's modification instructions effective for aircraft Say: 1085. Installed parts are listed in ASC 225 page 8 and were furnished in kit form by GAC product support Savannah, GA￾Successfully performed GAC CMP code 361064 Bleed Air Isolation Shut Off Valve operational tests. Using the FAA Approved G-IV Aircraft Flight Manual operated the Auxiliary Power Unit and started both main engines and verified that the APU AIR. LOAD, ENGINE START or CRANK, and the ISOLATION. VALVE cockpit switches performed their intended &actions. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. The effect of this change on the aircraft's electrical loading is negligible and no changes were made to the aircraft's electrical load analySis report The effect of this change on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report as a caupgar anered Am nand W waded DNS* WOW It - mliS%roll AM. NO AOCIELMAL =EU ARS ATIACHIZI *DM' O Atationd Sheet Are Attached SDNY_GM_02754188 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241110 EFTA01326703 ITMlEartj`‘N .,. FAA AIRCRAFT REGISTRY CAMERA NO. /A/ DATE : 7. 7y ® MAJOR REPAIR AND ALTERATION 011 Nall esommomi (Airframe, Powerplant, Propeller, or Appliance) rain Jae rain tat - spas PO to alga larAA On CI* MN Idadfuriee SOL "Frf 04 7 nismucTIONS: Pont or type all entries. See FM 43.9. FAR 43 Appendix II and AC 43.9-1 (or subsequent revision Menial for instructions and dii position of this form. This report is required by law (49 US C. 1421). Failure t report on result In a civil _penalty not to exceed 51.000 for each such violation (Season 901 Federal Aviation Act of 19SM. I. Mace{ -/ Maki Gurnee-earn Aerospace Model tG-IV . __ _ Said No. 1085 Natiornfity and Registration Mark N88GA 2. Owner Name (As shown on registration itertillette) • ACEIUNI LEASING CORP Adam (As Omni on rewaration cannons) FOUR EMBARCADERO CTR SAN FRANCISCO, CA %III 3. For FAA Dee Only 4. Unit liken/Ronan S. Taft unit . Make i Model I Saial No. Repair ( Murton Airframe (As described in Item I above) X Powerplent Propelkr Appliance 1Wo .... Mcderesar 4 6. Carkirozety Steteroad A. Mean Nome and Masai B. Kind of Agony. C. Certaczne No. LANCE A. MATTESON IMO E. SAN FELIPE DRIVE SCOTTSDALE, AZ 35253 X U.S. Catiksted Mechanic Foreign Catilicated Mechanic AP Ilan Catifacated Repair Station Manufacturer D. leanly that the repo mace ammo =de to due mai) Identified in bane above sod described o the reverse armaments hereto have been made in accord= with the To:Orem/nu of Pone) of the U.S FLOM Mama Regithikas aid tha the inkemetion famished bate is ow sad Ceelitt lo the ben of my knowledge. Dale . . . 15/ signor s2: _.......4 i• 7. Approval for Ran to Pnn to the orthodry given groom spooned below. the toth'clemithed in Om 4 era inspected ia the re= pracrOxd by the Achennirwar of du Federal Mission Attraninion sada CII APPROVED 0 REJECTED BY FAA FILM..Mt Sinew Mamtfacturer x basevaion Azahodation Other (ePedY) FAA Designee - Repair Station Pews Approved by Tampon Cola Mit Group Cote of Approve/ or Rejection -4 - 1 Ct' -- , y Ovens o or Signals{ of Mahatma Yydividtrajf nisstise. . - 52670504 IA a<a P r Michael Donnelly 47-Ca5V4ilinrmt44 44emt :4 "1" Biarrinerre gi lW4 9WY,4.79"'"'"" - ).. SDNY_CM:027541EIS SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFIA_00241111 EFTA01326704 "2"."-": TE'443E-A"r FAA AIRCRAFT REGISTRY • CAMERA NO. A DATE: V: Z 5.4 79 NOTICE Weight and balance or operating limitation changes null be attend in the appropriate aircraft teoxd An alteration must be compatible with all previous alterations to assure continued conftxmity with the embattle airwoethiness poluiremalb. a. DesaiptIon of Work Accomplished (If mom space is reqvized meat adtmenal abeam Wan* with eiremft atmaayaadrapsomlon mark and drat wort completed) February 42, 1994 Gulfstrearn Aerospace Corporation (GAC) Model -1V, G Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet AI2EA. Aircraft in-service data • 1611.7 hours & 6611andings. I- -- Rettig° the following FAA Approved Data: Aircraft Service Change {ASC} 225 SUBJECT: LIGHTS mu 33) NOSE GEAR TAXI LIGHTS MODIFICATION dated November 1, 1993. CMP CODE 972250> The purpose of this alteration is to modify the nose gear taxi light mounting bmck,etry to provide optimum visibility. It also changes-the center taxi light from a spot light to a flood light which will eliminate shadows. This service change also replaces an existing circuit breaker and taxi light housing assemblies. Performed all of ASC-225's modification instructions effective for aircraft SiN -1085. Installed parts are listed in ASC 225 page 4 and were furnished in kit form by GAC product.support Savannah GA. Performed Al of die steps listed hi paragraph "C. Perform nose landing gear retraction to ensure clearance of taxi lights" and noted an interference problem between the GAC P/N 1159EL20064 Wire Bundle Support Bracket, refer to Page 6 Figure 2 View A-A and the Nose 1. ceding Gear fruition assembly. Corrected problem by trimming the leading edge of the bracket to provide properclearance and noted no other abnormal or unusual conditions. Successfully; performed all of the steps listed in paragraph "D. Perform operational test as follows:" and noted no abnormal or unusual results. In addition, checked taxi light operation individually and collectively to verify proper circuit breaker configuration; and Checked the operation of the Nose Wheel Stearog System with taxi lights ON and OFF and noted no abnormal or unusual results. Recorded compliance with this FAA fora 337 in the aircraft's marntenance records and returned the aircraft to night status. The effect of this change on the aircraft's electrical loading is -150 VA (watts) added to the Right Main AC BUS during tan light operation. Note: Taxi light operation is inhibited if the landing gear is not down and rocked; See ASC 131 <CMP cede 971310> TAXI LT POSMVE CONTROL for details. The effect of this change on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. This u “ 0900 gonad In cosmos er blictrel Dawn". wow) re 01/12/94 AM NO ADDITICNAI MEM% AU AlTACHID •@C. O Adcbtanal Shona Are Attached -et,r ----t aeArremila;visatiarlerlpreltroSta 4.•- •”:—n-el:t • ?••‘•• SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SDNY_GM 15,_02754190 and 17 EFTA_00241 112 EFTA01326705 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3.3'_ 94 . . 44.. , a MAJOR REPAIR AND ALTERATION US Down arraspras s (Airframe, Powerplant, Propeller, or Appliance) IMMO Minn ...A... ..••••••• ars liii imam Per FAA 136.047 Mee Idesidoeics 5 6t -Fl; e INSTRUCTIONS: Instructions and penalty not to Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent tuition thereof) for disposition of this form. This report is readied by LtIV (49 USG 14211. Failure to report an result In a civil aceecl S1.000 for each such violation ISection 901 Federal Aviation ACt of 19581. . . I. Aircraft Make . Gulfstrearn Aerospace Modd G-IV Serial No. 1095 , Nationality end Registration Mark N8SGA 2. Owner Name (As shown on resimsion cattate) BA Leasing & Capital Corp. Address (As 'bon on on cache) Two Embareadero Center San Fraoelsco, Ca 94111 3. For FAA Use Only 4. Unit laden/Ranee S. Two Unit Mike I Model I Serial No. Repair Abrasion Ai sine (As desinbed in Ilan F above) X Powerplant Propeller • AppiAnce TYPe. Manufacturer 6. Cordonsity Statemeat 2,6trays Nano end &Mpg. B Kind of Agency I C. Candle= No. - LANCE A. MATTESON SSW E. SAN PXLIPE DPJFE SCoTTSDALEAZ 957.59 X I U.S. Certificated Mechanic Fo ten Catificated Mechanic • I AP 1964049 I Certificated Repair Stition I . /donut:wrote: • D. I Cc* that the repair ounce akeration made to the ak(e) Mantled in done above mid demntied on the name or smechmada hut° have been made in accordance ..t the requiratoma of Pun 43 of the U.S. Federal Aviation Revelations and that the infcmtation ft:mashed herein is trot and coma to the beat a my knowledge Date 5 7, /94- , Signaltne e° dged hl&i2 `s.3 C .. / 7. ApproerJ for Return to Service Pornau to the anthoray peen persons Adminssiraa of ihe Federal Aviation spoofed below. the tmi Waged la kern 4 was maponed in the =OM poncaled by the Administration and is On APPROVED 0 REJECTED BY FAA Flt. Seaderds I learn manutu er rw x ineptennn Andwason Ma (Specify) FAADesignee Repair Sudan Poison Approved by Tampon Coale Atribeti1 Oro Date of Approval of Rejection 5,5-74--7./9 93 1 rostrums re Dettgataa. No. • S2670S494 IA l . :, . of A ' 'air Illiire- -- - ../ ' ...--P Michmi Doll:WHY -riAliewarliaek4.1169(Gtogniper-aas SDNY_GM_02754191. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_002411 l3 EFTA01326706 FAA AIRCRAFT REGISTRY CAMERA NO. 3 tun: 3- 3- 94- NOTICE Weight and balance or operating limitabon changes shall be entered in the appropriate aircraft motel. An attention rough< compatible with z0 previous alterations to assize continued conics:miry with du applicable einenntencas requirements. S. Desorption of Work Accompllsbed (If more space a recpung oh additional theets. Way* with trawl nitionalny and regstrzion mart and data work completed.) September 7, 1993, Gulfstream Aerospace Corporation {GAC} Model G-IV S/N 1085, N88GA, FAA Type Certificate Data Sheet AI2EA, Revision 18. Airmail total time in service 1493.6 hourt and 608 landings. Refer to: FAA Approved GAC Aircraft Service Change (ASC) No. 176 Subject: LANDING GEAR (ATA 32) NOSE WHEEL STEERING FAILURE - ANNUNCIATION dated February 23, 1993. Effective for Aircraft serial numbers 1000-1214. The purpose of this alteration is to add a pressure switch and circuitry to alert the crew of a problem in the nose wheel steering system prior to takeoff and/or landing. The pressure switch and additional circuitry allow additional parameters to be monitored. The amber STEER BY WIRE FAIL message will be displayed on the Engine Instrument Crew Alerting System when one of the following conditions exist: (a) Nose wheel nutcracker switch snack in the ground mode; (b) Nose wheel steering shutoff valve(s) stuck in the open position; (c) Nose wheel steering system inoperative due to loss of power, (d) Improperly installed steer-by-wire ECU or ECU connectors. Using the instructions and parts provided with the GAC ASC 176 Kit, performed all of the instructions applicable for aircraft S/N 1085, except (see Figure 5, Page 13) installed a GAC P/N 1159SB20223-11 BRACKET in place of the GAC P/N 1159F41094-39 BRACKET furnished with the kit This minor deviation allows the Relay Bracket to be removed for maintenance without having to drill attaching rivets. SDNY GeS4_02/5410 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 Successfully performed ASC 176 installation checkout (Paragraph H. Pages 6 and 7) and noted no abnormal or unusual conditions. Returned the aircraft to flight status and recorded compliance with this FAA Form 337.in the aircraft's ' maintenance records. F It has been determined that the interrelationship between this change and any previously approved • • configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to: There are no changes to the operational limitations; The existing aircraft flight manual provides Migration for dealing with the STEER BY WIRE FAIL EICAS message; and the change is compatible with all previous configurations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the aircraft's electrical load analysis and weight and balance data is negligible. This Saco:vow generator form Bled ea ASCIT6DOC: SPS4 Chambers. prepared by Michael Donnelly NO ADDITIONAL SHEETS ARE ATTACHED. *END' O Additional Shxts Are Amen:6 EFTA_00241114 EFTA01326707 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3.S ® hi.i. poem.. 1 ./L2POR REPAIR AND ALTERATION (Ak'ri amp, Powmplant, Propeller, or Appliance) me... ,,PET c•c", " ,,a ,s Fa FAA Thie Only c 0 L- r 5 .9 - ' • swarms ,samosa INSTRUCTIONS: cam or type all entries. See FAR 43.9. FAR 41 Amanda S. and AC 441 (or tutdehoeitt revision thereof) for Instructions end disposition of this Form. This report b required by law (49 US C. 1421). 'Mims to report can result in a civd penalty not to exceed $1,000 for each such violation (Sefton 901 Federal Aviation Ad 0(1954 I. Mardi Make ' Golfstream Aerospace Mold G-IV Sala! No. . 1085 Nationality and FtsaMennice Mark Nitl3GA 2. Owner Name (As stows co registration certificate) B A Leasing & Capital Corp. Addnsta (M shown cm regionalism eatiforate) Two Enobarcielero Center San Francais Ca 94111 ....- isaatJaier SA042151wanly: :seta . 4...s Riverihman infrewarts id b amrovrO ea :le oe Ova dmerbrd =Fa ailmt to cooterrny irspetho a z 'Erma a Nefas e -91114--v v - ..).0 -43 _.:t - OAR 4. Usk Identification 5. Type Ufa . Milks I Model 1 Said No. Repair Altendico ?Whom (As daubed in Item I above) ********** ••••46499 X 1 Powerplent proi can. t AiVisTice t Two . . • simorasamw 6. Cesiminity Slonement • 21...pparta NO and Address B. IOW of Astaicv C. Catlin No. LANCE A. MATTESON . . 65600E. SAN FELIPE DRIVE SC01173DALE, AZ MO • ' . X U.S. Certifiated Metairie AP 1664049 .r Fortino Certificated Methane Certificated Repair Station , Mat= DAD:eery that the repaa Nadler iiieralice made I o On mit) idedirs1 in von 4 above mai casented on the mom er madam_- hems bavc been male ist atientarce with the tespinemet of Part 43 of tte U.S. Foleral Aviation Regoltioni ad the de informant° fiatiated bran is owed coma do the born dray 171O.thit- 7 Date tt-ft —cr.) Signature 0M/thorned ‘ec je:S......... • 7. Approval for Return to Service Pirate oars Fatal BY to lb: =hairy given panes sprified bdow, de mil identified in item 4 ern laspected is dm 'rarer preeenled by de Athninistrztor Avidice Admin.:rice as OD APPROVE) 0 REJECTED FAA Ft 3adertis Impar \ AID x Insmenos Authorization Odicr(SMOM FAA Daiiiime - 1 Repair Stance Pastei Appened by Trasport Canada Ainarthiness Gram Date of Approval or Rajemion . -il.ilry . adtholin DmipsamiRis 5267054,14 IA Emanate of Audio Nfichaei Dcrrneth. • . . . • • ..___ - - . SONY CM _ 62754193 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241115 EFTA01326708 FAA AIRCRAFT REGISTRY . CAMERA NO. 3 DATE: 3_3 -_94 NOTICE compatible Weight and with tehmce N previous or operating Antrim hesitation changes Ad be emend in the appropriate aircraft record M thermion mist be to assure continued conformity with the appraarek airworthiness requirements. Daalpriom of Week Accomplished 123/1 space l? required, meth *Mean stmts. Irks* swath sinzica snorer* ad reguntime mat Nal tie win aopleigri) August Certificate 11, Data 1993, Gulfstream Aerospace Corporation (CAC} Model G-IV, SIN 1085, HUG& FAA Type Sheet Al2F_A This change requires FAA Field Approval production The ptapose of this change is to update this aircraft's fuel booretptpitp vent hose system to the current standard. This modification-will eliminate the need for4W-erdiffenitit'pert number hoses in spare stock and provide for a neater sadiste logical initaffati6C; Modified the LEFT and RIGHT Main ea AfftglittflentEntister-fsnapVint and System by. Removing Removing discarding the existing four each vent hoses that connect each fuel booster pump to a wing tank; and discarding the number 6 AN Fitting and Os ring packing Stalled in each of the four Union booster pump vent ports; Installing a new MS295I 2-06 Ce ring packing on four each new AN8I5-61) of Finings and installing one fitting ('O' ring packing side toward the booster. pump vent port) into each 143 the Vent four Hose booster pump vent ports; and Installing a new Gulfstrum Aerospace Pan Number 115H40200- all newly between each new booster pump vent port and the closest existing wing tank port Secured installed ports and hose fittings by torquing to the current maintenance manual torque value and identified with torque stripe. All parts were new when Stalled and purchased from GAC Product Support Savannah, GA 31402. Performed FUEL CONTROL a leak chock visual inspection of all four fuel booster pumps and attaching hoses while doing 28-01) SYSTEM FUNCTION TEST in accordance with CMP maintenance code 280005 (card and noted no leakage or abnormal operation. Returned maintenance the aircraft to flight status and recorded compliance with this FAA Form 337 inthWilloriffs - records. It has been determined that the interrelationship between thischange and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination automatic; There includes, bin is not limited to: When performing it's intended functions the operation is are no changes to the operational limitations; No flight manual suPPlements arc end the th required; continuous osnation is compatible with current production standards and all previous alterations assuring conformity with the applicable airworthiness requirements. The effect of this change on the aircraft's weight and balance data is negligible. This areptaer mentor torte filed a VeiniOSEdot; 5, 99 CbgeWas. PrcPand by. Kahn Deo* NO ADDITIONAL SHEETS ARE ATTACHED. 'END' Q Addend Shea. Are Anached sbAiTeii:briD41§V SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 I 16 EFTA01326709 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3_ - 94 A il) MAJOR REPAIR AND ALTERATION v i dun= a -as.pat (Airframe, Powerplant, Propeller, or Applies's(*) / slal MISR mean. lai Mem' . 01014 727)40/ hellall•Coly Officeidadliesemos t5-BC -a? INSTRUCI1ONS: Instructions and penalty not to Print or type all ewes. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent revision thereof) for disposition of this form. nib repon is requited by law 149 USG 14214 Failure to repon can mutt in a civil xceed $1.000 for each such violation (Section 901 Federal Aviation An of 19501. . I. Arad Mahe - Gtillatream Aerospace . Model G-1V ' Serial No. 1085 Nationality and Registration Madc N8SGA 2. Owner .' • Name (As shown on mist:raw anificets) B A Leasing & Capital Corp. Address (As shown on rerasmitoo catifonte) Two Embarcadero Cram. San Francisco. Ca 94111 • 3. For FAA Uwe Cady • • 4. Unit Identification . 5. Type Unit Mein I Model i Setae No. Repair Merton Airframe .... (As des gibed in Item 1 above) ' - X Powell:plant • . . PropeRer a Appliance T* Manure:nun A. Ceitereelly Statement A. Agenryel Nana and Address R. Mod of Agway . C. Cara:eta No. • LANCE A. MATTESON 8560 F- SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 , X , U.S. Catificated Mt:claret AP 1864449 . Foreign Certificated Mechanic Catificatcd Repair Stance ' Manufacturer IN I am* dot dm weir nadior Manisa made to the mike) idereffied in item 4 Move aed deathbed on the reverse or aratenems hens here been made In axcedeom with ra :mei:amens of Pat 43 of the U.S. Federal Avalon Ragelations and that the information feeedded herein is tree nreleoraia to damat eiT my ImoMedea Pale „9 ,7 7 :irri • 7. Approval for Retro te Service Pumcmi to tbe milbeety given pions specified below. the and illersined in Mesa was inspected ha We maw prsaMed by the Adrnisescrace Maw Federal Anxion Admousalcion ands IK1 APPROVED 0 REJECTED BY PMdik Sewiatea Spence Mane/masa i I baPeciwn Arthwawann Other (Speedy) FAA Designee' Repair Mama I PetiOn Approved by Tampon I Canada Airwatbinin Group Date of Approval or Rejection 547 f 72. Certifiers ar• - Owieries No. 526705494 IA Signs of A ideal Michael DonneRy SDNY_CM:02754195 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241117 EFTA01326710 FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: 3_ 3- 94 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alb:radon must be compatibk with all previous alterations to assure continued conformity willa the applicable airworthiness requirentogs. • S. Daseripdon a Work Accomplished (Snore space is reqviroi mach additional sheen. Identify with aircraft natio:lay and reginnuon sit and else work completed) September 7, 1993, Gulfstream Aerospace Corporation (GAC) Model G-IV, SIN 1085, N88GA, FAA Type Certificate Data Sheet Al2EA, Revision 18. Aircraft total time in service 1493.6 hours and 608 landings. Refer to: FAA Approved GAC c-ry Aircraft Service Change {ASC} No. 3 Amendment 2 Subject ICE AND RAIN PROTECTION (ATA 30) WINDSHIELD HEAT - • TEMPERATURE SENSOR TEST SWITCH - INSTALLATION dated February 26, 1993. Effective for Aircraft serial numbers 1000.1155 having ASC 3. . The purpose of this alteration is to modify the wiring to the windskiiikheat to ) perature sensor test circuits installed by GAC ASC 3 so that both temperature nsors o each cockpit window can be tested. Using the instructions and parts provided with the GAC ASC 3 Amendment 2 Kit, performed all of the instructions applicable for aircraft SIN 1085. Successfully performed ASC 3 Amendment 2 operation test (Paragraph C. Page 3) and noted no abnormal or unusual conditions. Returned the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's maintenance records. It has been determined that the interrelationship between this change end any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to?There are no changes to the operational limitations; No changes to the aircraft flight man\qal are required; and the change is compatible with all previous configurations assuring continuous conformity with the applicable airworthiness requirements. • The effect of this change on the aircraft's electrical load analysis and weight and balance data is negligible.. This Sacco:pan generator them Ned as AScsAvn rm a n aen. prep .4 by badsDa,„,b,ur NO ADDITIONAL SHEETS ARE ATIISCHED. 'END* CI Addidonal Sheets Are Attached • . SDNY_GM_027Sti SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241118 EFTA01326711 Pa Asa.. .... an Ma. 7.17PMX , ® • MAJOR REPAIR AND ALTUtATION - Toe IAA the Only us this ' (Airframe, PowerpIat, Pittprlier, mr APPIalla) er.......,.. Polinl Aar ...-- as= •kmarathe .5-.? c • ,-<sz 2 INSTRUCTIONS: Print or type all entries. Se* FAR 43.9. fAil 43 Appendix B. ad AC 43.9-I (or subsequent mislon thereof) for Instruction; an on of this form. This report Is required by lea (49 US C 1421). Fealty* to report can result in a civil penalty not to exceed S 1,0001= tad such ylolathM (Section %I Federal Aviation Add 1958). I. Airalf) Mac ' Golfstream Aerospace Medd G-IV Stria No. loss Nationality 0 Registrstioo Mule N88GA 2. O Name (Al dries on regime:ion oaths) B A Leasing & Capital Corp. Address (As on on repontice catficee) Two Reabanadero Cm1Cr Saa Francisco, CS 94111 3. For FAA Ese Orly 4. Unit Ida-dilation 5. Type' licit Mat I Model I Said No. Repair Al= Airframe (As detertlxd in Item 1 above) X Powaplent Propeller Appliance Type Manidatarer 6. Casformity Statemart - A. µstye Nese al Addis B. Kat of Agoicy C Catificate No. LANCE A. MATITSON 1560 E. SAN FELIFE DRIVE SCOTTSDALE AZ 65256 X I U S. Cerakaed Mectamic AP 1644049 j Fen* Certificated Medmic TCatificated Remit Station I Maaufacturer D. lertly diathermia mint elms= nude/oft tee=(.) identified in des 4 above cd 6=nbed cede creme a etuchaeces ham his tem made in accerderice 0 the rotaramits of Pm 11 0(5 y.s. R&M Attie Reptant dim the iefernotis fimieled tent S int aid arta to de tea dory towledet Dam Y---N-F Sigmlur loift2a i 7. Approval for Retro to Service Passed to the asloity given pima tprified blow. the me ideaihed in eat I me capeeted in the name preceded by de Athatiso car of dm Fetal Anton Ackrionaba ma is Cgl APPROVED 0 REJECTED BY FAA Ft Sumba bass Mtalfaconer i baps= Axidatatesi Other (Brady) FAA Designee Repos Stabs Pence Append by Titspert Canada Mn dtea . Cisco Date of Approve/ or Ridection 814/ 2 193 Gots or Deilotre No 526705494 IA Signature of Authorized r ?ached Dannelly •.“ r=7;' . V .tr. • • zr . ”5 in hi: 't lt . na • SDNY_GM_02754197 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241119 EFTA01326712 NOTICE Weight and balsam or operating liaimtioa changes shall be emend in the awroprime aitcrillrecord. An sheralion meat be compatible with all previous alterations to assure continued conformity with the applicable Unworthiness requireameas /I Description of Work Accomplished Of mere spar is required. math odd:kcal deem. loss* each antral ruescoltry ad rcgaraa mak ad due work ccepleteM) August II, 1993, Gulfstream Aerospace Corporation (GAC) Model G-1V, SIN 1085, MAGA, FM Type Certificate Data Sheet A 12EA, Revision 18. Aircraft total time in service 1481.6 hours and 600 landings. • - Refer to: FAA DER Approved GAC Repair Drawing Number SE05201903 REV. A, STANDARD REPAIR - SPHERICAL BEARING, N.LG., FS 119., BL 0.0 Sheets 1 and 2 of 2, dated 5.5-92, Effective for this aircraft and signed by John G. Wilder, FAA Structures DER SO-483. The purpose of this repair is to prevent torsional movement of the Nose Landing Gear Brace Assembly (GAC P/N 1159L40801-5) and the Nose Landing GearDrag Brace Assembly (GAC P/N 1159LM40588- I I) that causes the loosening of the existing bearing (P/N GB146-10) in the Drag Brace Fitting at fuselage station 119.0. Removed the Nose landing Gear Assembly from the aircraft. Performed removal of existing bearing PIN GB14G-10. Inspected and reworked existing Drag Brace Fitting, PIN 159B10053 per GAC Drawing Number SE05201903-901, Standard Installation. Installed new K210-3 Bearing Assembly and torqued to 110 in. lbs. Installed Nose Landing Gear, Drag Brace and Dovmlock Assemblies per GAC Gulfstream IV Maintenance Manual, Chapter 32-2-0, page 204; pant 3. Successfully performed landing Gear Normal Function Test in accordance with GAC Gulfstream IV Maintenance Manual, Chapter 32-0, page 201, pan 2 and Nose Wheel Steering Function Check in • accordance with GAC Gulfstream IV Maintenance Manual. Chapter 32.500. page 201;para I. Returned the aircraft to flight status and recorded oaeopliaer.t with this FAA Form 337 in the aircraft's maintenance records. It has been determined that the interrelationship between this ;emir and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft This determination includes, but is not limited to: There arc no changes to the operational limitations; No flight manual supplements are required; and the repair is compatible with all preyious configurations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the aircraft's night and balance data is negligible. This nacos:pester manta form filed as N0SEGEARD0C: 5769 Ono= prepasd by 16:;tral DbeooJy NO ADD MONAL SHEETS ARE ATTACHED.. !END*. SDNV_GM_02754198 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241120 EFTA01326713 *ra ~Vink" Lts-nrts rkower•--..00m us *wan miNTOrwarninT~ . TRA Alanten RECISTRT CAMERA AD. DATE: 6- -(13 e ALTERATION Pon, Rporoml OMB fia 2120~ • MAJOR REPAIR AND ufatarnon Por PAA Ure Ody cd anmemarn (Alrframe, Powerplant, Propeller, or Appliarice) name een Menseno War (5 e tinCe - 4 41 se orstaucnOtis,Prim or tYPII Ill•eltihs. Sa FAFT43.9. PAR43~mM e. and AC Ci-I falitaguenlreamonowometer Manntions and doonallon d tha We:Mommen b ~Ome inlaw On USCAKM h Panda nalfannat Man in ltdd MOUW mtalwand KOM Mor mok mach vadatim (34rnhon Int Naleal ~Me Ad d len). 1. arend Mike GULFSTREAM AEROSPACE wam G-IV ~d Na 1085 Nimonarny anlirgr uee repya ' Z Crnmer Name fernsMwn On ~4~ 01/PEVaD BA LEASING 8 CAPITAL CORP. Aanleg Ms Oom On rontratko ~Ko" TVO EMBARCADERO CENTER SAN FRANCISCO, CA 94111 3. Per PAA Uwe Satd4. ,...........27„, ayiaaya aa 4.,,,,aa Sv' "ffs ITTIKORI3 M a aan eg n Mr •::.•• descrod Ihn Sa ~Irae race~ br • or•rt la NOrilán Ka. Y- -F25 InTE a. om Itle.ntilletbod S. Type UNI Mere owm &NO No. kawa Mbmmm ~RAKE e a Wo n 1 nor') mornemm....mo ram, X POWERPLANT PROPELLER MOUANCE Type Manuladuret ...., 4 C. COrdendel naland A. Agencyk Name and Jans e. Kind of Agency C Canna* No. LANCE A. MATTESON 8560 EAST SAN FELIPE DRIVE SCOTTSDALE. Al 85258 x u9 Caturcatee Naam AP 1864049 Nmon Catereed nweema ~zo Roomt Sims• wo.s.a, 0 . 10e~~ 140,04"TO/0~~1"de WIKT un ROmomwed in Omm 4 More and drocroDed en me oreme of anmNmem homo fan Man node we Itecorhhhhe milt th* thChlitentleaS of Pan C dl die V.S. F innam %quines,* and t the Informat•on , lum~il neem re na and Ca nal to Me ben Of my nowledge. -...."" OM. APRIL 20. 1993 Dr' loomOmi • L ---,—, ... 4 c c..... . x.mprows Re Rdne Te imisib. rammelt to tam imum e Ily Olm pemems speolied ~AAM unit Woed« In dam a Ht immarn,n me nameet PrnsfandBy K» Adaruniftwor of Ina Pedro Athibon ANnimstration and is »PPROVED Cl REJECTED FAA PrilMimes.% inspeaor Urnunclumr I MIrnarSma•al BV PA* ~gnoe . Now Stalen PemoNmenONTantadat Canada ammarnas Group Da* 0 kommen *a Repelen • WASA3 ~ma m DwrOMOOn Na 6 2 0 0 rttri7fr Signalur. of Autroved lno r - 191C.744 1 1)Pentredir SOI•iY dá4j27 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,0 ang41ór d 17 - EFTA_00241121 EFTA01326714 • • '`r.-77,7,74.1litanOW7Cr#4,,lit 1 Illes„ TAR AIRCItATT REGISTRY ... ...a. I CAMERA NO. S I DATE: VP --- 9--- -sit NOTICE Waters: and balance or operating Imitation [banessnail be enteral in the appropriate aircraft record. Anther:monmust be compatible with all previous altelations to assure continued conformity with the applicable airworthiness requirements. a. Oesenaten of weft acteepane III more spec, me required mach additional mesa. identity min aircraft nano/urn and registration mart and data work completed.) 0420193 Guff strewn Aerospace Corporation {CAC) Model G-IV. Stria/ Nunn es 1085. NDIGA, FAA Anaaft Type Cando:ate Data Shea AI2EA, Revidor IS. FAA Append Data: FAA Form 8I10-3 Statement of Compllaret with the Federal Aviation lb:gala:ions dated 2/3/92 for Gulfs= Model GV. 1159. d 1159A; listing GACRtpair Dwg 11595BM 189 REV. C title CORROSION REPAIRTBALLAST COME. SURF. ELEVATOR sniped by Struction DER John G. Wilt ex, Designation Number SO 683. FAA Acceptable Data: GAC Productioe Dwg 11590520002 REV. E, duets I and 2, inhading through Engineering Orda (EO) RI; dated 1113/92. these drawinp append forprod•wwiew by FM form 8110-3 dated 1118/92 for Gulfureatn Cr4V Anna by FranIt Salmon! SG-7034 Strunna DER GAC C-IV Meicaterme Masai (MM) -Interim Revision 16-1, dated 30 Mardi 1992; OACCeIVMINIYel, I. REVISION 16 dated 6 DECEMBEt 1991; GAC Pe:chain Dwg. 159CS20434, titled SIGN INS7L CODRROt..47YRE-FIEV-STA 1100 a 168.78 LE. MI& 2 rf 2, REV 0 dated 1240-91; and GAC Production Doug- 1159CS20443, titled BALEPTSVS7/. CONTROL SURFACE - ELEYAMR, Ail& 2 of 2 REV F dated 10/28/84. ThentrpeseefilepeieirtetreolaceeitiaMinedinboard nifing edge assembly on the left devisor.. This repair involves: A. The removal the left deviator from the istertee, B. The removal of • inboard trailing edge riveted assembly; C The installation of a new inboard outing edge riveted assembly; D. The removal of a Medan of tbt leading edge riveted skin to pin soon to the balm trim weight attach pond E. Assembly. painting balancing end attachment of the elevator control surface to the aircraft. In accordance with the GAC Conatterized Munn= Program ICBM code 2736.07 anvil the left deviator, GAC P/N 1159CS20022-59, S/N IOW dated I 1 /88. from the anent Flemmed the toned riming edge assembly, GAC EN I 159051120400, S114 1113. date/ Aug 23, 1988. from the left elevator by dribs( ow the attaching rivets Installed a new inboard trailing edge assembly. GAC PIN I59CSM20400-89/F-2/01, SRN 1400, dun holt 1993, onto the demo( by riveting in acht MAPCO with the applicable instructions contained on GAC drawing 11590520002. Rimmed leafing age skin a the balance at wight enact points by drilling ram n rivets to gain meets to the balance trim weight and: pone sad added I each GAC PIN I IS9CS20443.5I (0.5 pound) weighs and -53 doubler in accordance with data cormiood on GAC Dwg. I I 59CS20443. REV F. snouts:id 2, dated 10/11/68. BALLAST ITVEIGH7717,571. CONTROL IRFACE-ELEVAIDR. In accordance with the above referred to GAC Product:cmDee& detailing SKIN NM mstalkd original elevator leading edge to by Mang. Trated, sealed, primed sal painted tetrarch all bare meal. In accordance with the GAC NMI ATA 27-0 Flight Cootrol Systems decked balanced elevator; final balance data after paintin LH elevator 0.0 in.Abt NOSE HEAVY. In accotsbnee with GAC CMP codes 273007 installed be maned left elevator. GAC PIN 1I 59C520002-59, SRN 1086, dated I1/88, to the proper position on the aircraft The mad was not tat flown because it vets disenimd that the tate dal was dote would not change the flight cliamatristies or 0mo/tonally aft xt the Bight operation of the ant This determination inchaded, bin was not lintel to, anderation that the repaired elevator tamale balance, shape. mega and original type =fame design was cot changed. Recorded compliant with this FAA form 337 in de sinnit's maintenaam records and =mod the aircraft to flight tame. Aarall Total Tent: 1362.6 heat Aarah Cycles 547 landings. Changes to the artralTs weight and balance was negSgible Ttm morear ecorraird 6:0 prepond by Mathool Pau idly teen a Pc M at/50. Midas CLUAY112073ELD3C,1555 . Calm • ADVTIONAL SHEETS ARE AITACHErt na.ar Addazontit ShWrIt Ai. AitaErtycl r . • • kiwistit.- • f. agt., :1 & Fit . 41,4/ a • 1 • • •'-•!2..17 5 1 ' • : SDNY GM 02754200 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241122 EFTA01326715 FAA AIRCRAFT REGISTRY , CAMERA IRO. DATE: 40 a t r" ' Sgi Nisi 0.1*.119402. ® MAJOR REPAIR AND ALTERATION Far/AA US. Oa, uac....cus (Airframe, Powtrplant, Propther, or Appliance) erspoils Aillall OtEse Idemdcown Z) 1 ttr i/. 2) INSTRUCTIONS: Print or type all entries. See FAA 419, FAR 43 Appendix R. and instructions wvi disposition of this forrn. This moon is required by law (49 US.0 Peray to to acted 11.000 for each such viotulon (SecOon 901 Rola AC 43.9-1 (or subsequent reviCon ifsenc4) for 1411). Failure to ninon can result m • civil Act of 195/1 I. Aircrati Make ' Galfstream Aerospace Model G-IV • Serial No. • TOES Noionably ad Registration Mark MICA - 2. Owner Name (As shown co toptinunn ciro.5mtc) B A Leasing & Capital Corp. Address (As doom cm *strata outdate) Two Embaraidao Caner San Francisco. Ca 94111 3. For FAA Use Only 4. Unit Identification S. Type US Make I Model I Saul No. Reps Altermam Airframe (As desaThed in Item I above) • I PowapLarit - Propekr Appbsecc ' Type Madam= C Conformity Statemaa A Agemis Name al Address B Kird or Agiscv C. Cates. No. LANCE A. MATTESON /560 E SAN FELIPE DRIVE SCOTTSDALE, AZ MSS X USCertiScated Meths* Foreign Calibrated Mothasic . AP 1861049 Certificated Repair Stab= Mazufactura a I catty that the mut andke abernice made to do =Ms) idadifiod in mei 4 dote mddesailed ce the Mint Ot °tea berm bin beCti mat to oxcart= with de nstprenamts or Part 43 ciT dic US Federal Mimi= Repack:4w al dads infamatica fonistoTtenia is me and correct beta tot at my Roma /age Date Ci : 2 / '' ?..., Signatia t 7. Approval for Retry to Service Pinson dm mitbrily pm persons spec:del Sow. the ma ideetifee in dm 4 arto imps old in the r natal by the Adminanore °fan Federal An Adman:sire and is CM APPROVED 0 REJECTED BY FAA D. Stmlurdi bcost. • Manufictister R ingo= Askant= Otter (SpolgY) FAA Drama Rcpt Stake Pc Amoral by Traimert Comae AirocatioasCiosp Due clApprovg or Reamial Ili ZIP , cot rs Onipasims Nu 324705494 LA &pat of Malrituni — - - -- — — Nfrined Dome& - - 13 r pilan7f44474C:re . . . SONY GM 02754201 L SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241123 EFTA01326716 • r' ""2"...S0a57- - .9 . Yei; ' -Ds I FAA AIRCRAFT REGISTRY . a _ en 1. . CANERA NO. aDATE: 10 — 1 1 3 NOTICE Weight td balance or operates talon change shall be eared in the appropriate termed record An aluraboo 0142 be consparibk with all previous alterations to assure cominued =fort* with the appfrable airworthiness reqtaemems I t Description of Wort Accomplished (If more space a naming nue eat ood them Wady with tome • , and avant= mirk addie Wert omPlotet April 20, 1993, Oulfstream Aerospace Corporation {CAC) Model O-IV, S/7.4 1085, NSSGA FAA Type Certificate Data Shea A 1 2E/1. Revision 18. • • FAA Approved Data: FAA Airworthiness Directive AD 93-04.02 Rockwell Icrtertatioaal/Collins /niece Division TDR.94D • Mode S Traisparlere FAA DER approved form 8110-3, dot Aped 16. 1993, Ideatificsnoe of Drawing Numbei(s) 08069197 ad 0806919111. edited 09/01,94 ResisiotA, Wag Diagram' No. I and No. 2 Teepee (MOD). John R. Chamdess NM-476 Systems 4: Equipments DER. and Western Coentionder Incorporated FAA STC No. SASO44NM, as approved February 6, 1991. The purpose ofilitictenge is to =Key this aircralls wiring to correct wiring discrepancies team the TCAS and the Mode S transverses syuans Woing disrepute were discovered she both TDR-94D Mode S transponders were modified to Cola; PeN 62:4210-003 a required by the above fisted AD. Prior to complying with the AD this Mend was equipped with Collis PfN 622-9210-002 assn transponders insetted in accordance with the above listed SIC and utilized discrete wiring to the TCAS word hod from each tampon/a, The -003 modifiemire sans transit eders utifim A1UNC 42r data and require removing the discrete wiring for 'STET', - ra-r, 'ALT PORT 7 OUT. and 'REMOTE [DENTIN'. ModSed this aircraft's wiring to conform to the above listed drawings %floor deaden to the approved data with regard to the 'REvIOTE inarr ad 'TEST' was done,, follows: (a) Wire 1SX22822 was removed from al transponder Rff P2-55 ad inserted into #1 transponder Rif PI-16, (h) Wire 2S3C21B22 was removed from e2 transponder WY P2-55 and boated into er2 transpooder RR P1-16; (c) Wire 1SX21A22 sod Wee IS702A22 was spliced iogetter ear TCAS control pad P1; (d) Wire 2SX21A22 and Were 2SX7seso were spliced together new TCAS control pad P2; (e) Wee ISX23A22 had be pmiously removed horn muisponda count pad Palo E and rapped and stowed. and (4 Wire 2SX23A22 had hem previously removed from 52 transponder cord panel Pia E and capped and stowed. Dusan Avant (FAA CRS 'DVS I54F) performed m enegrati sysems tin pa FAR 91.411 and both transpooda systems were toed to amply with Part 43 Appendix E (c) Work Order No 22.37R, Mud 4/I 5/93. Ramp to reeled that the memo co-ax come ton were reversed between the I I and 12 system a the TDR-941)r1163; comae co-ax conreatons to conform with the above feed drawings. Now Trans--der ramp teeing was doe ming LER L-band antenna •HAr steads go ' prim false alerts is arbons TCAS equipped Maid - • Returned the dread to Eight seats ad recorded corgiarace with this FAA Form 337 in the aircraft maircessax records. Ainneft Total Time: 1382.6 been; Aircraft Cycler 547 lags It has bee &rased the the intardetioeship between this change and toy previously approved coaster/M.9n will not introduce( any adverse effect upon the airworthiness of the aircraft This determination incluiten Ss is not limited to: The minor deeigices (a) through (d) above accompashed the intent of the approved data; No changes to the eitoraffs electrical led analysis data were nude; Them are no changes to the operational limitations; No digit manual supplements are reqsjed; and the installsion is compatible with SI previous alunetions assuring CO0SLIOU.S conformity with the applicable IliTY•OnSICSS requirareets. The dim of this change on the wash's weight and balance dais isles:jolt / This mom= gacrord form wet der uses MABC4W33; WORD 2 O0, AD9a 7216 Chas pep. by Mat Dcally. NO ADDMONAL SHEETS ARE ATTACHED. 'END' 0 Additions/ Sleets Are Melded k s RFJ 1 v.,4 • vr.21•• r:. • .7 a fili= cwito:liXits - SONY OM_02754202 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241124 EFTA01326717 !II ro AIRCRAFT REGISTRY l,"CAMERA ND. wi DARE: 4 _2_93 ••••••• 00. ' zkan itsuasreketInbaSads .' sir44 ',write-- .1 ® MAJOR FtEPAIR AND ALTERATION . nano 0 ;mans.. (Airframe, Powerplant, Propeller, or Appliance) r........sq xammweq ',IS AliSli — Owe. nNaatt Facia Us Owl. WarIdanoticaaat ' 55 t --f f:Sb ) INSTRUCTIONS Print or type all entries. See FAR 43.9. FAR 43 Appendix L and AC 43.94 (or subsequent revision thereof) for instriblons and disposition of this form This report is required by law (49 USG 1421). Failure to report can result in • (MI penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of IOU:. I'. Aircm8 ..... ?stake Guifstream Aerospace . „Cl atIV — Serial No. 1085 " and Registration Mak . NSSCA 2. Owt -Name (As shown co regutrabort catifiudc) B A leasing & Capital Corp. Address (As do= cm regisizaion eertitale) 'Two Embareadere Caner San Francisco, Ca 94111 S For FAA Use Only . 'I A . • es. ' 4. Unit kleatifkation 5. Type Ucit • Make I Model I Said No. Repair Mama Airframe (As descrised in It , I abort) • . • 1 Powerplant 7 * ....-.5 Propeila AppEaree • Tqst, ").. -. e Misaufrower 6. Conformity Statement A Aoscx's Name and Address It Kind of Aricccv C. Catificaa No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 15258 X U.S. Cat on:al Mechanic Foreign Certifie43 Meekank AP 1864049 Certificated Repair Station Manufactiser a I certify than the repair altar gum= rare to the ma(s) idenriScd is run 4 abase and detailed m the rause or anactwocnn her= have hem corde in aceordacce with triecq=stocou ofEnt 43 of the US. Fecloul Asia= Rept.= =I thalete iskniusie fionisbal borcos is true and mica to = tat of we knoakdat Date -20-n Sifotaure rd leant . 4':c 7. Approval for Mora to Service . Parma (IS BY lode mita* Men persons specified bra, the adidentified init= 4 ass moose! in the ma= prurenied by the Aaninisvaire Third Avila= Atimaisimica India 11) APPROVED 0 REJECTED FAA Ft Sada Spier Nuessfactung x lasaectim Aurtateginn Otter (Sreafy) FAA Designs Repair StaSm Passe Approval by Treason Canada Mealtime Comp Date of Approval or Rekcoon 2— 7.4o-99 canoes a 1341000=Na. '526705494 IA Sipatum Of ' • 0.0"" ' Wald Donnelly SDNY GM 02754203 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241125 EFTA01326718 1 • ••••rreir--1 - rl I CAMERA RCRA NO, FTw REGISTR DATE:11. ..2,_9(3 I III FAA AI Y • NOTICE Weight sad balance or operating limitation changes shall be enured in the appropriate aircraft record An ahenuion nuns be obestible with all pinions altentioth to assure continued conformity with the applicabk airworthiness I equiremcau L Ikstription of Work Accomplished Or eve spare ithereired, mach midi:ken dens. SOF/ •th =nett nationality aid agrarian mark and dare mark February 20. 1993. Gast= AtiroIAngx Corporation (GAC) Model G-IV, SIN 1085. N880A. FAA Type Certificate Data Shea A I2EA, Refer to: GAC FAA Approved Aircraft Service Change (ASO Nattier 231. SUBJECT: ELECTRICAL POWER (ATA 24) "E" BUS ALTERNATE POWER - MODIFICATION: dated JULY 31, 1992 and GAC FAA DER Approved Wiring Diagram LEO 46603241 rev none. ASC 231 Deviation. date 02-05-93. The purpose of this change is to replace four wins that wan removed during the installation of ASC 231. This alteration stores the FWD end AFT Emergenry Battery 'CHARGE INHIBIT circuits to the original production °prefiguration Nftinneci.tlth s fl ail" err PNL 13125.4.1] z f :Hot.= Sump /SSW a new Isfil-W-21759116-20 wire 21M111031420. stripped the Sedation from a free sad, airy installed • Dew Deutsch C7S-20/20 socket contact onto the wire, Sated the wile assembly into GIS - B. Rooted the free aid along coning wire rims toward THE, at [hetes to leogth stripped the insulation from the free end, crimp Stalled a new Desch CTS￾20/20 socket coma onto the wire, inserted the wire assembly into TI1E - IC Modified ,he R CKPT JCT ENE (306A IJ as follows: Stamp klatSed a DOM Md-W-22759116-20 wire IPU1103620, stripped the insulation from • free end, crimp installed a new Deutsch CTS-20120 socket cornett onto the wire. Sated the wire =co* into 712M - C. Routed the free end along aiming wire tuns toward TJ4A. oat the wire to length. snipped the insulin= from the free and. crimp installed a new Deutsch CTS￾2020 socket contact onto the wire, inserted the wire assembly into INA - F. Secured all areas disturbed during thermion. Modified the FWD EMERGENCY BATTERY WIRING [68A1) as follows: Removed wire IPLI9010A2ON coasted between MIA IP IA- land Sae grated Removed the end cap from eating wire I PU I I12B20, stripped the insulation from the free end, crimp installed new GA0135MMOS socket contact onto the were, inserted the wire assembly into 68A1P1 A to Secured all areas dirket:sod during thermion. Modified the AFT EMERGENCY BATTERY WIRING [68A21 as follows: Removed wire 2PU9010A2ON connected between 6$A2PIA - 1 and simraft ground. Removed the end cap from existing wire 22U1112.A.20, snipped the insulation from the free end crimp installed • new GACIISAMOS socket comas onto the wire. inserted the wire assembly into 63A721A - I. Soared all ants disturbed during thenuloo. Fathoms masts athekout m aceoräan©e Mtn ASC 23 i ail pats of paieraph 7 L4 sot no floors: cps rice Remind the fact to flight status and recorded compliance with cis FAA Form 337 in the aircraft's nuirdeconce records. It has beat determined that the interrelationship between this change and any previously approved configuration will not introduce any ads:Serf= upon the airworthiness of the aircraft This determination includes. but is not limited to: The change to the aircraft's electrical load analysis data is negligible; When performing its intended functions the operation is automatic: There are no changes to the operational limitations; No flight manual supplants are squired; and the installation is compatible with all prmious alterations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the aintralts weight and balance dm is negligible. This coasthr seems farm was dole on ACAF3S6/20. Sag WORD 10. fried a CIASC23102ds PSIS by Schad DereellY. NO ADDITIONAL SHEETS ARE ATTACHED. *END* O Addidoral Sheets AM MI MS • .4. SbNY GM_02754204 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -15, and 17 EFTA_00241126 EFTA01326719 FAA AIRCRAFT REGISTRY CAMERA NO. 2 DATE: 3--)S--93 ® MAJOR REPAIR AND ALTERATION W. Il •mu••• m . . en (Airframe, Powerpiast, Propeffer, or Applinet) %dad NISI= Ada/MIS ow • taws Pre WAS l • iOS OAS Llanbabos 5 -0i 'A); • iNSTRUCTIONS: Print or ran all eels. See FAA 43.9. MA 43 Appestat I. and AC 45.9.1 (or mbar:wont revision thereon foe irennactions sad disposition of this form. This report b rewind by law (49 UAC. 14211. Failure to report can meta • • CAN penalty not to emceed $1 SO0 for each such violation (Section 901 Federal Aviation Aa a 1931). I. Airmaft Nuke Gallant:am Aerospace Maki C.-W Serial No. 11025 144417aliaY red Regatta Mark NEC A, 2. One Nom (As town as registraext oroficeie) B A Leasing & Capital Corp. Addis (As town al roparsoco tati5cate) Two Embarcadena Center So Fr wart Ca 114111 3. For FAA Use Ovey t Unit Ittentifkatiaa 5. TM* Urtit Stake I Model I Serial No. Up= Abash Airframe (As clesaised io Mani Love) I PowpLant Propeller Appesoce Type Mau= ii. Conformity Swasett A. Amica-s's Name red Adam R Kid 0 f Araw C Cate No. LANCE A. MATTESON S.560 E. SAN FUME DRIVE SCOTTSDALE, AZ LAM X • U.S. Certifgemd Mechanic Foreign Certificated Mechanic Ar *M441$ Certificated Rimer Swam Manufacturer D I orgy Mat dm repot as/or Menke sew lode eras) identeed al Con 4 Mom red damned ca the mane a sand -a rent, here beat made in axerdsoce with the requiem= of Pen 43 of de US. Federal At Reipaa ad gm de iefensaias (aided brain is ins rod area to de boa dray krairedge Data / / cf. , 7. Amami far Ran a Service Paws= to de seferity given mom cecina! Wow, do ma idessthod i it 4 ins imported it the cat presaged by tlz Aftwastreter dale Federal Miriam Adecitannaien ad is an APPROVED 0 REJECTED BY FAA Ft asedmils knot bianufahatr 1 bap:aim Auelmizarice Oder (Spa:dr) FAA Dewiese Rep* Sums Pence Appored by Dation Coda Aiwartlimme Grasp Da of Apron] a/R*2i= .T24 2, 1993 cabals Cr Sigma= of Deeproce Ho. 52470504 IA -r;a: :- Wichsed Dormeily • • SDNY GM 02754205 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241127 EFTA01326720 _ 'H9211Wayea rra • FAA AIRCRAFT REGISTRY CAMERA NO. a DATE: 3-is---13 NOTICE Weigle and tern or oparing Futon charges ran be awed in the approprire agate record_ An ettererioe must be compsuble rib el previous altendious to esure comieued cocforSy with the eppEcede einvortlioness requirentetts Derriptioa of Work Arremplithed (If ern epee is reenrett redo ackfitictr emu reedy web wart istraddy es: repstnoon ark and date viva competedO January 31, 1993, Gulfstream Aerospace Corporation (GAC) Model G-IV, SIN 1085, N88GA, FAA Type Certificate Data Sheet Al2EA. Rem to: GAC FAA Approved Aircraft Service Cange (ASC) Number 207, SUBJECT' Auxiliary Power Unit (APU) Electronic. Control Unit (ECU) FAULT SIGNAL - IMPROPEMENT: dated: JUNE I, 1992. Related FAA Approved document GAC ASC 8A AnTillny Power (ATA 49) APU FIRE TEST - IMPROVEMENT; dated: Match 30, 1989. The purpose of this change is to prevent the Data Acquisition Unit (DAU) "nuscornpare message from being displayed on the Engine Instrument Crew Alerting System (EICAS) when the APU overspend shutdown is selected With the preient design it is possible to receive a false DAU MLSCOMPARE EICAS message because of an out of tolerance signal generated by the APU ECU. Performed all of ASC 207s MODIFICATION INSTRUCTIONS fisted as effective for all Gulfstrearn IV aircraft Note: The effoctivitiy of the service change should be Aircraft 1031, 1006 through 1155; not all Cruffsmaun IV aircraft Aircraft Service Change 231 von purchased in kit form from GAC Product Support Savannah, Ga. 31402. Performed installation checkout in accordance with ASC procedures paragraph C all parts and noted no abnormal operation. Returned the aircraft to flight slams and recorded compliance with this FAA Form 337 in the aircraft's iosmance records. It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to: The change to the aircrafts electrical load analysis data (0.02 amps added to the APU control C8236 during fault condition test] does not cause any exceieclann. in the normal or emergency power sources: When performing ifs intended functions the operation is automatic; There are no changes to the operational limitations; No flight manual supplements are required; and the installation is compatible with all previous alterations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the arcraft's i weight and balance data is negligible. msompileriptergcr ram en ha ce GIPITAreiSCk are WORD 2.O. riled r C1ASC2O76:c; ewer by trchad Etraity NO ADDITIONAL SHEETS ARE ATTACHED. 'END* 0 Ada:loot Slims An Merkel SDNY_GM_02754206 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241128 EFTA01326721 LCARERS AX AIRCRAPI N0. V. EEC DATES I STET 2-4 ' - 9 3 kin A•1." ... Oka Wo• 21.1.00) 'ID MAJOR REPAIR AND ALTERATION Far FAA Meat, es . .oasse Deree e (Airframe., Powaplase, Propeller. or A Pr011occ) ..........- ...s.ererem other kluged:Soo 5- 6 t - t P •,) INSTRUCTIONS: Print or type all emnes. Ste FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 14213 Faint to report can result in a chli pen.dry not to exceed 11.000 tor each such violsoon (Season 901 Fetal *ratan An at 1954). I. Airaafl Make Cultures= Aerospace Modd G-W Said No. IOES NatioeigAy and Registration Mark • NESGA 2. OVAMIr Neat (As demi co regimen= coafica) B A Leasing & Capital Corp. Adams (As shown oo *Salim oath:ale) Two Eabanadero Crater . Sul Promisee, Ca 91111 3. For FAA Use Slaty 4. Unit Idetaitlestioe S. TIT* US Make Modd I Saial No. Regan Mama Airframe (As cicsaased in Item I above) I Po...erotica Propeller ARIA/act Tyr Mat= & Cowforaft Slarapent A. Agr's Nome al Aetna R XIS of Apace C. Cate No. LANCE A. MATTESON ' X U.S. Certificated MCCIISC SSW E. SAN FILM DRIVE Foreign Catificatol Mer.lanie AP 1861019 SCOTTSDALE, AZ *32U Care-aced Rare San= Manuficarer D. I certify that the repair aralke ant= nude Loth' mi(e) idereified in roma above awl lambed on de mane anadaeas hove have km made in aeciadaesx web de requiem= of Fart 43 ofthe U.S. Federal Mistiest Rtadatims arid that tlx reformaan furnished tam is Ins sad Dana so the ben dray knowledge. Dare Slgnaoae cda.,-, zi /?PS Imo / W 6 , 7. Aaron' for Rerun Lo Service Penman tole aahaity Seen passe geedial baser; the air electrified in item 4 wa ®patted in de roar rooted by dm Admixing. ants Fakral Avimiao Admitisindat had is NO APPROVED I:1 REJECTED BY FAA FY Staler* Space Manufacturer x hapreso Aothorizoim Odor (WA) - . FAA ThaPa• Rica Station Pan Append byTriesart Cade Airworthionts Dace of Approval of Rea:ciao .7 #. - 74.12 .., i f pi Casa DraipsteoNo. 51670504 IA of Michael Deemer& AA Fern • b• • 002754207 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00241129 EFTA01326722 FAA AIRCRAFT REGISTRY CAMERA NO. 2 DATE: 2- ct- 9 3 NOTICE Weight and ban= or oteming klub= chews shall be entered S the appeoprisse zinzatl reset An onion sun be cotsnable with el scrims then/Soto to assure cowed confonnity wilt the appbcabk sirwordioso squirms= & Deaiption of Work Accomplidied (Vox= sax u nosed such aldisicest daft. Identify web sacra cusenals oil mg/stream mark and to wok conspbend) January 2, 1993. Gedfirream Aerospste Corporation {CAC) Model CblV, SIN 1085. N8SGA, FAA Type Certificate Data Shmt Al2EA. Refer to: GAC FAA Approved Aircraft Service Change (ASC) Number 231, SUBJECT: ELECTRICAL POWER (ATA 24) "E"BlIS ALTERNATE POWER - MODIFICATION: dated JULY 31, 1992. The purpose of this change is to provide an shanate source of power to prevent the loss of critical systems in the crag an E-Bantry (E-Batt) fails during normal operation. The present design has many systems powered only by an E-Batt Should an E-Batt fail dining normal operation all of the systems powered by that batty would be lost. This service clusage provides Essential (MS) dc btu power that will save taracanically as an alternate power source to the F.-Bases should an &Bait fail dwiiss uorinal operation Parfait:Mid all of ASC 231's MODIFICATION INSTRUCTIONS listed es effective for skald 1001, 1060-1211. except for the following deviations: (see Figure 4) Wire Number 1PU9005A14 and 22U9005A14 were not installed; ensued two new 10 gauge wires were sump ideotified 1PU9005A10 and 2PU9001A10 god commted as follows: wise IPU9005A10 was connected between the Line side of CB2311 tad the line side of ASC231CBI; wire 2PU900$A10 wan conneved ass shown (Figure 4) u place of 2PU9005Al4. Raychem solder spikes were used to mate all three way connections. All instalkd wires that required crimp installation were fitted to the proper size contact or teronival. Now: The listed deviations were required to maintain ccaformity with previously approved configurations and did not alter the intended function of the approved ASC 231. Note. Figure It'Sezedified Schnook Diagram* is no coma Om Figure 3 foe CB idesoenion): ASCDICBI should . be labeled F. E-BAT ALT PWR and cosseted to PILOTS el ESS 2IVDC BUS; and ASC23ICB2 stotdd be Wiled A E-BAT ALT Psofk am connected to PILOTS *2 ESS 23VDC BUS. ASC 231 Kit wee purchased from GAC Product Support Savant. Ga. 31402. Performed install/airs checkout in accordance with ASC procedures paragraph P d pots and noted no abnormal operation. Returned the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's msniteranot records. It has bits daermined that the interrelationship between this change sod no prniubsty approved configuration will not introduce any adverse effect icon the airworthiness of the ant This determination includes. bust is not limited to: The change to the ainnes electrical load analysis data is negligible; When perfonning its intended functions the operation is reno.matic; There arc no cbangei to the operational limitations. No 'light manual supplants/ me required: and the installation is compatible witha all pinions alterations assuring continuous conformity with the applicable airworthiness requirements, V The effect of this change on the aircraft's weight and balance jail is negligible. This ones= oasts fun so dace on GIM40.6/30, wog WORD 2.O, filed as CAA= I eke; reepered by. Mida Cosectly. NO ADDITIONAL SHEETS ARE ATTACHED. *END* O Additional Sans Are Anacted GSA 7 542 0 8 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SONY 15,02and 17 EFTA_0024/130 EFTA01326723 A& An RA ca , Wan Roe a DAUB. 1;-30-a1 -..._, m..... Oa.. DICSIZI ® --. MAJOR REPAIR AND ALTERATION Far AAA the OS vs wa nt nanny (Airframe, Powerplant, Propeller, or Appliance) news Anew se. INSTRUCTIONS. instructions and Penalty not to Print or type all entries. See FM 43.9. FAR 43 Appendix R. and AC 43.9.1 Tors disposition of this fonn. This report is required by a(49 U.S.0 14211. Failure to 'Need S1,000 for each such violation (Section 90I Feelers Aviation Act of 19591. misloinfaZ report can result Ina chid I. Aircraft Maim Gui Rare= Aerospace Model C-IV Said No. 10125 Nationality and Resignation Mari MICA 2. Owner Name (As sans on regisizan centlate) . B A Leasing & Capital Corp. Malls (Aa Mown on *maim note) Two Embareadero Carter San Francisco, Ca 94111 3. For FAA US. Only 4. Uset Identification 5. Type Unit Make I — Model I Serial No. Repair Attention Airframe (As desented in Item I above) X PM/anise • Propeller Appliance TYE,' Manbconee 6. Conformity Straeswi A. Amoco Nes and Addams B. Rind of Agency C. Catifraw No. LANCE A. MATTESON UM E. SAN FELIPE DRIVE - SCOTTSDALE. AtIka193 X U.S. Certificated Modsnie &gaga Ortafreated Mataric ' AP 11144049 Cedeeted Repta Safi= Martufmnaer a testify eta the mar anda Anion ma to ate maks idonalle4 mlam 4 stove and dieenbed on the reverse or _____ haw have beat made it oxotemee with the tershemeati.of Pan 43 of the U.S. Real Mision Replanom me Um the infonnision katted bade is no and COMOL to the barium knowledge. Date ifiai A-s, /tn._ s@wne r 4bdiv : 72,--Ca 11. 7. Appromd for Return to Sava - Perna to the setaity Riven ram spaified below. the ea Sada in ha 4 a impered in the rant poseraxd by the ' Adminiontor of the Fedad minion Adanaimaion ;nib l APPROVED 0 REJECTED BY FAA Flt swab - .....^• Manufactures i lospecho a Artaboringion . Caber (Specify) FAA Drips Reply &Mon Pawn Approved by Tneeport 7. Cameo Almaden= Mom Gate of Approval or Rejection /1- 2-r-9 2- Or Signature of rierismaicao. 526705494 IA ter t Michael Dortray • ---sb4rd-o.4 b27S4269 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241131 EFTA01326724 I FAA AlIC AFX incistn wan E. ?k Inn 12-3( - 92 • NOTICE Weight and balance or • compstbk mit an previous operating limitatiov,:hangcs shall in the appropriate tart record. An alteration must be alunaiors to assure continued fo ity with the applicable airwortbinas reqirements. Desalp Um or Work Aaoaiphsbed armors geese u squired mach skimped des Identify ISM Some itineareity and remorse= mat nd du wag completed) Type November Catificate 23, 1992, Data Gulfstream Aerospace Corporation (GAC) Model Sas( 1085, N88GA, FAA Sheet Al2EA. 92-001, Refer to: AEROSPACE UGHTING CORPORATION {ALC) FAA Approved Information Bulletin No. tided UPGRADING SERIES "66"FZ.UORESSITLIGH77NG SERIES SYS7ENS WITHAL -"I.2" LAMPS original release dated October 15,-1992. existing The impose ALC of this change is to upgrade this aircraft's Cabin Fluorescent lighting System by =toting the Lamps and Connectors. Series "66" fluorescent Lamps and Connectors and installing the ALC Series "12" Fluorescent eliminates The installation upgrade to the AL -12" Series Fluorescent Lamps on this aircraft the requirement of having to comply with Airworthiness Directive 90-14-06. 31.85.1A Rammed the existing 14 each ALC P/N 6635.1220-25 cabin fluorescent lamps and 28 each ALC PIN 1235 lamp end connectors and installed (in the existing motmittg clips) 14 each new ALC P/N AL- -1220 lamps and 28 each new ALC P/N AL-5113 lamp end connectors in accordance with the applicable INSTRUCTIONS in the above referred to ALC Information Bullet 'Al 101-8 installed Cohn parts Drive are FAA/PMA approved and were purchased new from Aerospace Lighting Corporation; . -, Holbrook, N.Y. 11741; telephone 516-563-6400 and 516.563.8781 fax Berfonaxl to ALC System INS*CITON and CHECKOUT in accordance with paragraph 5.0 of the above referred Information Buie& and noted no abnormal operation of any of the cabin Fluorescent Lamps. mairlieTnce ReturneA the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's records. confvhcation It has been determined wgl that the intareli5orship between this change and any previously approved not hlreCitlett any adverse effect upon the airworthiness of the aircraft. This determination reviewed includes, but is not limited to, consideration that the FAA New York.Aircrall Certification Office has Lamps the information and procedures contained in the D3 92-001 and considers the AL "1r Series Unit and AL-5113 Lamp Connectors to be acceptable; and Mavis= FAA approved Power Protected installed at each Fluorescent Lamp circuit that will automatically &connect power should a malfunction The effect of this change on the aircraft's electrical load analysis data is negligible. The effect of this change on the aircraft's weight and balancedata is negligible. Thu comma= wart= form war dour NO on ADDMONAL a mgr. Amos wen WORD Z0; Med a CSAI.CLTS doc Paharl DctromnY. ARE ATTACHED. *END' CI Additional Sheets Are Altschul SDNY GA4_02754210 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 132 EFTA01326725 • - ....i. • _: I . j .:i FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 19-9ą" •. *MAJORREPAIRAND .0- prunes oo pana ; @ ALTERATION • "'- • .ftirathe anty moire • Pilenia Ihrietpl!st, rrpralt • cF.SPYinet) Indian . . msw.. Office lireeneden a9C ad INSTRIKISOM Print or type all entries. See FAX 43.9. FM 43 Appendix B. and AC e 3.9-I (or sunnom revision therm/ for Instnxtions and disposition of this form- Thh report is required by law (49 US C 14 2 11. Failure to report an result In a cMI Penalty not to need $1.000 for nkwd‚ violation (Senn 901 Federal Aviation An of 19$s), 1. Aircraft ,...Caltstream Aerospace Modd C-IV ł • Soria. $0. . ' ille5 Nationality and RegistraSon Mark • NSSGA Z Cimsa Neste (Al dwom onegistratim cerdfiarM - - . . B A Leila* & Capital Corp. Address (Aa dawn co registration catiflade) Two Embartadero Certa San Prawico, Ca 94111 3. For FAA UK Only • . t Urn Ideaderatbae ' S Typ Udt Make I Modd I Serial No. Rew Agamiom Airtime . (As dercnbed in Rem I aboM) X .. - • . . , • .. Proper Aperture TOP • Maftraincr A. Mats Name aratt Min . B IDS afAmdcy C. Catificus No LANCE A. MATTESON X U.S. Catificated Mechanic /1560 L SAN FELIPE DRIVE . Foreign Catifacated Mechanic AP 1864049 . scorrsoms_ AZ asz.ks C.atiEcered Repair Stanco Manufacturer D. lamny dat the repair ardor skean malm to St) idepalkd S On 4 Mm and downbed en dw reverse a menuems lwem have bam ads hi accordance "nth nie reni= °Pm 43 ate U.B. R&M MMus &inn and tai the informed= Aniist.wd herein is true and own to the bon of my knowledge. . .--, Date . ł/7. . . 22 / y e Z- *Signature of • Cr M.ial • • - - .) t Amoral for Haan to Service kurant to ttr arbom pre pans imaged berm. te out Mmdxl ir, ime 4 oma irpaciatt ia te ram= preacrixd by the Admirientor oft. Fakes/ Aviatai Antenatko aM d O APPROVED O REJECTED e BY FAA Ft Sean Ignite ihilinuSicturer = lawin am Ditiar ) FAA Deligai• Rfn Statim Palm Awned by Tremom Cann Antos - • • Date of Approve/ or Rdedion 8/3/A Ł- - Dann Cwanallo. 5267/5494 IA Signature of ' Michael Donotfly SDNY GM 02754211 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFM_00241133 EFTA01326726 - FAA AIRCRAFT REG} AIL 0 .7. CAMERA NO. ort . .• N.* • NOTICE Weight end balance or operating limitation changes stall beentered in theMpopriste aircraft record. An alteration mug be compatible with all rots alterations to mane continued conforzeity with the applicable airaorthioas tequitemects & Deaniptlem fl out Accomplished (If more space a required. mad Coed Meat. Mat with Jinni nanceality ad regbaatire ark ard date workcm0lfrd) August 31, 1992. Cruz/seem Aeromwe Corp. MedeIG-IV, SIN 1085, NSSGA. FAA Type Certificate Data Sheet MINA￾FAA APPROVED DATA:1 FAA form 337 dated August 2, 1991 for this aircraft; FAA form 8110-3, Statement of Compliance with the Federal Aviation Regulations, dated 4-6-90, for Gulfstream G-IV . Airplane, GAC, List of Data - Identification - drawing 11595B41039 REV A dated 4-6-90, effective for aircraft 1000-1130, titled APU SILENCER GARRETT GTCP36-100G PEP 39 (G-IV) TOP DRAWING; and FAA from 337 dated December 27, 1989 for this aircraft detailing STC No. SA 1 I INE, dated November 24, 1982, covering the installation of PATS P/N 43206-9 FAA/PMA louver assembly. The purpose of this change is to remove the Gulfstream Aerospace Corporation modification to the Auxiliary Power Unit's (APU] Accessory Cooling System installed by PEP 39 and re-install the previously approved configuration that uses the PATS, Inc. APU Accessory Cooling LOWCI. Removed the GAC P/N 1159B21419-93 panel (APU inboard enclosure wall) and re-installed this aircraft's original GAC production P/N 1159621419-79, Rev. MI (date code 0887) panel. Re-installed the PATS, Inc. FAA/PMA approved PiN 43206-9 Accessory Cooling Louver and attaching hardware onto the 1159B21419-79 panel. Attachment of the Accessory Cooling Louver is detailed in the above referenced STC SA 1 1INE and was accomplished with 5 each NAS1103-3 bolts; 5 each AN960CI0L washers; 5 each MS21059.13 nuiplates that were attached to the panel with 10 each MS20427M3-3 rivets. Performed operational check of the Auxiliary Power Unit, including electrical and pneumatic loading, using applicable procedures contained in the Gulfstream Aerospace G-IV FAA Approved Aircraft Flight Manual and noted no abnormal or unusual operation before, during or after the operational check Recorded compliance with this FAA form 337 in the aircraft's maintenance records. and returned the aircraft to flight status. No flight manual revisions or supplements were required or installed as a result of this alteration. No changes to the aircraft's continuedAirworthiness inspection schedule resulted from this alteration. It has been determined that the interrelationilip between this change and any previously approved configuration will introduce no adverse effect upon the Airworthiness of the aircraft This determination includes, but is not limited to, consideration that: there will be no cockpit procedural changes; the modification is not related to any safety or Airworthiness condition; the design of the APU compartment and accestory cooling arrangement wall:tot allow fire migration to other areas of theaircraft; and this alteration was previously installed on this aircraft (and other similar model aircraft) with satisfactory performance. N changes to the aircraft's electrical Iliad analysis or aircraft's weight and balance report were required as a result of this modification. Mu morn reented ism ;awed* Wad Darellyag s'/UN/1o. lied sr evottaaeallOA0131MODCC. ' NO ADDRIONAL SHEETS ALE MIAOW •E".1" O Additional Sheets An Attached . • SDNY GIN 027542 2 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I I 34 EFTA01326727 ! is glattilOttf 22:11-ItT 8. Iiii_2_ • . - .- • • ---- • c 1 • I ® . MAJOR REPAIR AND ALTERATION uloon.m. • Yeafreae, Powerplant, Propeller, or Appliance) Pa•flem MISISIa • °VS. tire:a Fos FAA Um Out aka Wotan cat- r:io d Icentocnotcs flint or type all truism See FAA 43.9. CAR 43 Appanclix 8. and AC 43.9-1 W SubFAKAnnt revision thIll*On for Instructions and dispoiltkannf this font This c4GOrt Is required by law (49 U.S.C. 14211. Failure to ', Put an rnuft In &del Penalty not to exceed SI 000 for each such violation (Section 901 Federal Aviation la of 1958t I. Aircraft • Make Gullictream Aerospace Mot C-IV Sall No: INS Nalianakty and Rcatittation Mart MCA 2. Own= Name (A. flown on ntuntoo crate) B A Leasing & Capital Corp. Address Qs mown ea recierefiee cerolleas) The Embareadere CS Sas Freaclacs, Ca 94111 I Far FAA Ube Oaly • 4. Usk lilltes 5. Tyre Una Maim I Model I Swig Ha poplar as Airframe (As described in ltan I alms) •••••••••••"•••••• . , X Rowerplani Proptier Applience IYIse Maullocemor it. Comforsity ware A. MeembNee eat Addles B. ICS of Agpacy C Dans No. IAMB A. MAITESON 1560 E. SAN FELIPE DRIVE . SCOTTSDALE, AZ a ISI X U.S. Certificated Medanie Fortran Certi6mtet1 Matta AP 1964•49 Catficated Renee Stencil hunufecturer D. tautly cha the near and/or ammo= aide CO the Se) ant m E 4 ton sal delabed an the warn or asahmeta balm taw beat meat is =orders with the reciremeas of Pat Odds U.S. Feted Mt Regatta= el Rase b ass facriehal herein at= eitt awed tots be of ay browledar. , 7-3•TZ.--- Sapience oraliatlas ' . 7. Appreval fec Raw te Sank* Panel to the tabor* Pan paums Readied below. the lack deeded la ism 4w leipeCted 1 the se= pessibed by the Ancohnimior of the Freed Mt Ailmicuarsion and is CO APPROVED 0 REJECTED yli - FAAFIL ii=Yril Mambas= x bspeenne Areharsom to (3pea4y)• • .• BY •FAADeilpes • Rape Swam Paws Apprecald by Ilaapas OW& KIEWIONWIS criccp Dan Approval or Rejection 7 4 7s- fe OwcifieW or Docipnfolth. - SUMS IA of 12/ 4;nt . namely (84-82) SONY GM_02754213 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241135 EFTA01326728 Li-fittilli"off at:Ilinsiiiin . NOTICE Weight Wbalance a operating Sitation chimps shall he altered in the oppropiate Mash mead. An alterstion amt be complete with all previews abatis to assure continued conformity with the-rehab& ainvonhinen romirements. t Dem*San 'Mark Ateemp tithed (If ma spa a required nI isidawne ,he . Idwity web Mae rationality aid region= mak and data wart canerad.) 07/0492 Gulfstmom Aensspace Corporation rag Model G-IV, Sale Numbei1085, NINCIA, FAA Airco& Type Cattalo Da Sheet Al2EA. Aircaft in-wince data wl116.5 home and 449 landings • Refer to the following FAA Approved Da FAA Free 8110-3 Statemerd of Compliance with the Federal AViAli011 Regulations dared 2392 for Gulfstream Model OW, 1159, & 1159A; listing GAC Repel Deg 1159SB30189 REV. C tine CORR0SIO,Y REPAIR/BALLAST net., CONT. SUR', ELEVATOR signed by S ts DER John G. Wilda, Desigraten Nimiba : Refer to the following FAA Acceptable Data: FAR 43 Appendix Ai FAR 91417 (bk GAC G-IV Mainteninie Memel {hung tat aim Revision 16-1. dated 30 March 1992; GAC G-IV M/M Vol. 1; REVISION 16 dated 6 DECEMBER 1591; GAC Production Dwg. I 159r-S20434, titled SP:NOME CONTROL SURF-ELEVSTA 1100 to 165t78 LE e l & 2 of 2, REV 0 deed 12-10-91; and akc Production Dwg I 1-59CS20443, tided BA/7-ATINS72. CONTROL SURFACE- HZVATOR. eh I & 2 of 2 REV F dated 10/21418. The petit of this repair is to inspect the and remove any onaoson that has pruned onthis airmails elevator control surface in the inn where the den= ballast weights me attached. This inspectenheair involves: A. The removal of the le and right devators from the *Safe B. The removal of the leading edge riveted alit to pin access to the ballet weight assembbes and idiots Mutant; G Idatifying the beast mania removing the What weights and inspecting *weights end enacting hardware for comnion; D. Inspecting the balance beam assemblies for OXIDTIOEL E. If cat is found, the removal. peponten and/or treatment of the affected areas; and F. The proper re-staanbly, balancing, sad seemed of the elevator control surfaces to the aircraft . • In =ado= with the GAC Comp sued Mentenmce Program (CND" cedes 273007 and 273008 removed left and tight eievators from the Matt Removed the leading edge skins of both elevaion. Identified all ballast wages fa popes reasaanbly, removed the ballast wages, and pined areas to the balance beam assaults. Perform= ramectice oftodi elevator assemblies and attaching parrs in *accedence with the above referred to GAC Repair Dwg The inspection reveled centre.,aim and cad olotint wet not intact on both elevators • Perforned CORROSION REPAIR PROCEDURES FOR LEFF AND RKBIT ELEVATOR LFADLNG EDGE ASSEMBLIES it accordance with the above referred to GAC Repair Drs. Note: NO interim rework was pestered. Re-assembled the Sad elaator ballast weights in their anginal paell' using new hardware purcbased fuze GAC in accordance with above mimed to GAC Production Dwg. detailing BALLOT (WEIGH?) MIL CONTROL SUREACEBLEVATCR. In accordance with the above referred to GAC Production Dwg. detailing SIGN MTh ends original =dile edge skin (which ms within let) after popes preparation and tearment Treated, seabed. Primed andPanced to match ell ewe metal In scieadance widiebeGAC MINT ATA 27.0 Right Control Systems balanced both dentin (LH elevator 0.0 inea. NOSE HEAVY and RH elevator 0.0 in/lbs. NOSE HEAVY) In accrete= with GAC OAP codes 273007 and 273008 re-installed the let and right devotees to they proper positions on the Aiwa Perfomsed den= credrel tenet check in accordeice with GAC CLIP code 273005 and palmed gust lock system function test in accattmee with GAC Cie code 277015. The Mere was not test flown became it was determined that the repair this we dale did not chorine the gee chenconistics or substantially aired the thght operation of the anent This detention included, but was not firmed to, conederation that the elevator atemblYs weight. balance, shape, strength a engine type =Sat deep was not charged Recorded compliance with this FAA form 337 in the eradts maintmance meads and reamed the tart flight status. No threes to the Suits wage 'rebalance reseed from this repair. TA.€0•PoIAI TAAAAAA b. Prnrod by swiss Deny tag gppwn.nk OM NA cirattLONSIOA0790110-DOC NO ADDITIONAL SEMI AS! ATTACHED "MA 0 Additions/ 9seet Are Anschon1 SDNY GM_02754214 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241136 EFTA01326729 ![..I.RIEVATcri 'MI78117/92. MAJOR REPAIR AND ALTERATION oz. Denim ' doweiemo (Airframe, Powerplant, Propeller, or Appliance) t •••• sawwwi asid•• w cm, •• unarm • For FAA Vag)* OIS•4 Iseediteacs 6714 -Erie INSTRUCTORS. Print oc type m entries. See FM 43.9. FM 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for irdstrual005 and disposition of this form. This upon is required by law (49 U.S.C. 14211. Failure to report can musk in a dull MANN not to exceed 51.000 for each such volition (Section 901 Federal Aviation Act of 19591. I nog . Make Gulfstalas Aerospace Model ' ei-W Said No. 1085 Naafis/Sy and Registration Mat MICA .2_ Owner NI= (As down on revere= waffle) B A Leasing &Capital Corp. • Address (As shown on reyestrytion ontinars) Two Etabareasitro Center Sea Presidio; Ca 74111 3. Far FAA Use Duly • 4. :US Ideallieseke - I TIP, Urea Make Model I Sail No. . Rya Altimeion Airframe . t • • (As dumbed in Solids:we) ••••••••"•••• **** X ToNerptint ' Propellor ' Applierce TYRF Menabansw • ,_ C. Comfanoltr S￾A. Afgatiline and Addran B. Kind of Agway C. Ceetlicets No. LANCE A:MATTESON . /56OE. SAN FELIPE DRIVE . SCOTTSDALE, AZ SS= X U.S. Certificated Mechanic AP lart4049 . - • Fon,* Certificated Mamie Cathode! Repair Sega= Menthe= D. I eatify tha the rep ir auVor Mentixt made to the wa(e) identified in ilia 4 lave and 6ineribed on its inert or Mschinsall halo have bom Male ta exordsoce with the require:0am of Pot 43 of the US. F Atm end this the informsion famished hetein is erne and comet to the bear. my knowledge. Dale Signal= o t Asoroval kw Retro (*Swam Parma to die Mb:City Own pawns speeded below. the exec identified in item 4 wet imposed in the larAtlf prte oSsel by dm . Adminatneor of the Federel Aviaioo Adnunierrawn end is I APPROVED CI REJECTED BY FAA Ft fwd.* Isq•cras MantIfiCtuter x blipedn Althodaliati Odes (Specify) ' ' • FAA Dawn Repair Stake Fano Approved by Tempo Gouda Airercohinea Group ' • Date' f Approval or Reaction 2 -9--9 coats. iv D•dpidc•N• SIMIAN IA Signinue of Michael Death /AA Fern ISTIOS-931 • • • SDNY GM 02754275 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 • EFTA_00241137 EFTA01326730 }" c rA E NC oI P. AFT V . j .E DCA]; T r: F.I 171, 2.. - . . • ___ NOTICE Weigh and ISilanee or operating turatabon theists shall be enterod Si the appropriate aircraft record. An skerabon net be comp:Wilk with ad pmious she:Mons to assum continued °andante/5r with the applicable airworthiness requirements. t Daserlptlee el Work Atebenplisbed (If mom ry s s molted. mach additional ahem. Identity welt mend rwionassy and rouration mark and Wu work completed.) lime 23, 1992, Guffstream Aerospace Corporation PAC) Model C-IV, SIN 1085, /488GA, FAA Type Certificate Data Sheet Al2EA￾R.cfcr to: GAC FAA Approved Aircraft Service Change MSC) Number 175 A, SUBJECT: POWER PLANT (AM 71) ADDITION Of FIRE ;Nap PO ACCESS DOOR HINGES, dated: .kPRIL 10, 1993 The pinyon of this service change is to improve the Sr resistance of the engine component access doors . located on the engine cowling, "Ibis alteration replaces one aluminum hinge assembly, attaching engine component access doors to engine cowling. with a stainless steel assembly. This change in conjunction with \ the two existing fireproof latches, wit provide a sturdy three point support for the engine component access doors should the remaining aluminum hinge bum through. The purpose for this revision to ASC 175 is to update the hardware Cams( on Figure 1 and change the location of the 1159P41270-25 and -26 hinge halves on Figures I and 2. It also updates the ton on Pages 2 through 4. Performed all of the MODIFICATION INSTRUCT ONS listed in the ASC 175A for aircraft 1000-1137. All Stalled parts were purchased in Kit Form from GAC Product Support Savannah, Ga. 31401 Returned the acraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's maintenance records. Filled out the ASC 175 A complinc card and returned it to Gulfstream Aerospace Corporation. There was no change to the electrical load analysis data. The effect of this change on the aim-rafts weight and balance data is wait ma commuter $ennaor form w does on OPINalleit. bath; WORD ZR Mod lb CflASC1/51..doc pawed by Modal Downy. NO ADDITIONAL SHEETS ARE ATTACHED. °ENV - O Additional Sheets Ate Attached IllbodelPnisseovan- - I :••-•T w`-'1W:71-trit,1*, SONY GM_02754216 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241138 EFTA01326731 ILi• FAA AlPgtA. Tr AELITT. : 2 8117j /91 i € . • MAJOR REPAIR AND ALTERATION en. du (Airframe, Powerplant. Prophet, or Appliance) snanine.. on", nhao if IAA Or Oily Oran :ant Ci llt - D O INSTRUCT/OHS: instructions and penalty not to print or type all entries. Sae FM 43.9. FM 43 Appendix 9. and AC 43.94 (or subsequent revision thereof/kr disposition of fhb form. This report Is required by law (49 U.S.0 1421). Failure to report ran result in a chit need 54000 for each such violation Genoa 901 Federal Aviation Act of 19S0. • I. Aircraft Make . . . OW &main Aerospace Model G-IV Soil No. DOSS.: i . Nationality end Registration Mark N8SGA 2. Owner Name (As shown on repentionatIllfinta) B A Leasing &Capital Corp. -' AMP= (As duns sw. repaired= webs) Two Embircadero Cater Sao Francisco, Ca 94111 1 For FAA Use Ooh • 4. thdlIdinstMeallan t TYPO Unit Make J Model I - Se:1Mo. %ma AMISS Airframe (As desenbed in Ran I shovel 77-7"nr•••••••••• ., . a Powerplant _ n . I — Propelier .. I Aptatianoc ITN .. • • . .. . A Ormferadtv Stamm & Althen Naas md Addles - B. Kind of Mery • C. Cordes No. . LANCE A. MATTESON ' - OM E. SAN FELIPE DRIVE SCOTTSDALE, AZ 152.51 X U.S. Cannata Mechanic AP 1144049 ' Foreign Conflated Mechanic Certificated Repair Stanon I Manufienzer a I catty that the repel nutty Litton made Co the muds) idantdied u nem 4 above and described on the mans or such:nes hereto have beat made m accordance with is rommeaems of Pan 4) of Me ti.S. Fettle* minim 4ultw ad tha the intonation furniahad henan a woe and cornett/add ben ci, my imowle Dare L-45- rz__ Signature of T. Antos/ fee Res* to Sevin Mosowa to the audio* given poem specified below. the us Weeded in itan 4 was impend in the at pmcdtel by the Adminintnix °film Federal AVILOIT Admirtionnon and is T APPRONTD El REJECTED . BY FAA Ill Sam* lawn' Manufacturer • Manton Andiontaion . ! ! i : 01. 440 1POMYY • FAA Despeo I Reps Banal I Person Approved by Transport : Canakb Aineonitineas Dote of Approval or Rejection I cenliamw pawn wo. 7 -7 -92- i s:67.5494u Miebad Dorm* Ng • 1 1 eityYeeplinteeteseA71:=0.A4aPA"•;eat 2Mortedatili tlhTe.;i SONY GM 02754217 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241139 EFTA01326732 IFF7997:7:17:71, -7•••• rte.- - — t Description of Work Accomplished Of MM. s. la required. wtach. Wino:Cud ghee. Weald y with wash ruccrishry mid regtanon mast sod dat week comps]) lime 23, 1992, Gulfstream Aerospace Corporation (GACI Model G-IV, SIN 1085, NSSGA, FAA Type. Certificate Data Sheet Al2EA: - • Refer to: GAC FAA Appftved Aircraft Service Change (ASC} Number 175, SUZUECT: POWER PLANT (4TA 71) ADDITION OF FIRE SHIELD TO ACCESS DOOR HINGES, dated NOVEMBER 151 1991. The purpose of this change is to ®paw the fire resistmee of the engine component mass doors located on the engine cowlingg. This change replaces one aluminum hinge assembly, attaching engine component access doors to engine cowling with a stainless dal assembly. This change, in conjunction with the two existing fireproof latches, will provide a sturdy three point support for the engine component access doors should the remaining aluminum hinge burn through. Prepared the aircraft for safe maintenance and pertained all of the MODIFICATION INSTRUCTIONS fisted in the ASC 175 on the above listed aircraft All installed parts were purchased in Kit Form from GAC Product Support Savninah. Ga. 31402. • - „ ---• —• •••— — SDNY_GM_02754218 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241140 EFTA01326733 • o REGISTRY CAMERA NO. j DATE: 7.-43^9a Amer.: am m ZID=5 el- - . MAJOR REPAIR AND ALTERATION "Brix* UN ORO sloes slew (Airframe, Powcrpbat, Propeller, or Appliance) "rata -I a.sem se i14/1•10110•• to cb( '-' ":5°P° INSTRUCTIONS: Mot of Tyra all entries. See FAR 43.9. FAR 43 Appendix 8. and AC 1 211(fr subsequent revision Llano° for Inatnfolora and diSpraicIon of thks fomi. This report is required try las (49 U C 14 1 allon to repels can naSuk In a civil Wan not co exceed 11 A00 for each such viola/Jon /Section 901 Federal Aviation Art of 19581 I. Aireaft Mike Gtestreatii Anne, Mat -IV G r Sail No. I885 Netionnlity end Registration Mick NSSGA 2. Owner Name (As ibmemoa resimmtion oblate) B A Leasing &Capital Corp. Address (As tan on repstretica eaftillcale) Two Ensenada. Cater Sem Entedeco, a 91111 3. Per FAA 1. se Only 1 4. Unit lamellate S. TM. Unit Make I Model 1 Seel No. Rot Notion Anframe (As desated in [enlace) ••••••••• I Powerplant Proyelter Appliance TYPI i _ .— 4. Owtherstie Smatter A- Mori time al Mem ' B. KM or Mete C Cease Na LANCE A. MATTESON WO E. SAN FY-LIPE DP 3In sCOMDALE, AZ U2 X I U.S. Cali oted Mabee AP 1$6•4049 7 Fatin Cathode Nicehertic Canie' Rpm Stetson Manufactura D. 1 cal* Na Oa I WS See ention meek to the nee) knife in kese e Mee od dente on the tome or mactentota hereto have bookmade in meordetese Ma the requirements of Peet 0 cite U.S.F kisiion Repletion. arsi Ms the intent= farnisle heel is tem te aana to the bet o my knowtedm De Sh; 1e￾Signettre f 44 1 . 7. Amwerral ter Rein O. Sonia ' Pursuit to the cabocity siren parsons specified Wow. the unit identified in item I ea heed OM mamer presaileed by the Athena of the Federal At Adenine= and in CM APPROVED 0 REJECTED BY PAMIR Image Iwomet /*antam= i hopecion Mehrehation . . Other (Spacity) FAA•Dmisme Rape Oise Peon *Wee by TattOxi Omani Airmathinim Group --51 Demo Amoral or Rejection 51 i i if z__ engem or .10esipsdaaNt 5247•304 IA Signature of ' /gyp/gyp nddvi . Maw/ Donnelly IAA lwt 137(0s-el) - . . • • SONY GM 02754219 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024/ 141 EFTA01326734 FAA A1RCRAFT REGISTRY CAMERA E0.31.4 DATE: 7 -a3-qa NOTICE Waght and balance or °pawing limitation changes shall be entered in the appropriate thrash record An aeration must or romped* with all previous &cations to rinse contirmed conformity with the applicable airworthiness requiremaus. Description of WoricAccomplbbed Ornate trace u mired, mach addmorwl Meow Me m* was matt reoccubly and registrar= rust rd das work completed) May 28, 1992, Gulfstrcain Aerospace Corporation {GAC) Model GdV, SIN 1085, NSSGA, FAA Type Certificate Data Sheet Al2EA. Refer to: GAC FAA Approved Aircraft Service Change (ASC) Number 187, SUBJECT: ICE AND RAIN (ATA 30) P1TOT HEAT ADICATION - 31ODIFICA77ON., dated AUGUST 3, 1991. The purpose of this change is to provide annunciation for the pilot heat system which will better reflect when power is applied to the haunt. Presently, it is possible to ept at OFF light in the picot heat system when one of the heaters is not working and one is working. This ASC wig eliminate the misleading indication. This change reroutes wiring in the relay and junction paned (326A1) and will require approximately 15 man-hours to complete on the above listed aircraft. Performed all of the MODIFICATION INSTRUCTIONS listed in the ASC 187 for aircraft 1001, 1006- 1143. Note: removed the 326A1 panel from thuairaaft to do the modification. Noted the following errors in ASC 187: Wire Number F217A20 should be removed from De stsch Ground Terminal Block ¶24-B* and discarded and Page 7, Figure 3, Triangle 2 should read "ACFT G-IV S/N 1001, 1006.1143' instead of 'ACFT G-IV S/N 1001, 1006-1043'. Note: it was not necasary to use the wire number F214A20 or the OAS805A3 Splice to extend the existing wire. • All Stalled pas were purchased in Kit Form from GAC Product Support Savannah, Ga. 31402. Performed Operational Test in accordance with ASC test procedures paragraph F all pans and noted no abnormal operation. Returned the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's maintenance records. The effect of this change on the aircraft's electrical load analysis data is negligible. The effect of this change on the aircsafrs weight and balance data is I:eery/Mc. This computer gsnenaor to win dons on gPfb08016: miss WOW lac EMS m CAASCIttdon prspad by htszhael DormeBy. NO ADDITIONAL SHEETS ARE ATTACHED. *DID* C Additional Sheets Are Attacked • I • • - • ••I SDNY GM 02754220 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241142 EFTA01326735 FAA AIRCIAPT. RECTSPRT CARRRA 20 An' 7-as-9 • MAJOR REPAIR AND ALTERATION utoccreft. a Vensosnmen (Airframe, POMONTIlarlt, Propeller, Or Appliance) ' aigliniimmo. Arbemerso FOrm Approvtd -- No. 2120-0320 OW For CAA Use Only arepicatlog.. 4- I A-- -s- ,>-) . . ..... INSTRUCTIONS: Print ortype all entree SeeFARCEI.FAR 43APPendlz B.IndAC43.9:1 fOreolsemittent reTfefenihere*BN4Inetnlebone and Opposition of Pus form. This repents fequIred by taw (401.1.S.C.1421).Fellunobareplet Can Mull in &ChM penalty none weed St.003 for eachasiCh violetiOn ISection 901 Fedor& Amgen Act of 19663 • I. Afrereft Make GULFSTREAM AEROSPACE MOW G-IV Renal No. 4 loss Nahonakty waren Mark 2. Owner Name f AS shown on sestisirstkon ceMbeeffl • BA LEASING & CAPITAL CORP Addiees (As shown on regdfrafhan 40bl'asfe) TWO EMBARCADERO CENTER $AN FRANCISCO, CA 94111 . 1. Fee FAA Use Only • 4. Unit Identatcatfon E- Type Una Mane i model I 5.1,51 NO Reim" Allefabon AIRFRAME /As Pe <va t labs I Y XX POWERPLANT PROPELLER APPLIANCE Type Manufalswer • • ' S. Cenionelty gleeestiont tv A *genera Name end Address 6 Kind oe Agency C. CertItIcalle NO. LANCE A. MATTISON . 8560 EAST SAN FELIPE DRIVE SCOTTSDALE. AZ 85258 . U.S. CNINCSOUOCINnoi , - .1411 1864049 formptCortscatal mammas Conan:me ReerStahon Inool.if hoot ' D I certify oral the repair endAralteratton made to Me un HQ. earned Molten a above and drartbed anthem...armor Attachments Wee hare been made in ageOrciance wen me requirements of PIO 43 of the U.S. federal AviSSOA Regulations end that the information furnished he 4 trot and correct its the Deal of my nootedge. Date 3..4—/C44 —re...._ • • Signature of Au heft Inchvalc a_ . ' • . Approval log Return To &NUM . Pursuant ACInonottfll0f BY 10 me authority given persons speed*, Dam. Merit q•nbffed in dem A wet oUPOCIO0 Ifithe mina, prescribed by Ibe of the Federal Aviation AOTiroMfIlliOn and it e APPROVED 0 REJECTED l FAA Al. Slandards InspKior Itifanulacturer . X• Impeehon Authorization Other CS:Meer) • i FAA Designee I Roper Smoon . , OVIOO OOPIOVNI by Transport Canada Antennae= Gr o DIII•01AppflowidOnlyeCtOn I CANUICalto Of Designation No 514/ 4 f e- i 5267054941A Stratum of Ind I • , MICHAEL DONNELLY FAA Form 037...... VIZAWFV2aivettags;il; SONY GM - 02754221 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241143 EFTA01326736 PAA AIRCRAFT REGISTRY CAMERA NO. -Si DATE: 7 -a3 -ega • NOTICE Weight end balance or operating limitalionthanges shad beenlered In the aPPrOPriale aircraft record. An alterttion ri sat be compatible with all previous alterations to assure continued conformity with the, applicable airworthiness requirements. Deees.pUeo a Mat A.ccOingiahed ' at mom , P, C11 is required. MICA eristitionei sheets. Identify with small nalionanty and registration mot and date rent cOMMIS.1 . May II,1991. Gulfstrtarn Aerospace Corp. Model G•IV. SIN 1085. MUG& FAA Type Cad:Scats Data Sheet Al2EA. Refer to: Gulfstream Aeritspacc Corporation FAA Approved Aircraft Sat Change Number 157 SUBJECT: FIRE PROTECTION (ATA 26) SMOKE EVACUATION VALVE INSTALLATION - BAGGAGE COMPARTMENT, dated March 27, 1992; Gulfstream Aerospace Corporation FAA Approved Aircraft Flight Manual Supplement 89-03 Rev B 16 January 1991; and FAR 25.857 (b). The purpose of ibis change is to install a system designed to assist in smoke and fume evacuation from the , baggage compartment aft lavatory and aft galley areas. The system allows the baggage door seal to be deflated and allows cabin pressure to evacuate smoke overboard past the seaL A two position manual selector valve is Stalled above the cabin entrance to the baggage compartment. The valve positions are • labeled EVAC SMOKE (deflates the door seal) and NORMAL OPS (normal control of door seal) An access panel will need to be designed on installation to match cabin interior. This panel should be' designed so it cannot be closed when valve is not in the NORMAL OPS position . , Performed all of the applicable effecfrvity installation instructions detailed in the above referred to ASC 94 installation instructions. Fabricated SMOKE EVACUATION VALVE access panel cover to match existing interior scheme and so that it cannot be installed when the valve is not in the NORMAL OPS position. Performed installation check out by complying with ASC 357, paragraph C, Perform installation check￾out as follows: all steps. Verified that the aircraft's flight manual has the above referred to flight manual supplement Stalled that details specific EMERGENCY PROCEDURES dealing with SMOKE AND FUMES EVACUATION and SMOKE IN BAGGAGE COMPARTMENT, AFT GALLEY OR LAVATORY. Recorded compliance with this FAA fonn 337 in the aircraft's maintenance records, antretumed the aircraft to flight status with SMOLT EVACUATION VALVF. in the NORMAL OPS position and the access cover installed. ft has been determined that the interrelationship between this change and any previously approved modification will introduce no adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to, consideration that the cockpit procedural changes arc included in Inc - aircraft's FAA approved aircraft flight manual. No changes to the aircraft's electrical load analysis or aimraft's weight and balance report were required as a result of this modification. pfisIZA/SCe WORD ell CIASCI b7.dac. prepind by: 311ctel Doetily. NO ADDITIONAL Slare ARE ATTACHED. '72,1r O indilparial Sneels Are Attached •U see 1 Del-C.44.1%11 •-• ..... • - SDNY GM 02754222 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0(1241144 EFTA01326737 callmiCem-wpworar ar:fesinar-Z - -4014a4. MAJOR REPAIR AND ALTERATION us Deounee crewman:nu (Airframe, Powerplant, Propeller, or Appliance) resew Dwane, 1 Fortet OMB N Approvod _": "' o4124020 t￾Poe F PA Ueet tirdy 0ariltentircatkut az. -}st)o INSTRUCTIONS:PAM or typfaii entnes.See FAR43.9.FAR 43 ADO•nditt B. and AC 43.9-1 fOttubsecluatra feeniOn l‘feOR inf insinfain sad dispotation clot form.TNaseport is requited bylaw (49U.S.C.1421). Failure to Japan can redone Advil wally nOI tended El.000 tor each such violation fSecti t Federal Aviation Act of Ma). 1. Alactift Mak, GULFS AEROSPACE _.... tac4/4 -IVG . Seri& •No. 1085 1, A • , Nationality and Registration Mart N88GA 2. oilleet . NOW (As shOwn On feetstraMt Centaca40) &Ain& & CAPITAL CORP. ` N. • Adana= (AS shown on repisoolion coadielOW TWO EMEAFtCADERO CENTER -- SAN FRANCISCO, CA 94111 - '. • • ‘ - a: For FAA Use OW/ - / i r A • - 4. Unit Identiricabon E. Type Unit • Mate MOCIel . Serial No. Regale Attomoon AIRFRAME i 0 towel XX POWERPLANT PROPELLER APPLANCE Type I I . leanufaCtunof . IL Conformity Stateroom' -. A. Agency's Hama and Address 8 Kind ad Agency " I C. Certificate No. LANCE A. MATTESON 8560 EAST SAN FELIPE DRIVE RflITTST)Al IF A7 tic7 AR U S °initiated Medstme AP 1864049 • • Soften (.'olaCatea mamma ! I Condeams Rene Simon I I manutenutee . 0. i heath" IPPON wad anOtor auenthon made To the wets) 'annul:HI in nom 4 atroveand °ascribed on tfie revene of attatnin•Alahatel0 have been made in accoreance with the movements or Pen13 of me Y.S. Federal Aviation Regulation, and that DM information .. furnished herein is live and carted to t tend 01 my ancsiodge. • .. I • Date i Stratus/ ot Aum indm,S ..e r-e•e'f . 7--.. F. Approve. toe Iheiton TO Sanaa - Pu Aorrosostrator BY suam to tne authority give persons specified below. thejel identified in item 4 was inspected et me manner presctibsd by Me of Ine•Federat Aviation AdmomstraliOn and is A APPROVED CI REJECTED ' ' FAA Fie Standar:IS InSPector Manufacturer' . X InSpeCtiOn AWN:tea:4n Other iSooe•Pn • . — FAA Designee Repko Station r i Person Approved by TransoOn I Canada Aneonhautes Geo Date of Approval ot &Poulton Censticalece.. ' -47;57fr Designation No. ia 5267•54941A -•.• ' - Signatuted1Se _MICHAEL DONNELLY FAA Foam 337 to aft SONY GM_02754223 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 145 EFTA01326738 TIMA AIRCRAFT I STRY Mtn: 6* -OO -sAti cAr. so. I Ai NOTICE Weight and balance or operieng limitation changes shall be entered in toe appropriate aircraft record. Analterationmuffed Compatible with all previous alterations to assure continued conformity with the applicable aliwOnhiness requirements. De•Cripti0n el Wort Accompliahed (if trent space if retorted. altaell eddittOnat aneete identity with *meta nationality and registration mei, and deft wore contoarecH May 14. (Mfg:ream Aerospace Corp. Model G-IV, 544 1085 8188GA. FAA Type Certificate Data Shed Al Va. Refer to: Gulfstream Aerospace Corporation FAA Approved Aircraft Service. Change Number 94 SUBJECT: FLIGHT CONTROLS (ATA 27) GROUND SPOILER FAULT DETECTION FUNCTION TEST - MODIFICATION, dated July 31, 1991. The purpose of this change is to eliminate removing the interior to gain access to the relay and junction boxes in order to perform the required tests during the 18 month inspection. This is accomplished by relocating the Ground Spoiler test plugs from the relay and junction box to the left hand avionics shelf. Added jumper connectors will simulate relay removal required dining Fault Detection tests. Performed all of the applicable effectiviri instal/anon instructions detailed in the above referred to ASC 94 installation instructions. This change adds 4 test plugs on the top left hand avionics shelf and modifies associated wiring. The installation required approximately 69 man hours to complete. Replaced connectors 07L2P1 and 07L2P2 with new .Acro Electric P/N AE559L10SL3S-B connectors. Noted the following errors in the installation instructions: Step E, Page 5. ASC94K901B and ASC94K902B should read ASC94P90113 and ASC94P902B; Step E. Page 6, ASC94K903B should read ASC94P903B: Parts Required. Page 6. item GAC800PT18-32PN Plug CHECK delete the word CHECK: item GAC800PT18-32SN is not required; Figure 5, Page 12, Wire O165O20 wasiis connected between TJIT-D: Figure 7, Page 14. Wire G173A20 vtavis connected to 1121J-F nein though effectivity is listed for 1096-subq., Wife WI43G20 connects to TJ4U-K even though effectivity is listed for 1096- subq., Wire G I 88C22. wavis G 188C20. • Performed installation check out by complying with Gulfstrerin Aerospace GIV Computerized Maintenance Program Code 276004. Ground Spoiler Fault Detection System - Ftfilictional Test and Code 276001 Ground Spoiler System - Functional Test and noted no abnormal operation. Note: Disconnecting ASC94P901B is the same as removing NUTCRACKER RELAY It: Disconnecting ASC94P902B is the same as removing NUTCRACKER RELAY 46; Disconnecting ASC94P903B is the same as removing POWER LEVER IDLE RELAY #7.; and ASC94.160B has the same jumper points as 325A1J60. Recorded compliance with this FAA form 337 in the aircraft's mairiumance records. and returned the aircraft to flight status with ASC94P901B. ASC94P902B. and ASC94P903B connectors installed. It has been determined that the interrelationship between this change and any previously approved modification will introduce no adverse effect upon the airworthiness of the aircraft This determination includes, but is not liMited to. consideration that there wit be no cockpit procedural changes and the modification is not related to any safety or aisworthiniss condition. No changes to the aircraft's electrical load analysis or aircraft's. weight and balance report were requited as a result of this modification. pS iwse. W0Ill) in CSASC94 dot papered brIdatiel Daly. IC ADDITIONAL SHEETS AM ATTACHED. t%O• a Adla'anal Sheets Aol ATIKNO .4 C: nlsesa) n, SDNY_GM_02754224 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 146 EFTA01326739 FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: 3 - 20 - 12. i12//01€41P' 0 MAJOR REPAIR AND ALTERATION ""."-I v."' I rwiftn°1113APP473 2120-0020 Mearnenen JAN 3 0 e.c.12 Porverplant, Propellei,eir Appliance; For FAA Use Orta/ ' cslomooren (Airframe, aimItTAWorn • - -- — .. • - - - • ' - • ' •-• VNY FSDO Office Identificatice • / 11 -O -0 ' INSTRUCTIONS:Print or type all tedriesSee FAR 439.FARCIAOpendix Band AC 43.9-1 (or subsechsent revisionthereof) for inslifictIon$ and dittaMitiOn Of MIS bon. WM MOOR Mier:wired by law fitil U.S.C. 1421). Farldreto repartees result i acne conaltynot tattooed SISOO for each such violation (Section WI federal Aviation Act of ISSIO I. Alma Make Goirstream . Mmpr et • Model Crlir Sena! No. LOSS adendlity and Rearadon ark . MEGA 2. Owner Name (43 shown on norstrorion corriAcirl) -. BA Laskin ad CROW Corp ' : ...r.c raficlrele (As strewn on registration arid irata) Too Esibenalsro Cabe as lbsodue, CA MILL . 3:Fee FAA the Oak ... - 4. Unit karma:Won S. Type Unit Make Model Serial No. Repair 'Alleration AIRFRAME .--..-. awr.rwiwerre~wwwweat dintweedMO•nr) abort/ x .• POWERFLANT PROPELLER I . APPLIANCE Type li rir m • • Manufacturer ' ILICanteivelly Saran A. Agency's N Me and Address i b. bind ol A$14aCY . C. Cerra-cam No. :Western Commaarkf, la lit w? sal Lidos.* . • RA311801LAbtrae 3,4 1000 Dall y_Drive Faeign ta.rals muse R•49 1, 2 & 3 Van Num CA 9140f ' . X Cortir,unto RePalir Slaw e r m,t, . Menducwrot Instrument & D. I certify that me repair and/or anerationjnade to rap in have been made In sccordancerth the requirements tumished herein is true and correct Wine best of my ItnowMge. Iii) identified Marne above and described on the reverse or anachmenu hereto of PIS 43 of its U.S. Federal Aviation Reputations and that me inforinction Dee Jitabsiy 27, 1992 Signature MAuthorized Indivirloal .../....e,...-".41 ' Amen& ler bewn.7. &woo, Pompano the authority sea persons specified below. TM um titled in item 4 was Inspected In the rmnmr prIP0100.1 by pre. ACIMillilltalOf of the Federal Aviation Adsninistration IllIbri : APPROVED 0 REJECTED • i FAA Fit Stewards leepeetor klamtleauter Riga:ration Authorlution Olher(SPNWY) 10 0•119.164 X • - Repair Station. Ftson Approved by Transport CartadaproortlWeal Group r '. Date of Approve) or Rejection 'JAN 2 7 I99/ - Cerfificele or onottu tioa yr... °. Hiosth=€(......... 4 4 FAA Penn 332 male SONY_GM_02754225 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O241147 EFTA01326740 I FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: 3-20-42 NOTICE Weight and balance or opirating limitation changes shell beintoned in Me apprOpriali abate record. An alteration must be compatible with all ruinous alterations to assure continued conlormity with the applicable airworthiness requirements. DmicripliOn el Wort Accomplished (It mote space is required. attach additional shags. Identify with Winn nationality snit registration male and date work completed.) Honeywell Traffic Men and Collision Avoidance System (TCAS II), as previously ' installed with minor deviations to Gulfstream Aerospace provisional Supplemental Type Certificate #5A30335O issued December 6, 1991, has been FAA Approved for placement into service by authority of Gulfstream Aerospace Corporation Sit 0SA3033S0, emended on January 17, 1991 Reference FAA Form 337 dated December 12, 1991, covering the provisional installations. • The TCAS Receiver/Transmitter unit has been installed into its mounting rack, the circuit breaker previously pulled and locked out has been activated and the placard installed adjacent to the TCAS control stating: 'TCAS INOP PENDING STC APPROVAL-has been removed. Gylfstream Aerospace Ground Test Plan/ReponittSC41 129602 for Honeywell (TCAS) Systems has been accomplished to verily the installation and operation of tee systems as installed in this aircraft; test results have been recorded and are on file with this facility. FAA Approved Airplane Flight Manual Supplement, GAC Document ftSC41 129M0Z dated January 14, 1992 and FAA Approved on January 17, 1992, is required for this alteration and has been provided. The effects to the aircraft's basic weight and balance has been calculated to reflect the above mentioned alterations. The aircraft equipment list has been amended to reflect the new or modified equipment installed. The installation as described, 'tuts been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. G Mallon' Sheen itie Attached va a gerfirgr ia % SDNY G0.4_02754n6 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 11 48 EFTA01326741 FAA AIRCRAFT REGISTRY t .11 CAMERA 13 Oa/ • R .DATE: 1 - 24 - 92 . • I 0 MAJOR REPAIR AND ALTERATION us ceormart elaaarerce . (Airframe, Powetplartl, Propeller, or Appliance) Aidnimesten ildemiseem • Fain Approves OMB N027200030 ' FOEFAA Use 0* OfficeAdondfloation .1A7(4)0 0 - -1 INSTRUCTIONS: Print or type ill.I etudes. See FAR43.9. FAR 43 ApoentaA B. and AC 4S9.1 iorsuesememmesiontlamit08 torIntuitions and disposition phis torn. Trim tenon is rernared bylaw Ng %M.O. 1421). Fs lure lo reponcen result In • civil penalty not to exceed $1.000 for each such notation (Section 901 Federal Aviation Mt of a63). I. Allaret Make • • Galfstrem, Amnion IMMO ' G-TV INS Nationality inc Regissazion lash NMIGA -• 2, Owner 1.42". S4 shown on neiartirloncertiticner Mlewin sod Capital Ceres Address (AS shown on regatretiOnartilicaln Toro Embercedmo Cater Sea Francisco, CA 94111 . 3. F.r IAA Doe One/ • 4. Un4I lOwaltIcalkm4 - I Type Unit Usk* • Model SerldNo. Repair Alteration AlAFAAME • • (As Oncelb40 In lam f4above) X .-- V *. pov.-F.apuor . ... • - . PROPELLER .1 .'! - MrelJARCE Type - • • f . . minus._ . •.. ii. CattfornWly Slalegawd A. Annoys N ma and Address 8. 10M 0 Agency i C. Cerr:ficste No. . Western Caamancler, Inc. - t 16300 Nib Drift • Van MOIR CA 914% , us c.,14,:aue wer..4 ' RA3R8MILAistreele 3,4 Sadao r 2 & 3 Melted erat & Peerractefleti Insinu Cotton Gnaws, Mechanic - II—Cethicate n.,44 Via • Manutectie• D. I certify that die repair and/or eiwauon made t6 the uo t(f) IdentifiedInitem I above and described On Me reverse or ameninentspereto neat been matte in accordance with the ilollieftenents of Pert M oi tn. U.S. Fan: Aviation Regulations WO that the IntormetiOn iuMiltiect herein 4 Inn end cane/Ito the test of my nonleclge. ' • Date December 12, 1.991 Signature of Authentic; I I ." - A -7. eamemi lee To lweesta to the authority Inn pentons specified below. tm ani died Nitem 4 will infpnled in the manner prescribed bY the AdlniniltililOt 01 the Primal Aviation Administration and Is APPROVED ID REJECTED FAA Inspector Rt. Sier4wds manufainer . Inspection Aurnoraman ' ate (Smarty) BY FAA (*Knee XIReoair Stelion Person Morey*: by TratiOCel Canada Ainimminess GM* DatewApp,...,...... DEC 1 2 -1991 Dniotoitiesz.. ales Sep Authorized Ir, cO4./._______E, ....e—e.../..., - . • FAA Form 3314ta.set SONY GM_02754227 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 149 EFTA01326742 FAA AIRCRAFT REC,ISTRT CAMERA M0.1 N DATE: - 24 - 92 rylq it y • NOTICE • • Weight and balance or operating IlmitatiOn changes Shall be entered in the appropriate aircraft record. AnalterationMust be compatible with Ill previous alterations to assure continuer/ conformity with the applicable alnvOrthIness rebuke/hell:S. • I. Description of Work ACcomplished (II more Viten rebutted. Mats additional sheet:rides:11y we/takers!: netionehry ens registration mare and thee work completed.) t. This supersedes that portion of FAA Form 337 dated September 7, 1989 regarding Systems, installation Inc. . of Engineering ap auxiliary Report radio rack in this aircraft per Elsinore Aerospace #1,23. Elsinore Aerospace Systems Report #1-23 ieferenceA on the original FAA Form 337 covering:: this installation does not represent the nature of the actual rack that is installed in this aircraft. . . The auxiliary RAI forward radio rack as installed: in this aircraft conforms to Report the configuration 1-52 dated 1/18/89, of that entitled found in Elsinore Aerospace Systems, Inc. Engneering i "SUBSTANTIATiON This report has been FAA approved. - RH FWD AVIONICS RACK". by Robert E. Poteet, FAA Structures DER //NM-494, with FAA Forth 8110-3 dated 12/05/91. The effects to he aircraft's basic weight and balance has no! changed as a result of this correction to the records pertaining the above referenced installation in this aircraft. The installation as described, has been found meet to be in conformity with the above mentioned approved data and continues to the airworthiness criteria under which it was originally certificated. END 0 Additional Shot. An MUCHA • 9/1:2Wt-fitittk4rf P:;9k,IP.-L1:. r --t— soNiietvi:02754228 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 150 EFTA01326743 FAA AIRCRAFT REGISTRY • • 1 CANTU. N0.1 N DATE: 1 - 24 - 9? .• 0 MAJOR REPAIR AND ALTERATION in ceornwen onoscorceo, (Airframe, Powerplant, Propeller, or Appliance) Win Assn Form Approved OAS No. 2120-0030 -. • For FAA Use Only ON ico Idea, legion OP --r$O4O — / INSTRUCTIONS:Print of type allentnes. See FAR 43.9. FAR 43 Appenclie B. end Aq 43.9-I for subsequent revision thereof) lorlintruclIons and elnipOsition of this tom This report is required by law N9U.&C.14213 Fanureto upon an resultin a civil pepeltynottonceed$1.000 for each such violation (Section 901 Federal AvistIon.Act Of N.M. . . I. Aircraft Iteke GuIrstreem Aerospace Modal G-W Serial NQ. • DM Nationalny and Registration Ma* -PaliCA • 2. Owner Name (Al entown an registration omit/can) BA Lamle:sad Capital Com. - Address (As shown on toolstralion cortiticaril) Two Embercedero Crater Sao Francisco, CA 94111 3. For FAA Us* Only 4. Deft IderitIllealon ... S. Type Unit Make Model - BMW No Raper Allsratoon , AIRFRAME . . ' (As daserityrd In item I 400.) X • P0VAIRLANT' PROPELLER ' • • APFINACE Type ' ' . • a t • , te., ManullidluterN • & Cailorinily Statement - - A_ Agency's Name and Address B. Kindof Agency " C. Cenlecate tat.. Wawa temiamoder, Inc. 11.30D Dab Drive Van Nom reA 91406 • US cemnbased mechanic, ' .. RAIRAPIL Airframe 3,1 rotor Corlafrated lichank Rae, 1,2 &3 x Cerielkuee Rini, Station umbid P NM, Woulacium • . • I Instnuntit & sort D. I certify that disrepair anatoraiteration made to the woofs) identified in item 4 aboveand described on Me riveral or anachmenu hereto Mill.0111.1 mad in accordance with the requirements of Pan 43 of the U.S. Federal Aviation fliligyiSSOOS Sad that the inlonnation • . lumished herein islrue and correct to the pat of my nowledge. ' Date , December I.I. 1991 0 .e . Signature of Authodued Ind I 9 • 4 ...C.-. : N 7 Appeal lee To Service Pursuant to the montrity given persons specified below. the uniyidentified in item 4 ins impacted in the 'memf prilted by me Administrator of the Federal Aviation Administration and la e' PROVED 0 REJECTED FAA Fit Standards IrepaCter Manulactures inspected,' AutnOritatien Other (Specify) BY -• FAADemme. X Reedit Station Pawn APOnned by Transport Canada Airworthiness Group °Meer Aeon:welter Repoction DEC 1 2 1991 Certificate orRRML DotignM No. Siguy AuthOsited ty ..."--e--/-e- Ca' r-"0-4--ll-"-t i FAA Fpm 937 Mier e. 0411: I v*C111Thitridaltan t - ::)_. _..-tlecauc-nt Aft . SDNY GM 02754229 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 0 EFFA_00241151 EFTA01326744 lr FAA AIRCRAFT REGISTRY CAMERA NCI./ Al DATE: ; - - NOTICE Weight and balance or operating limitation changes shall be 'Meted kith& apptopriamdrerelt neon'. An aeration must be Compatible wills all previous &ifnations to enure continued conformity with the alnanable eirlsOsthinese requirements. S. Description or Wort Accomplished Ili more spies is nausea attach elthoonal swim Identity with aircraft nationality and twastration mum one data work compiesea.) The following structural modification has been incorporated into this aircraft in accordance with data approved by Schwartz EnWreermg Company • 1. 14per L-Band Phone Antenna Installation - WCI Drawing #08068088 Rev. IR, dated 11/15/91. This drawing has been, FAA approved for installation on this aircraft only by Peter A. Schwartz, FAA Structures DER itSW-586, with FAA Form 8110.3 dated 12/11/91. • The aircraft's basic weight and balance has been revised to reflect thcabove listed modification. The work described, has been found to be in conformity with the above mentioned approved data, and continues to meet the airworthiness criteria under which it was originally certificated. Work order 6719, on file at this agency, coven the above described work. END • - 0 Additional &loon Ara Attached .1 • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241152 EFTA01326745 1, !AA AMUSE RECESSES • CAREW 10a N DATE: I - 24 - 92 • • • :Zs 0 MAJOR REPAIR AND ALTERATION . utoicamarm eamayem, (Airframe, Powerplant, Propeller, or Appliance) - Nam n amen ileiniertakei • RUM No. OMB No. 21204020 • Fee FAA the Only meal Idenahcedon • g —eit-ea l INSTRUCTIONSPrintor type all trade. Se•FAR43.9. FAR CAppendix Rend ACW3.9-1(orewbsecruent revislonthersoBtor instructions and dittIOSItiOn at thiSIOnn. This report Is Noulred by It. (49 U.S.C.1421). Fa lure so reportcan reSult In•chil penalty not tomcod 51.000 for each such violation (Section 931 federal Marion Act 611950). • 1. Alone Make • . • • ColEstntam Aestepeee - Model _Swore' Semi NO tring NetiOneliry and Registration Marl; Ka ri 2. Owner tillThe (As shown on argot/40°n conilican) BA Leasing and Capital Cap.. Ad0nms (As shown on togisootion c•rtincals) Two Fdatensdero Cala' To Prendsco, CA 94121 & For FAA Use Only • , • . 4. Unit kamUlicemon . S. Type Unit Mike . Model . SOS raj Repair Anitansn AIRFRAME . wwwhiwmwwwrwwwwwrww.(As dew bed in gent I shove) X - i FlOviERPLANT PROPOSER • a . • • APPLIANCE Type h..) ManuleCturer • • r" • I Conleetray Stemmed 1r A. Agency* Name and Wren - a Kind of Aden C. Ceti mate Na a lac 16300 Daily Drhe Van Noy& CA PIS • I U s. geminate, Mae RA3RBOBL Airframe A 4 Radio I 2 & 3 Use/Std Instnasent i.4ory Farago CandtesistiMeniaree . 1 Ortilimiel Reps Vaasa umuracturei 6. i canny Mat therepaireml/oraberation made to led unapt) identified in item 4 above and d•Saibed On the reverse orshachments hereto hive been made in aCCOrdanCe with the requirement& Of Part al of the US. Federal Aviation Regulations and that the Inlonnation furnished herein Is true and correct to the best et my knowledge. Dale thkearer 1.2, OK Signature of Authonted ineav 7 r..4 fa T. Apparel for TO Sefeloe , Pursuant to the evthority given persons specified below. Pie unit IdentIfied In dun 4 urn inspected in the minces prescribed ay the Administrator of the swan Aviation AOrnentratalion end le. 0-SPPROYED 0 REJECTED FAA Ft Stand*" Inspector asnuyacuter . Inspection Aulhodzation Other (SpeCdr) BY FAA Designee - X Repair Mewl Person Approved by Transport Canada Airworthiness Gasp MIN of Approvalor Rejection DEC 1 2 1991 te Or 04eIgnatiOn NO. CertinarAS BRSOBL Sig na hOrliedr. ..O--e--<4__ Aut 631 ✓'‘C.www.-4 4 7 FAA roan 337 uteri • SDNY GM 0275;3231 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00241 153 EFTA01326746 LI FAA AIRCRAFT REGISTRY CAMERA 140.1 A' DATE: 7 24 9 NOTICE Weight and balanceor operating limitationChangesShall be entered in theapproprlate aircraft record. An aharation must be compatible with all wet*: alterations to assure continued conformity with the applicable alnvorthiness requirements. Descriplion of Work Accomplished (II mere spot* is reooked. erten additional Skeels. idennly wen tif din nellonaUty and registration mark and date work completed.) The following major Gulfstream Aerospace Aircraft Service Change has been incorporated: . ASC #178 - Instruments (ATA 31) Electronic Checklist - Installation NOTE: An airplane change that makes the electronic check-list incompatible with the required crew procedure in a manner that could be hazardously misleading will require the corresponding change to be made to the checklist or the display to be disabled entirely. This determination is to be made by the operator at the time that such changes are incorporated. e Flight Manual Supplement Number GIV-89-03 Revision C has been inserted int6 the current copy of the Airplane Flight Manual to reflect this change. The effects of this change to the aircraft's basic weight and balance and the aircraft's electrical loading is negligible." Work order 6764, on file at this agency, covers the above described work. END CI Adddponal Sheets Are Attached • - SONY GM_02754. 232 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241154 EFTA01326747 FAA AIRCRAFT\ FICISTILT CAMERA "Or/ $9 .\DATE: / - 24 - 92 0 MAJOR REPAIR AND ALTERATION • InCeormari eitimainacn (Airframe, Powerplant, Propeller, or Appliance) Anieressmosim seinsiesmen • Form App/oved OMS No. 2120.0020 • For FAA Um Only Office MentifieetIen i•Cd-CF1 r INSTRUCTIONS:Print Of type ell ems es See FAR 41g. FAR 43 Appendix LAM AC 42.0-1(Or stresraidenlaraSiOninent00 [Or instruction/ anddisposition of this form. This report is required by leve (49 U.S.C. 1471). Faun) tOMport can result in • civil penalty not to 'acne $1.000 for each such violation (Section 1)01 Federal Aviation Act of 1956). 1. Meath Make Gatrelnam Aerospace Meal G-IV Serial No. Natkrnaety and Regret/aeon Marx 2. Owner Name (As shown on mgairation ceetitt.atil) BA Leasing and Capital Corp. Address (At mown On legestsation ~Wale) ' Two Embroider* Gutter Sao Francisco, CA 94111 3. For FAA Use Only , 4 - 4. Uall lantihcaticia 5. TYPe Unit Make I PAWN I Set Na • Repair Ntetation X AIRFRAME (Ant ;reel' fl It also i t POWERPLANT PROPELLER • APPLIANCE Tyra • Manufacturer • a Coalonolly Slaternme A. Agency" N me and Address B. it ol Agency i C. unmade aci. - Western Commander. Ina U.S Cerin.attos aNc...nc RA3118091 16300 Deily Drhe Feregn Coellece3r< iercPunc Airframe 3,4 Radio I, 2 & 3 Van Noya,CA 91406 A Can:tared Read Sisbon limited Permaxticatsfy i • Nenutacinn• Instrument & 0. I me-Myrna; ton repair and/oralterationmede to Neuritis) Ave been made In +can:Lena wen the requirements furnish:0d herein it IIIMIIICI torrid to the ben of my identified in item 4 an me cierientsw on the r•Wri•Or in•Chments hereto of P n 43 Of Me U.S. Federal redeem Regulations and mat the InformatIon nowledgo. / Data • December 12,1991 Sigraturo of Authorized Individual ....e---- I Mena for To Sen4oe ~yam to the authority give person specified below. the ern{ riddled In item 4 was Infp•CtId in the manner aresalos try cm Aernwtsueior or ins Federal adman Administration and a APPROVED 0 REJECTED • I FAA FIt StanclaRIS Inspector / /AlOuNiCtufte InepeCliOn AtrtNartnbon OINN (StaarTY) By [FAA Designee X Reeler Station Person Approved by Transport Canada Aiwartninela Group Cafe I Approval or Rejection DEC 1 2 1991 Geniiate - a Onignation No. RA3RIIMIL Sigtuthorized eI y1( 0 .......z ta...........4 .-45•14-,de..— FAA Fonn 337 • • • . .* SDNY GM 02754233 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241155 EFTA01326748 FAA AIRCRAFT REGISTRY CkNEtA 110.1 N DATE: 1 - 24 - 92 ■ NOTICE • Weight and balance or operating limitation changes shoot.* entered in the appropriateaircralt record. An latOtatiOn MOSt be compatible with all previous altaratiOnS to assure continued conformity with the applicable airworthiness requirements. DescOomm of WA Mmm, ftlAiW (II More SDK* le required. attach ackfig(nsl shalt Identify wan sacra nationality and retistation mate and ante work completed.) Installation of provisions for a Honeywell Traffic Alert and Collision Avoidance Seiron (TCAS II) has been accomplished in accordance with Gulfstream Aerospa ce ration Supplemental Type Certificate NumberSA3033SO issued on December 6, 991 per Gulfstream Index List. SC 41 129802. Revision C, dated December 4, 1991. Minor electrical wiring deviations to the above referenced STC have been accomplished in accordance with those diagrams listed on FAA Form 8110-3, dated 12/11/91 as approved by John R. Ciambless, FAA DER NM-476, Systems and Equipment Engineer. „ . The TCAS antenna provisions have been installed in accordance with Western Commander, Inc. Installation Drawings #08068090 Rev. IR, dated 11-21.91 (Upper TCAS Antenna Installation), #08068079 Rev. IR, dated 8-28-91 (Lower TCAS Antenna Installation), and #07068179 Rev. IR, dated 7/30/91 (TCAS. Antenna Curvature Adapter [Honeywell]. These drawings have been FAA approved for installation on this aircraft only. by Peter A. Schwartz, FAA Structures DER #SW-586, with FAA Form 8110-3 dated 12/11/91. Software modifications to the following components are reflected by part number changes as listed below and has been accomplished by Honeywell - Avionics Division as approved under the above referenced STC: 3 each SG-884 Spibol Generator. (from P/N 7008570-903 to -904), 2 each DC-884 Display Controller (from P/N 7007540-932 to -942), 2 each FC-880 Fault Warning Computer (from P/N 7007484-904 to -905). As instructed on Engineering Order Cl of Gultstream Aerospace-oCag SC41 129002-01, the TCAS computer has been removed from its mounting rack nd the circuit breaker has been pulled and locked out. A placard, installed alljacent • to the TCAS control states: 'TCAS INO1) PENDING STC APPROVAL". IIII The aircraft's basic weight and balance has been revised to reflect the above listed modifications. The work described, has been found to be in conformity with the above mentioned approved data, and continues to meet the airworthiness criteria under which it was originally certificated. Work order 6719, on file at this agency, covers the above described work. END a Add rt,onsl ShettliAnt A ...waddeadStetask.sk-...'..; "4.4 ' - - SDNY GA4 2754234 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,_0 and 17 EFTA_00241 I 56 EFTA01326749 [ FAA AIRCRAFT REGISTRY __ CAMERA SC.; T DATE: I - 2.: _ 2 4 e tna-i RECEIVED FAi. r : 0 MAJOR REPAIR AND ALTERATION 199 in twoomew DEC 1 6 ortoecenmea ii,14—Y FSDO sanneerawn (Airframe, POwerplard, Propeller, or Applian Asimpensew Form Approved was No. 2120-0020 For FAA Uee Onk °ma idenc.ocri= if -el Of INETRUCTIONS:PrIM or quell entries.See FAR 43.9. FAR4.3 Apbenoia B. and AC432-1 (or suberoptentrevisiow tnereoft kw inelmetione end dispobtion of INS form. TM; report is retwiredby taw pleu.S.C.I42”. F lore to reportcan result Ina civil penalty nO1toexceed $1.000 foe each such violation (Section 901 Worn AviatiOn Act ol1968). I. Aircreft 1. Mate Amapa Mode G-IV - Gaeta*. Saul • No. INS Natenatity ma Registration Mark NMICA 2. Owner Name (As Sheen on regIstraloncerldioalt) BA Leashes and Capital Corp. Address (As Mown on espialawn canines:a) The Embarcadero Comer Sao Francisco, CA %III 3. Val FAA Use Only • 4. wet Mentlaration 6. TYPO Unit Maim Model Serlal No. Repair Afteratkin • AIRFRAME CAS diacAtope In !Hai i arroyo . X . POWERPLANT PROPELLER ,. APPUANCE￾TYPe . Manufacturer • • G. Confomeryitemment B. Kum of Agency Ma Gnats:aim A Aiency4 Name and Address immarm • C. Corarketa NO. Western Commander, loc. 14.100 Daily Drive Yen Nuys, CA 91406 . RARRISMIL Airframe A 4 2 & 3 Fowerplant, dr A a- wl Forum Cemiates Neck em I Radio I, A Cenotrawd Paper Stoma I Limited 1 Instrument sammoum D. I Certify MN the repair and/of Nitration mar* tog» unMeMantrlied in item 4 above andoescalbed ono reverse oratticluents hereto hove bean mar* in accordance with the requirement, of Pan 4301 Me U.S. Federal /Malice Regulations and that the Information furnished non is true and carted to the but of my knowledge. Dale December 12.199E SMnatomid AutheritedAdividuel / . T. Apprenil To Service Pu Administrator scant to VW IllAhCalty given persons specified below. me nft...Identif leo in item 4 was liespecied In the manner prescribed by the of the Federal Aviation Administration and is rAPPROVED 13 REJECTED FMIII.Stendards Inspector manuteesaw la•Penion Mathlti011 derraperayi . BY FAA Designee X Repair Stake " FWDOnAppeOvapd try Tranaparl Canada AI/wordage Warp Detect A DEC Mal or Rejection 1 1991 Certificate Of Deeigne noD_ o. ItAntS08L 77 AutitorlzedCac aa..... l L ...,47 -1---1-1--e- . FAA Pena 331 to -r • •r • • ' SDNY_ d 1/64 nr - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241157 EFTA01326750 FAA AIRCRAFT REGISTRY CAMERA NO./ 'DATE: I - 24 - 92 NOTICE Weight and balance or operating limitation changes shell be entered in the appropriate aincraltrecord An alteration must be compatible with all previous alterations to assure Continued Conformity with the applicable altwOcthilaa3S requirements. Description cot Wont Accomplished rThOIO 3POC4 is require& attach addifetnal sheets. Identify wetly aircraft natranahty aria reqqtraffon nark and dale work completed) This supersedes that portion of FAA Form 337 dated September 7, 1989 regarding installation of a third Honeywell Flight Management System, a third Honeywell Inertial Reference System (IRS) and a Single Honeywell VLF/OMEGA Sensor as previously installed per Western Commander, Inc. (WCI) Supplemental Type Certificate SA3T74NM. Previous installations approved under WCI STC NM3774NM have been modified or upgraded in the following manner: Installation of a third Honeywell Flight Management System has been updated by incorporation of a third FMS computer (modified to Part Number 7004402-976), a Single Honeywell VLF/OMEGA Sensor System has been removed and a Dual Global Positioning System (blended) utilizing Honeywell receiver processors (Part Number HG-2021-AB-02) has been installed. These systems have been installed in accordance with option 6 of WCI sealed Top Drawing 08000004 Revision F dated 5/08/91, as approved on 7/18/91. This installation conforms to pages 7 and 12 of Western Commander, Inc. Configuration Control Document 08006005 Revision B dated 5/03/91 and FAA approved on 7/18/91 under WCI STC SA3774NM. The Airplane Flight Manual SuppleMents that were previously provided for the above listed systems, have been removed and replaced with the following Airplane Flight Manual Supplement Documents (dated July 18, 1991): 08015011 Rev. A (AFIS), and 08015014 Rev. NJC (FMS 3) and 08015015 Rev. N/C (GPS). Minor deviations to the above referenced approved data with regards to the installation of both Global Positioning System-antennas has been accomplished in accordance with Western Commander, Inc. Drawing #08068080 Rev. IR dated 8/27/91. This drawing has been FAA approved by Peter A Schwartz, FAA Structures DER #S W-586, with FAA Form 8110-3 dated 12/11/91. The effects to the aircraft's basic weight and balance has been calculated to reflect the above mentioned alterations. The installation as described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. Work order 6719, on file at this agency, coven the above described work. END Additional Sheen Are Attached _ - ----- *----ipico0:4-tro542a6— SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (10241158 EFTA01326751 FAA AIRCRAFT REGISTRY CAMERA NO.! DATE: 7 - 24 - 92 • • 0 MAJOR REPAIR AND ALTERATION ol nwo'-a, in,,,„, (Airframe, Powerplant, Propeller, or Appliance) maw swam Aerrenonnr Fri, Approved , OtAS No. 2120.0020 Fes FAA Use Only orrice Wenlincadon q•- 0 'On INSTRUCTIONS: Panto. hale all Melee Sat FARalle.FAR43Apperdix Band AC 43.0-1 (Or Sutdefluant renSiOn Mantel lor instructions and disposition Minis loan. This report is required by law (49 U.S.C. Ica Failure to repeal can result In 'aftpenaltynot to tamed 91.000 for each such violation (Section 901 Federal Aviation Act of 1956). it. Aireasit Mate GeffOrSem Aenswece Model GIST Social No. IOU Nationality and Registration Mark NISGA 2. Owner Name (As flown on nonrralon candid. fill BA lasing and Capitol Corp Adams/As shown on ragastrarioncondidala) Two Esobercadere Cates San Fracristo, CA 94I II A Rir FAA Use Only 4. Unit ldwitineadon , S. Tyre .. Unit Slake I Serial No. Paper Alteration AIRFRAME • . (A d bad' If 1500 1 X . • r MIOPIEUER • APPUINCE Type .. Manufacturer - S Cmdcwaili Suilowee r A. NSW* Name and Address Western CommandeerInt B. Kind 01 Aganey C. CartifiCalll No. USCancan. Want J RA3RSOSI. A/drawn A4 16300 Mtly Delve neer dendeated Wealaine • I Radio . 2 er3 Vs. 749S V1406 . A Unclosed Rage Mama I limited Poeferplamta . ( InStrument & Aceasesy D. I candy Mal thermion end/or aeration made to the Wig have Wen made In imainninCe with lira requirements hatnished herein is true and COMO to the but of my $) ideMIfied in item 4 above and demand on the fawn Or attachants hereto of Pan 43 of dm U.S Federal Aviation Regulations and that the iniormation nowledge. Date Deosenber IX 1991 k Signatur f Authortzed Ina • . m - • 7 Arionwei ler P To Seam Pursuant to the authority give persons speeiliffd Delow, the a ' tined In nem a was inspectad in pm manner preaddeed by the Administniter ol the Federal Aviation AdmMistratiog and Is APPROVED 0 REJECTED - TFAA Fit Standards rInspacaor Manufacturer.' - acacia Audwritation. Other (SPOT) BY • FAA Derby** X hpair Sistias • Parson Award by Trowels, Canada Ameenniness Group Ws olApployal orRelection DEC 1 2'1991 Certificate or ' 411tillast. - SignrAuthorized ,Ogiselci , • --ers—e-a— CA! FAA Form 331 irt.ma r• • - : CM)2754-237 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241159 EFTA01326752 1 FAA AIRCRAFT REGISTRY 1./ . CAMERA NO.; Y DATE: 1 - 24 - ;'-' . NOTICE Weig hi and balance or opera ling limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to enure continued conformity with me applicable airworthiness requirements. a. DesaWden or Work AcCerhrilithod (II more Span is reclulfiCC art•ch additional 'Meta Identity with annul natantiCy and ItylVrtriCn frank and date work arnpieted.j Removed existing Collins TDR-90 Mode C Transponder Systeni and Stalled Collins TDR-94D/Mode S Transponder System in accordance with FAA approved Western Commander Installation Top DraWng 08006006 revision A dated January 18, 1991, as listed on Supplemental Type Certificate #SA5044NM as approved on February 6, 1991. Minor deviations to the above referenced a data with re to antenna mounting has been accomplished in a with Western Commander, Inc. Drawings 08068091 revision N/C, dated 11/20/91 (Top ATC #1 antenna), 08068087 revision N/C, dated 11/15/91 (Top ATC #2 antenna), and 08068092 revision N/C, dated 12/02/91 (Bottom ATC #2 antenna). These drawings have been FAA approved by Robert E. Poteet, FAA Structures DER #NM-494, vnth FAA Form 81104 dated 12/95/91. Transponder system ground test requirements of FAR Part 91.411 (a)(b) were accomplished with IFR Ramp Test Set Model ATC-601, in accordance with Appendix F of FAR Part 43; Mode-S testing requirements addressed in FAA Notice N8300.99 including verification of ICAO address code (N8SGA - Octal Code 53016023) were satisfied. Altitude reporting test requirements of FAR Part 91217 (b), were accomplished in accordance with procedures contained in A.C. 43-6A, Para. 8, to 45,000 feet. Pitot static re-connect check requirements per FAR Part 91.411 (a)(1) were accomplished with Barfield PitouStatic Tester Model 181111 162, in accordance with Appendix E of FAR Part 43, Part (a) and was found to be within tolerances•established by FAR Part 25.1325. System operation was found to be satisfactory for return to service. . The effects to the aircraft's basic weight and balance has been calculated to reflect the above mentioned alterations. The installation as described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated, Work order 6719, on file at this agency, covers the above described work. • END O AdditiOnal ShOets Are Attached a Ilk 'ewe • . . e • .. ....wwwaaillbw. rsafeew+trewellibleetha r• ar ..w•rat SDNY_GM_02754238 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 160 EFTA01326753 FAA AIRCRAFT REGISTRY CAMERA NO. I DATE: 1i — — US 00•4411444 Of TRANSPORTATION '• • FEDERAL MIATIOtteADAWESMATION MAJOR REPAIR AND,M.TERATION (Airframe, Powerplant, Propeller, of rene Appered Elettett Reap. Ne.14-660.I FOR PIA WE ONLY teeth IDENTITICADON Zair - et.41)r.., / • INSTRUCTIONS; prim or ope ell mariee See /ALUM 1%R 44 Append... 11, ed./ itc4).Tot Co. oubekomo of•idooMeTeeo0 for knouniono sod dispoopion of this form. I . MUM 0.1.40 I MODEL • • GulEst • ream Aerospace GIV ...• SOUL NO. ' 5 ]NATIONALITY AND 403403411014 MARX 1085 . ..0" . USA W886A-- • 7. °WM NAME (Ai Mon on fopiskertiss evelifp*Al • •I ADDRESS fAi Jan so ontendon ceneteste) BA Leasing and Capital Corp. . o ISan. Francisco, CACenter 94111 • . 3. Ied MA USE ONLY , t 7--- .--'''. CFA 1000. A O , .- / ... c S •Pj. 0 ebe, 4. WI I nuncio - vv. scfril ... ..... "Obit I Mat. NO. • Am MM. Amp. AIRFRAME . M. *woof/ as he; I Mom) POW/IIPLM0 • PROntta ee APRIANCI NH .• • • mmourecroome • E. ullfawn STOW: A. sowers NANO AND ADDRESS I. RIND Or AGENCY C Ca MCAT NO. Western Commander, Inc. 16300 Daily Drive 'Van' Nuys, CA 91406 trd tiltinCATIO edoutmee RA3R808L • Airframe f 3, 4 2, 4 3 11mi ted Powerpla 1 Instr. 4 acceSs. POSISt Wils•Cittf• .6101•ssc x Clinine.ATIO Mail ST410•4 aturyPACWOU • D. I Only due the wale end/or al ttttt iota nude to ai valets] identified ho hem 4 above tad described oa the imam oa' oeuthatoti mid Immo ben been made la sccepdatme ith ,be requiemoonto of Pan 43 of the-US; Metal A t i tt ion Reeeladoet tbs. ibe leformetio• hnliatsfil lop* as Mt • el count to Me hen of my knorlpdpe. . • DATE • .. AUG 2 1 1991 • SIGNATURE Of AUTHOR 1NDMDUAL C__ . 7. AMNIA'. TM MINN TO SEIM Ammo. is Ilw embodier give proem spetified below as unit Se ded io hem 4 no iri ted Jo the mane peneribed by ike Adminiontor of the Peden Atiedoo *dna& ttttt km lad is Ey APPROVED REJECTED sr NA AT. ItmeaerN cannel sweippeepte . MEN omeeCtiemancouanor4 flmostl Ma 011.0141 x ItMili MOON .. alOtaui. NSW OP MieteCill BOOKTOt OM CO siOCull Or APPROVAL 04 REACTION 8/21/91 ... - -..- IRTICICATE 04 INSIGN4TION NO g438808L SIG OP AUTNORIZED INONIDUAL ....4-4C-1.-t 0 at/e-t-tn.--( . own in V-6 rt . ' . • SDNY _ GM _ 027542§r SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241161 EFTA01326754 . . NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. identify with aircraftbationalfty and registration mark and date work completed.) • The items listed were installed in accordance with Gulfstream Aerospace Report 11159C-GER-023, Revision 12, dated•November 14; 1988 and the following- reports as listed in Consulting Aerospate Engineers, • Inc. and Arora Associates roports approved by DER NM-442 and DER NH-1362. The following major components installed per the reports and specifications as listed: . 1. Service Ladder -Installation 2. Service Tow Bar. Installation CAE AIN-GIV-10 AA 103-8 Aircrieit Weight and Balance corrections computated and_Equipment List revised. All workmanship accomplished according to A.C. 43-13-1A., Zhapter 2, Section 3. C) ADDITIONAL' SHE ETS ARC ATTPCICO •V.; OOVCPN,ILNT paisTiricoeneCTINIGN.WIWZO SDNY_GM_02754240 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241162 EFTA01326755 [ I 1C!E: DATEL/) - f .- (7/ IARTFli REGISTRY i • . ioc. AAAAA ENT ma. AAAAAA Contemn . SFDESAL AVIATION ADWINVID•TION - • STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Dec. 12, 1989 AIRCRAFT OR-AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream NODE% HO. a G —IV TYPE cbirpione. Rae.. lielleitlet. el.4 Airp.lane ilAaint Di APPLICANT . REX , INTERIORS, INC. LIST OF DATA - itittlITAICATIOti TITLE Report: AIN - GIV (Section 1 thru 15 covered by Rev. K) "Structural Substantiation Of Various Interior Modifications That Are To All G -IV Aircraft' STRUCTURAL APPROVAL ONLY Cabin Applicable Interior verify ' 3.0 and 5.0) inspection fabrication per ( I ..". only the data The installation of an FAA 1. . This approval requires that Aero • that the footman (Item - 2 Section is a forged or machined part. 2: Approval -is -subject to Aero Interiors of installation and components sketches in report AIN - G - IV. 3. This. approval is applicable to contained in report AIN - GIV. of all items requires the approval inspector. .." PURPOSE Of DATA To structurally substantiate installatign of 2 ' components in a Gulfstream G - IV. • APPLICALL IL REQUIREMENT/ (LIP opeetateeeneno • st FAR 25 Subparts C a D • -CERTIFICATION - Unlace authority or appointment under Peet IBS NONE • I. by direction el the Adisisist AAAAA mad la accerdaece with cent 'oar ad limitation # al the Federal bristles Repletion. dais listed above and ea attached • tuts namberd v ban numbed Is &teatime with established procedures ad land a coply with applicable artistica Reguleticss. \ • amoral al am data these data requirements el the Federal 0 11de/weal I (K) Therefore Amen SICHATUR (SI OF DESIGNATED tiCII/EE IIIG REry45ENTATNTOT DESIGNATION NUUBERNE) CLASSISICATIONITT >9_-- .--ua A-- --..--. DER NM 442 Structures Michael Kappa n FAA hum 8 110.3 II km SUPERSEDES PREVIOUS EDITION ..•. c￾SDNY GM_02754241 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241163 EFTA01326756 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: .. UArTARATIJET 0cIPLUISTImitlION \ µ N STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS OATC 16 AUGUST 1991 • AIRCRAFT OR AIRCRAFT COMPONENT IDENT:FICATION NAAR pus STREAM 'AMERICAN ' YODEL NO. GIY Tyra (floptalt. III.I.. 14•Ittopen, Adam MARC Or APPLICANT \ • AFRO INTERIORS - N. .../ LIST OF DATA' COEN TIFICATION • nit( AA REPORT N0.103 SECT. 8.0 • - TOW BAR INSTALLATION r \ ' • . • ‘ . I •-••••••A• • ,... • . • . PURPOSE Or DATA TO STRUCTURALLY SUBSTANTIATE THE ABOVE MENTICNED INSTALLATION MD ITS SUPPORT STRUCTORE APPLICARL E. SICOUI U. stmts. nat.') . . 4 FAR 25.301 .307 .601 • r • .303 .333 • • .305 ' .561 :605 - .607 AND .609 CERTIFICATION • UnDa nitwit; vested by tirtailea •I she Male loins., sod In accaldauct wish coadhieits sod limO•lioas al apialaaaeot oh, Pea III of Ai TeIled A•Istlaa Replallna, Ism Woe.' above sad as •N•chtI Ansa a•mbra —. N/A._ i's• 6 al. d In cc I • wish I III had penedarea Oa' land to dearly midi opplitable mutts...we • die Edepal ldi U» Theca lei Awimian Ilrillalloaa. Racemes.' oppyanl el slim dale . . Appian thile 4••• UCHATURIWO DErby4TEDENGuiEtaINO DEPRESOITAINEM DESIGNATION NUMBERSIII i k Cies • • jad-1362 ELASSIFICATIONI0 STRUCTURES ATISH K ARCIRA • • FAA Form 1110• 3 °net Fv•cattets PRLVIOUS EDITION SDNY GM 02754242 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241164 EFTA01326757 I FAA AIRCRAFT REGISTRY CAMERA NO. I DATE: I i — 4- - 91 i MAJOR REPAIR AND ALTERATION S ascot.* a Isnanown (Airframe, Powerplant, Propeller, or Appliance) it an Anamen minivenusko FOrm POINOved OMB No. 2120-(KQO For MR Use 0* Office Ideinilleadon - 4.1/'-00 INSTRUCTIONS: PrIM or type all Oman. See FAA 419. FAR43 Apperna 8.and AC4314-1 (or sunachoem revision then.° f oF intruedOne and disposition of this forrn.This report is required by law (49U.S.C. 1421). Failure to report can multi idyll wally not to exceed 51.900 tor each such violation (Section 901 Faders! Aviation Act of 1965). t . Make GULFSTREAM AEROSPACE CORP. Model G —IV Serial No. 1085 Nationality and ROgisIrM0.1 Mark - ' NEISGA 2. Dame Name (As shOwn onregIatinorminifleale) BA LEASING & CAPITAL CORP Acldeen (Az shown on regmfration mint ICAM) TWO EMBARCADERO CENTER SAN FRANCISCO, CA. 94111 3. For FAA Use Only￾i 4. UM Menem e. Type Unit Make I Model • EMS No. Ann Minion MIFRAME • . (Al CleICAOH A Rem I Mom/ JOC PO ERPLANT • PROPELLER APPLIANCE Type Melnulanrnra, 6. Conlonnay Staten* A. Agency's Nan* and Address 8. Kind of Agency C. Genie* No. LANCE. A. MATTESON 8560 E. -SAN FELIPE DRIVE SCOTTSDALE, AZ. 85258 K I us. gefbecated Mathew AP. 1864049 . Foracon Canicataci Macrae CeniricaMe Palma SO n Menpranger 0. 'witty IP.MI the repair and/Or alteration made 10 theynol(S)identiled in item 4 above rd deecnbadOnlhe mein ornaeMnents hereto have been macto in accordance wan the requirements of Pan 43 of me U.S. Federal Aviation RegulatiOne and that the inkirmetion ' hanistmo herein is true and Correa le the nal of my novriodge. Date r - S : 7( Sign a o ed In* 41 --- • 6- 7. Approval nor Ratan TO &less Supt. of Maintenance Pursuant moninistretor ay to the authority given persons specifier: Mow. the unit identified in item 4 was inspected in the manner prescribed by the DI the Federal Ay 'von Aornaustration and es v li APPROVED 0 REJECTED If AA Ft "annuls I nspacter manufacturer )D(iinwcionminonya iee - Other ISM*/ • • • FA,. Designee Repair Slat* Person ApprOwIdts TrinatiOn Canada Aint011eindaS OfOuP Oate of Approval or Reinhart 5 - 6 - 1/ Genital, or Signature of 'un su Ind, Dessmairon No. 526705494 „.... . t FAA F0fIll 337 .+7 B/5/91 7:33 PM 1085FACE.WPS Michael Donnelly_ _ _ • " - • SONY 0M32754243 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241165 EFTA01326758 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: — ••• NOTICE ‘" • hewn andbsianceoroperasinp limitation changes shall be twisted in the appropriate aircraft record. An auarationmust De compatible with all previous alterations to assure continued conformity with the applicable airworthiness mower:wed S. °meow) of Won Ancoffelignea (I' more epee is Winne. attach atkIttIOnal Meets Identity ATM ithwati nothanality liner/POWS:ion meth 500 date work comordedj 8/5/91 7:24 PM ilUlfstream Aerospace Corp. (GAG) Model 0-IV, Serial No. 1085, NBBGA, Aircraft Type Certificate Data Sheet Al2EA. FAA APPROVED DATA: GAC Recommended Air.:raft Service Change (AEC) 134, Subject: FUEL (ATA 28) FUEL BOOST PUMP CONTROL-MODIFICATION, dated April 28. 1991; and CAC ASC 134 mendaent 1, dated June 1991. The purpose of this alteration lstto add a 500 millisecond turn on time delay relay to each of the Wag fuel boost pump control circuits. The time delay relays (2 each), located in the fiel pump control junction box (Right Main Landing Gear Wheel Well), will prevent boost pump failures that can occur, during electrical bus transfers (power interruptions). Installed the parts of ASC-134 kit in accordance with the instructions contained in' the above referred to ASC and Amendment 1, except, instead of using a CAS805A4 splices (see instructions Figure 3, Page 8, triangle 2) installed a new Deutsch p/n DI-el-IA-02, plastic rail Terminal Junction (354A1TJ1) forward of relay 354A1K1 and installed two each new Deutsch p/n CTJ120E018 terminal Junction block* in the rail at position "K" & "L". Prepared the following wires for installation into the newly installed 354A1T.11 assembly by striping the insulation from the wire, crimp installing a new Deutsch CTS 520/20 contact onto each properly prepared wire with.a M22520/7-0i basic cool and M22520/7-,12 Xisliioner and inserting each wire/contact assembly as follows: (sire Figure J, age fs of the above referred to ASC for details) Wire No. 209000A20 to TJ1L-A: 209000820 to TJ1L-13: 059H2O to TJ1L-C: 1090005)20 to 131K-A; 109000820 to TJIK-8: and 06'H2O to Ij1K-C. Removed the existing 354A1 CM, CR2, CR3, and CR4; p/n 1N4006 diodes. Installed a new Motorola p/n 1NO/84A iransorb transient spike suppressor in place of the diodes that were removed across each relay (354A1K1, K2, K3, & K4). Torqued and torque striped all 144 inch stud nuts to 25 inch pounds and all 6/32 stud nuts to 8 inch pounds. All added parts and equipment were purchased new for this installation and meet the requirements of the applicable parts of FAR 21.303 (b)(1)(2)(3)or(41- Successfully performed the operational check out of the ASC-134's :.nstructions and the toaputerlmed Maintenance Program's Fuel Boost Pump Auto-change operational test. Measured each boost lumps current draw ((without any engines running) tc be 32 amps 2 amps. Verified that the correct pump operated with respect to tte cockpit switch selection and bOost pump circuit breaker function. No changes were made to the aircraft's flight manual, inspection schedule. electrical load analysis, or continued airworhtiness inspection program as a result of this alteration. , • Recorded compliance with this FAA fora 337 in the aircraft's maintenance records. It has been determined that the interrelationship—between this change and.any previously Approved configuration will not introduce any adverse effect upon the 'airworthiness of the aircraft. .This determination includes, but is not limited to, consideration that all normal. essential, and back-up systems will be able to function as they were intended and there wore no unique installations that might interface with this notification or•require deviations, to this ASC that change the priginel intent of the FM APPROVED design change. -7he effect upon the aircraft's .electrical load analysis and weight and balance were negligible and no changes were made to either report as 3 result of this alteration. END OF THIS SHEET NO.ADDITIONAL SHEETS ARE ATTACHED 6,5/91 7:24 N'ASC13..W.S Michael Donnelly O Additoonel Sheen Ate AllaCeed • • sySOP0s .0443, 7i SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 SEMGA402754244 EFTA ()0241166 EFTA01326759 FAA AIRCRAFT CAMERA NO. 3 V DATE: 9 - 20 - 91 • 45. t il/ u • . 1.. . • MAJOR REPAIR AND ALTERATION • • — a icrapbow, z. (Aireranii, Powerplant; Propillet, or Appliance) • . .. .. . . , . . .... .. mmeassem Form Approved OMR No. 2120-0020 For-FAA Use 0.ly Oita Identification " „COL _ las o a .INSTRUCTION& Pant or typeolantries.SaFAR 41.9, FAR 43Appendia EL isMAC 4.31-1 (or subsemrentrension thereof) forinstnalons ' and disposal:in Of this town. Tile MOW II nejtared bylaw (49U.S.C.1421).Faibure tO report can mein a mei penany not to mood S1,000 for each such notation (Section %l Federal muerte Act ol IOW. 1. Alma Mein ' GOLPSTREAM AEROSPACE CORP. model C' IV Serial No. 1085 Naumann, end Regisusnon Mark NSBGA Nom (As shown on minion CanACalle) ' • - BA LEASING & CAPITAL CORP. Address (AS 'hewn On rinaistnainn Candidata') TWO EMBARCADERO CENTER SAN FRANCISCO CA. 94111 , t Foe FAA Use Only • 4. Unit Idesnacellos S. Type Um . - ' Make . . Sinai N. ROOM AhMatiOn (AS ADSCIfen l' nem 1 &bra) XX AMFIIAYE . POWMANT -• PROPELLER ; ! , APPLIANCE Type Nana/Mum S. Conaway Statement A. Amnty's Nemo and MOM . B. Tind Of AgeinCy C. Castilian No. LANCE A. MATTESON 8560 E. SAN FELIPE DR. SCOTTSDALE, AZ. 85258 X ',flatmate Wawa< AP 1864049 Fonogn Gantt-nee nonninc cereutadeecor stow. istmanum D. I anginal 'nemesis and/or alteration made tO the on t(s) identified in dent a above end described on me felts* or lalaChmentS lieral0 have been made in accordance with the recarements of Pon 43 of the U.S. MOWN Aviation Regulations anti UM Mil iniOrmation Unread herein is um me COMM to the bet of my nowledge. Date 2 — 7 siffrata al In026.3zz. 6-- , . 7 acenival tor Mtn To Senna SUDE.' or Maintenance Pursuant to Me *Linen'," given Parma specified below. ON unit identified in item I was inspected In the manner prescribed by the AdminilleMOT o4 In. Fnecal Aviation Administratam and a CS APPROVED 0 REJECTED FAA FA Stamens steno. Manulanuist X Inspection AtahoniatiM °the (soon BY MA Designee Repau Steen — Person Approved Of transport Canada AMmeedenel$ Gawp . Daniel Approval or Rejaclen • 9 -2-1 r Connate or C.,.SIg?"1541. .."' 11 ' . 526/05494 Simmons of Au • • • MOM An• . joaet . . FAA Form SS7 nral • MlChaa - - sbNy-_-Gm:.27.2,3 — SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241167 EFTA01326760 NOCE Weight and balance0r Oiniaring !imitation chamy« Wal be antereil in the approphate ihrcratt record. An alteration musi be cOrnpatiblai willi alt prOvious atterallOna lotno," cOnhnued conlOhnity with the apphCabl• ainvolthinm requaaments. DInialpOon ol Wodz Accomplighed more ‚pace h ‚nawal altach «Wadiami anta lewady wrn Wiwat national« and nwittrat(on mrAalus dwa inwit [On‚5444.) TaMat 2, 1931. Gulfstteaa rearscre Cap. gr) ttch1 G-TV, wh 11:05, Ainatt Pipa OecHfimt6 ties Swat 4121i4- Peter to: FM KM 8110-3, Etaet af Caspharte vith 7tviatirn Itsulatzlens, dated 4-6-93, fcr ~sen G-13 A1cpUper C7C, vat i lata - lattificearn - dravirg 11933013039 MIA:1~ 4-6-93, effittuthe far sima 10M - tatlal AIG SilitcER mær arcm-ion rinna-rn •BP MØG. 213 ~sina Sa Gr HP3312 catat'al an ta fonen; ~nis: SE33-145 Rw G. thiffler ~0752-4 ED TA Malet Tastallatan - 1~011-15 Itv B E. Cl arie Ilte • 119rZ1419-119 lem s N2 Tateastrr Coaling tstallaticn papuge af tids alteraticn is to 1r:stall de @C Pmart Mamaer Rwym (lom) ~-1 NU Altecretcr maling Maidficatirn. Proed t7e edstirg FRTS EM/fric Mi 432C6-9 laver AsartLy, attaChing terSare, ad tle CC phi 11.3*21419-73, Par. NI (date aie r) pni, D= S NU stase. h:stalle:d a rew Gle Wn 1159321419-93 grel (MO altan !Sid sial) uslrg M320315-449 ~5-414 ri:~ as datailed m de ~e rareacd tu inarp fcr altainatcr (talrig TrataLlatiat • Sali Us edsting NU tall pips, atachin7 hadere, ard tle AFU 5x;e Valve ~Uting ta fa= tie aircraft. Irstalled a rew GIC pin 1~1633-147 ER7 tai pipa silens cr raffler), attaching huds= ad gz tria, as «afled cn s aloe ~d to darli:prr far Mina M:~ Inataliaacn, ard Saw 31.te. Ractired Ue irstalaticn af tle edsting 3307 9ainless 9:æ1 (.010) lulaldrg platgi ?samar fa- tle phi 3703313-101 Zlme amator (we FM Ram 337 far thi: aircast cts(ad 12-77-133). 411 parts det rate iretaLlecl as a result cf chrwcp ~ nar at de the cd hatallatirn ad fu:nist:Ed bi ae with tre 13993-1 Flt. 9icsacd tle ART car ertaent ad radaral a =Se cpaaticrel test of tle MC uting treirccaltrcs inni in ltds aiza aft's EM MIT OM Airccalt niria Maral ad roed tresl gratla befale, dring, cr atter tie tast. - Fa:turne tle aiccraft to fligt status, recackd omplIate wab tids EM faza 337 ani FIEP33-1 in tle ahcatft s maintererce rads. It tes real te rap tiet tre intecrelaticrehip brun tids Saft ad arylxavicus~Ad anfigraticn ell not inizoduce av aha= affat uan de aincrthiare cf de ~saft. %his chteaciratirn irclaried, tut es na lanital to, cassiddratia: tret da dage to de essigt re tle AK3 omar aut ad axEscray cmlirg arargreact visl nut alitu iks igatticn anto Wla arms cf tle ahcraft; ad all installed arberiaLs ad parts tave ban na TER aigocual far iratallatiat m Ss aitait. lt4t rhr9cs leve ban mad in tle aircaft's lada ad Wam krat. •••••••••••••im rims stEttmnntIO =S REATLICEED".******103-02-9142aPnen****i~ C Additenal Shoels ATS SDNY_CM_02754246 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241168 EFTA01326761 FAA AI R)3. 17. REGISTRY .7 CA2TR. A ? ... DATE: 9 - 20 - ‘,1; 1 , Ir e Ofttoonert dcoy:nom mow mien MAJOR REPAIR AND ALTERATION .. (Airframe, Poweiplarn, Propeller, or Appliance) Fix", Aeferfred OMB No. 212O-0020 For FAA Use Only', ject Office Montauban . 14/P - r ? INSTRUCTIONS: Prim or type all traria See FAR CS. FAR ALTAppendix El.andACC-9d (or subeeetsent revision thereof) fOr InStrUCtiOne and disposition of ens lOnli. This report it required by der (49 u.S.C. 1421). Failure io wagon can sun i acerb perialtynol 10 Meese $1.000 for oWt such violation (Section 901 Federal Aviation Act of 1358). • 1. must • Mete .GOLFSTREAM AEROSPACE CORP. Mcelili G -IV stew Na 1085 Nationably and flagistralica Mark N88GA • 2. Owner / Nett* (As shown on reottronion conitic41O BA LEASING & CAPITAL CORP. • Address (At shown On toystratiOn COnsfiCON) TWO EMBARCADERO CENTER SAN FRANCISCO CA. 94111 ___ . . 3. For FAA Use Only - a. Us liarntibrellon 6. Type Unit Make Model I Sera No. Repair Alteration AIRFRAME bas dncriWd in nem i aeon/ xx POWEAPLANT I PROPELLER . I -• APPLIANCE Type I MandlEtuter . [Cantonal" Slelemild A agency:5 Name and Address . ie. Rind of Agency C. Certificate No. LANCE A. MATTESON 8650 E. SAN FELIPE DR. SCOTTSDALE, AZ. 85258' 4 I u 9 Greece** Moctone AP 1864049 Foredo Cendfc.""Mtnanc Combats PleM40 &Mai . lainninCliotel 0. I certify Mel the teplet and/Ot enetavon made Wine un t(s)identified in !tern 4 aeon end descnbed on Me reverse or attachments hereto hive been roads m accordance with me requideants of Pen U of IR, US. FINPRN kneten R•OullIbOns and MN the intOttniliOn . hammed hereon it true anti correct to the WM Cil My nowlegge. Data 04/20/91 Signature ea Incline . Cr r T tAmmwsimmoumuswAm upt. of matntenance . Pureuent to vie Nononty invert atfICIIS SINCelled below. Administrator of the Fedeal Motion Admaitstralaon Ineynat identified in ROT 4 44ss inspected in me manner Ormented by the 41 APPROVED 0 REJECTED son If IlitSpectcr FAA Ft Standards . illanvIedurar Inspectein'Authonzetion Ogler (Spot) • . BY I IFAA0mignint Rap.' Stston Person Approved en Transport Canada AnorTnicreas Group Oale of Annecy.' or Partneri Certificate Or - q— 2 1 ''. 9/. . DescneltOn No. 26705494 Signature CI Aul I -.. FAA Fem. 337.•. M c ae o ell" 1 """!/...141,tt'e llraeldsit irlI ff eeWmr.•••_-nerearinalk;Sfew..- _ • SDNY G0.4_027S4247 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0(1241169 EFTA01326762 F AA AIRDFAE7 IvIS • CA1n7-4 AO. ; DATE: 9 - 0 - 9I NOTICE Weight and balanceOr operating limitationchanges shall be entered in the appropriate aircraft record. An alteratiOn must be compatible with all previous alterations to enure continued contestant,. with the aPpirtable airworthiness requirements. e. DirspiptiOn 01 Wen ACCIMINIOSSII tit mote space Is requited. Vlach additiOtIO sheets. Weedy with aircraft nationality and reartUationnsart end dale wore cciartiertia I April 20, 1991. Gulfstream Aerospace Corp. Model G-IV, s/n 1085, N88GA, Aircraft Type Certificate Data Sheet Al2EA. Refer to: PAA APPROVED Gulfatrean Aerospace Corp. (GAO) MANDATORY Aircraft Service Change (ASC) No. 186 subject: COMMUNICATIONS (ATA 23) COCKPIT VOICE RECORDER/AUDIO - IMPROVEMENTS, dated January 17, 1991. This alteration modifies the cockpit voice recorder system to comply with the requirements -of PAR 91.609 (d)(e) and PAR 25.1457. This installation adds an underwater locating beacon, provides required audio recording of the cockpit flight crew and ensures that the system is powered from the most reliable electrical bus. The change also revises the audible tone generator and audio control panels to the latest production configuration. Complied with Part One and Part Tvo of ASC 186 referred to above. The Fairchfld Model 93-A100-10 Cockpit Voice Recorder, sin 53674, DOM 8/88 vas modified to a Model 93-A100-30 (underwater locating beacon and reflective tape) by The Jet Center Van Nuys, Ca. 91406; the Baker Electronics, Inc. Model M1045-F284-RGH3 (Pilot's) Audio Control System, sin 8608104, vas modified to a Model M1045-F330-HG83, Mod 11 by Baker Electronics, Sarasota, Fl 34234; the Baker Electronics, Inc. Model M1045-F284-HGH3 (Co-Pilot's) Audio Control System, c/n 881067, vas modified to a Model M1045-F330-MGH3, Mod 11 Status, by Baker Electronics, Sarasota, Fl 34234. All parts that were installed as a result of this change were new at the time of installation and furnished with the ASC 186 kit. Successfully performed the ASC's operational test. Returned the aircraft to flight statue, recorded compliance with this FAA form 337 and ASC in the aircraft's maintenance records, returned completed compliance card to GAC. It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination included, but vas not limited to, consideration that the changes to the aircraft's electrical system (Electrical Load Analysis) would not jeopardize service to essential or emergency loads. The effect upon the electrical load analysis vas a decrease of 20VA to the ESSENTIAL 115 VAC PHASE C electrical bus and a increase of 20VA'to the ESSENTIAL 115 VAC PHASE A electrical bud. The effect of this change on.the.aircraft's basic weight and balance report vas negligible. END C AddtliOntal Shirts Aie Altached 1 SDNY_GM_02754248 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241170 EFTA01326763 _rAMERA DATE: 7.- 24- 92 FAA AIRCRAFT REGISTRY _ _ _ SDNYCM3275;i2;19 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241171 EFTA01326764 a FAX AIRCRAFT REGISTRY CAMERA NO. j DATE: 6 - 9/ 4 MAJOR REPAIR AND ALTERATION vs Ceceeen a Parcomen (Akira, Powerplant, Propeller, or Appliance) wan ins swiss Form Approved 01.40 No.2120-0320 For FAA Ufa OS Enke Mentilicebdo SD/— n P 0 INSTRUCTIONS:Primo/ type all entriee.See FAR 4391FAITIDAPtentlia B.and AC 4.1.94 (ot subsequent tension thereon lot instruction* - yd disposition of Ws lorm.This Mean is reavired bY lee M9D.D.C. TIDD•FailudelOMPri on "Wait M a lifal lidnallY not to nce.211"° Tor each we 'Anibal (Silakin 901 Foetal Amnon Ara O11161). ma I. sa Mak* GOLFSTREAM AEROSPACE CORP. Model G —IV Sent No. 1085 MMionality and ReWaration wart NBBGA 2. Ownor HUMP /At shown On rearttrittgli cartillcata 1 - BA LEASING E. CAPITAL CORP • Adtrass (As Mown OA nigisfranon clittifiattal TWO EMBARCADERO CENTER SAN FRANCISCO CA. 94111 1 For FAA Use Oat, ' • ..-rt 4. thelldentdlaillon . IL T. Unit I Make Model I . Sertal No. Repair Memnon AIRFRAME , :Assn XX pep i 0000•1 POWERPLANT • — PROPELLER I I APPMANCE Type I I Mantdattwes 1 - IL CoMensilly Stnemeed A MARCO Mama and Address B. Kind el Agency I C. Candidata No. LANCE A.• MATTESON 8650 E. SAN FELIPE DR. SCOTTSDALE, AZ. 85258 H= I Vs Certaninee mecitanc • - AP 1864049 . se.•444erb, cmeassecron4 I Gambes saw Simon . m,m,,,,,, _..• 0 I caddy mat Inc mow anclhar weapon maw toter ;initial idient.l.ed in ill/MdlibOweaft4OffaMMI nave wen rninW in accordance won ter requirements of Past 43 of ter US. hon.:Ned Perron d We and anent to me best 0 my knowing* Federal Amnon Reputation, on me reverse or ausenmonu mitt° and mat tne mtormatan Dale . 4.4-",.E /-.• 9/ . 6 Sigma I i - 7. Antonl PM Return re Samoa SUDS.. OE Heinienance . govin: molt* awnonly Enna persons specified below me ond CV% no m rum 4 was emporia' In per manner PreMnbed by dl' A041%mentMOI 01 the Federal Aviation Aornmrstration Ina es p APPROVED C REJECTED Manutsclune Inmecben Aumontalitin ' • X Other (Speedy? I I I 1 I I rnAA FitioSflanoatos • By 6 I (FAA Elsugnee I IRE.' Slit." . JCanadafteeonieness Good I I Person APProveo by Tranwort Oars on Approval or Repecoon i pos Cangilcanltione orNI. Li — n - 1 / .526705494 . 6"amide of Autnbrtati In ideal FAA Form 317 •-• • Michel onnel y r SON YIGN1_027 54255 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241172 EFTA01326765 FAA AIRCRAFT REGISTRY - CAMERA NO I DATE: 6 - - 9/ NOTICE • • Weight and balance d operating/omit al rOn changes shall be enfOrechn the aPPt0Pliste reSorchAn slinatiOn mustbe compatible with all previous alterations to assure Cant:hued conformity with the applicable airworthiness requiternetnft a. Oncripbon of Were Meese/dashed (It more niece l meowed. attecnadOWsOnal 'Pinta Idenuly wen secret narwnuuy and registration slant and late wet* cOMPOWWS1 April Aircraft 21, Type 1991. Certificate Gulfstream Data Aerospace Corp. Model G-IV, s/n 1085, N88GA, Sheet Al2EA. Aircraft Refer to: Service FAA APPROVED Change Gulfstream Aerospace Corp. (OAC) RECOMMENDED (ASC) No. 198 subject: AIR CONDITIONING (ATA 21) November ACM (AIR CYCLE 19, 1990. MACHINE) BYPASS SHUTOFF VALVE - ACTIVATION, dated °COOLING This alteration TURBINE modifies HOT' message the air conditioning system to prevent the on the °FICAS (Engine Instruments and Crew feet Alerting and System) wing or covl from anti annunciating when the aircraft is below 42,000 -ice is selected.- - added to ensure the air cycle Additional circuitry is the aircraft is below 42,000 machine bypass shutoff valve opens when feet and wing or cowl anti-ice is selected. Complied In addition, with provided installation positive instruction of ASC 198 referred to above. to attach the relay rail to locking to the 8 screws that are required the tail junction box (see figure 1). All parts that_xere installed as a result of.this change were new at the purchased time of insta frOm — . lation Gulfstream and furnished with the ASC 198 kit that vas (b) (2)(4) . Aerospace Corp. or comply with FAR 21.303' • • Successfully performed the ASC's installation checkout test. FAA Returned form 337 the and aircraft ASC 198 to in flight the status, recorded compliance with this aircraft's maintenance records, returned completed compliance card to GAC. It has been determined that the interrelationship and any previously approved between this change configuration wilt not introduce any adverse effect upon the.airvorthiness included, but vas of the aircraft. This determination not limited to, consideration that the alteration vas done in a manner that will not.intecfere with or adverstly affect the safe operation of the aircraft. - • The effect upon the electrical load analysis was- nebligible. report The effect was negligible. of this change on tBeaireraft's basic weight and balance • • END_ ts- st-114Fgaa"?. ite•Z:2?-444;a1" 17 SDNY_Gm_o27t42t1 • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF-EA_00241173 EFTA01326766 oteistc'- ‘" 4•Rer! ' 7 7 - •-• :len"?' - Br • IAA, AIRCRAFT REGISTRY tAmm O. RAM 3t.7-'9/ REGEIVE6 FAA O 5 En t MAJOR REPAIR AND ALTERATION FEBFED 0 • , Ohara , cif irneerewn ' (Airframe, Priererplanl. Propeller, or AppliarVny F-• no at, Nemeerwee• assammin - - rn Aere.v" . 0148 NO. 312C4020 . w--- Cot FAA Um Onte • Office Idenuedation li P.C.,. .-1 WaTuLY-7.:4113:PrInt or Typeset/mimeEa FAR 4.3.9. FARO Appendix S. and and heteptien Muir law Thl tan Is required by law (49U.S.C.1121). F :or each such vielilien (Salton 901 Federal Aviation Act e119519 AC 43.1-1 aura tOrnortoannsult IMMO • 4.-IV tersigmeguent revision owreel) ferinstructIons in a cMI penany eaglet:led • . \--- $1.003 . L Aircraft Maim GULFSTREAAIAEROSPACE ' ' • • N . Serial No. togs RO,OceMY and ROOM/Mien Mark USA RUDA • • 2. Orme . , Name (As sawn en reoutration combos(*) BA Leasing and Capital Corp. o . , Adores; (Oa shown on tooltfrallbn cortigabl). Tea Ember Frandsen odeto CA Canter San , 94111 • . . . t Mena Use Only • - 4. unit Meettikatien B. Type • Unit Make Mob! Metal Na. Repair • Month= AIRPAME (AidosOtits 1 Mho! l bow) • X POWSIFLANT I . PROPELLER a ApruAria Type Manufacturer ' 4. CeelenelteStreeteeM. • A. bitbools Hama and Mona 16. Kind Of hemem • i C. °protium Ho. Western Commander, Inc. 16.3110 Day Drive Van NuTst CA 91406 .. utctemeinas IAMPAIM RA3R8081 Airframe 3, 4. Radio 1 2 & 3 ,11zolted Powerplent, 'Instrument &Areressorr , X Certerer Rear Shaw • • teerutecom 0. I cora, that the repatriate( Maeda made to the oaf Mideadflad a Muni &tern VS daunted enure merit ex armaments hereto new been mare in ar..efOince with ihe repuiremenho of Part 43 el the US. relent Ariake Rnutaains and tnat toe informodon furnished herein ii Lea and o orreh tome best of my nowkolg. • . Oats Maury 41991 . • Signature at AuLlenne Marldual X 12A-----•' 7. amen la To SeSce Purrant to the atdnerhy given persona specified below. the unOleenaml In earn a was fashathed In 5W manner twelabed by ma Ada:tetra:et of the Federal Avietiun AddinistratIon she la WAPPROVED D REJECTED Inure Sterdarea I Imani so n ; tkIsitctor Instal= Autnorizahan Cam (Spree/ ‘ SY I na Desiree' Ix lane, sums, Person raormai Tampon CANNIAiiheifthitiel tii Group On ef Arrant erfleMetten Creacata or 4"" zed-, • . .RA3118081 2 . • / 0 1 / la -• '" I. SON Y_GliCO2754252 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241174 EFTA01326767 FAA AIRCRAFT REGISTRY CAMERA NO. / • DATE: 3- 7- 9/ SDNY_GM_02754253 NOTICE vicga• and balance oronaret ngtimnarlonchangesshanb. entered in throppropein!airerattrecord. Ariattaraiion must be cc:moil:eV with en meow aerations to assure continued conformity with the a0PaCare airworthiness OoserttOon Of Wort Accampllt NW • (Irma SPACP is Mown. coach additionat shoay kfeithly wW eiterfli riciionany and sligistrit;Oti mart and ate work COolOANOO) • • Installed Sensor Systems, Inc. L.-Band Antenna, PN: S65.5366-24 Serial No. 5712, at Horizontal Arm 151.0, in accordance Installation Drawing 1653-04 (-513 antenna installation) as substantiated by applicable portions of Elsinore Aerospace Systems Inc. engineering report 1.175, dated 12-11-90, approved by Robert E. Poteet, FAA Structures DER #494. • All workmanship has been accomplished in accordance with applicable pardons of Advisory Circulars 43.13-1A, Chapter 2, and 43.13-2A, Chapter 3 and 13. The Aircraft Weight and BalanCe Report and Equipment List has been revised to reflect this installation. The work described has been found to be in conformity with the above data, and continues tomeet the airworthiness critena under which it was originally certificated. END SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241175 EFTA01326768 FAA AIRCRAFT REGISTRY • CAv.EkA VD. / DATE: MAJOR REPAIR AND ALTERATION , It leLick-Li otMonnors EB 5 a.*:nkno.. (Airframe, Powerpiank Propeller, or Appliance • FollSe "man Alsoreirat — "' . VNY FSC r alsimowevau Otte NO. 21204:020 'buil • Far FAA Use alit '''' anal iesettification 0 Q -O-G! MInangratioatniniona 4 chli penalty flax to =tad SI.= INSTRUCTIONS.Printor two all orariek.SolFAR41.9.FAA a3AcpaniSiaL and AC 43.9-1 (OraoSatiothInwiaion and eisaosinon of this lonn. This *MIS IMAM O./ Ara f4OU.S,C, Ian. Failure to re9Ortean rano:tin by ur-n such violaban (Section sot Federal Aviation Allot IASI). - 1. Airtran Mak GULF s , STRF.AMAEROSEACE• Wool G-IV SON No. 1085 NaUonality ana Raer strhica mot USA NNIGA i Ovine, Name/At Mown on rogAsuatiOn Amnon:4y RA Lasing and Capital Corp. ,--• . • Aeven (At mown on mn.owition conaktre. , Two EmbascaderoCenter San Francisco, CA 94111 I Fot FAA the Only 4. UM Idannlicabon S. Type Una - - Mahe Mudd Serial NO. ROOS . A.Iternon . AIRFRAME . . . I As dolorlbOd AA hoe I chow,) X • - ICAYEAPIANT inOPILLER APPLIANCI • 71,4) - - Marataconar I. Caolonnity Ilateinoin A. Aptrimys NV,, and Manna I B. Kind S AgAncy I C. Granule No. • Western Commander, Inc. 16300 DallyThin Von Noys, CA 91406 . .. I uS.Careacitao woman< Airframe 3, 4 2 SU Powaylazt, & Aulasory - ANAL Iteceqn Cerilteeted lArc.anc. "o 1. X crenate. /lona Ss on IllmItal n Idinufliaitet IInsUomtnl 0 leutny um, too rifle and/or altmodon rnanato Co I unit(s) lanbtod In item I AbArro sod On.r.beden.nerrAteltOrarttAnmenCnvoto titre Nen nude es lieenreinCe wit. the requitenientl or Pan 4.3 of en US. Flat Aviation RagnIStioaa and that tie kiiarmation hardened herein le tale int correct le the Wu of my linowiedga. Dam • ' 1Signature,of Aulhodiiiis inateldual . Unary I; 1-991 • • I 7 . /ei.:•-•;-.. T. Amnia tarn re Sonia ' • PurtY4/11 to Ma aultionly Ceded; nate ...weird c4mulatratos el the Federal Aviation AtItninisInnon I Ir" Int $" " lifeaI luanitaton ' " / Inn ila01 I / _Y 1 I AA N yco" Ix ' Ammersada, . -*low. The ;:n9Orleor*3 In item 1 wag bora' in ma "Wass cede a -APPROVED 0 ASJICTED I I inna-bon Autnodunion I CIon:PIIIOU II !Pima Appeared by Tranuor: I Canada Ainionhnins Coto* I TIMIREbmIl bY Si. :IamnfAcolosatorgenic0en (CAMS= or ICelionaoon No. zit; /9/ ' I • RMRSOBIL, i5iOnficl Autriony/o4/9.7,xiGat ...? I .4.,-1-e - :Alf .. ' A FAA Farm 337 .1.10 -jets, • ipitOMIfirsr7"7 — . I SON1716N1_07542E.:1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241176 EFTA01326769 NOTICE Wednt end bitence or operating limitation change:shell tt: entered In IN en;w0Orlate eleven record. An attemtion must be competiWe with all previous alterations to assure continued cont‘trni, ♦:Y. int applicettisetretotchtness teduuenients. 1. Incorporated G•IV Phase IIProduct Enhancement Modification per Gulfstream Aerospace Document it 11S9SB42116, Revision A. Revision to the Aircraft Weight & Balance Report has been provided. Flight Manual Supplement 89-03 has been provided for incorporation mto the Aircraft Flight Manual. 2. The following major Gulfstream Aerospace Aircraft Service Changes have been incorporated: . . SDINFCG0.4_0/7§12er SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241177 EFTA01326770 r43LikaTlg::.: • ittekk AlitrIARE RECUT*? cmaita"no.. 0 2 tiara: ay.- /.3 1- 97. ll -verni ve: ; "row • . -2 0 MAJOR REPAIR AND ALTERATION vs move« encresmare (Airframe, PoserplanL Propeller, or Appilanee) Mom Anshe issmasseet Fond Apprdrred 01AB NO. 2I23-0320 for FAA un May ~Mew Dt.-Pa AO INSTRUCTIONS-. Note BMW entree Sea FAR 439. FAR 43 Appeals A enclAC43.9-i (or suteepuent ralsionthmeW lorInebotents end damortiOn ogee form This repon a rectered by law (49 U.S.O.1421). f ehrreto report can result I Gee sernly not CO none II.0O3 to, each stge resew (swoon 901 Feat Amnon Act (II 1955) ' t. AlrcMl • GITLESTREAM AEROSPACE CORP. Wen G- IV Sown No.. 1085 Netionaely onO Rejetralin nut N88GA 2. Caner Iteree (As Mee on redorradoneortMean) BA'LEASING & CAPITAL2.CORP. Add rcos (At shown On ~bon eettlIkeW TWO EMBARCADERO CENTER \ SAN FRANCISCO CA. 94111 - ‘. 3.•f-er FM Use OW, 4. Unit idenonesuon a. Tree UM Serial NO. ' Asper manse AYNMYE . • MeMermited on Men I Wore) rerT , . MUPILLEA `., ,.. APPLIANCE . I ACAMOrnIvineMel A, *Genera Hens len0 Areal B. Kindle Von C Centime No LANCE A. MATTESON 3015 NORTH HAXDEN ROAD SCOTTSDALE. AZ. 85251 S I US. Mehered lecterse AP 1864049 ror.yne.eaarnarumm eseitereeset ease mewed 0 ;centre tessentease Severetban~enedelOtiveunemsenatteatneemeseee too eau/its:I *nth< news of attacremenis hereto no* been made et accordance Me the sesteementi °ten 43 or thre U.S. Feder', Mitten Anulatens and that ow mnformaten banished non*, ts true and coma to IM Opt el ray !nowhere. Llete osi 9/pta r K- id • 7 A-Adroed Ow Rene To WrMee Supt. Of 2421 i Pit AAA ILCA Paean to the Dulaney given weans weasel mime se fine lama« in teem I was Mowed in ne manner preocrind by de Mffinetretor of the Feline Aviation ~tress end is Li APPROVED 0 REJECTED MA fief...incline Inspactor . - A Can (WOW InstecemAnhonntea BY MA Oterree Stann Pelenenneed try lemon Canna Amoneeen Group Dam cl Moron or Reectoon 1/7 y- 1 o One Cateen No. or o 44i7.05424 Sign!~ of Autorren FM Form SW “r rev Michael Donnel 1"10.4k000.5,4lbot. IL • * SbI _02754256 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, n 1 5, and 17 EFTA_00241178 EFTA01326771 FAA AIRCRAFT FECISTIT CAhTAA DATE; /j5-57/.. r64.64.mayes6sr. - " Jesm--?t;2_ • NOTICE • We4pht and balanceof operetinp limitation changesshall be enteredln thatapprOptlate aircraft mord An attention must be compatible with all previous alterations to azure continued abalone?* at the apptiCable einvonhinius requirement. censtamoiwesseasscasvo proonsyse•arrentemessauvorsithonsournmarrasenalved aM 6666mm,marldowsvoe°4666.4J November 9, 1990. Gulfstream Aerospac6 Corp." Model G-IV, 088GA, Aircraft Type Certificate Data Sheet Al2EA. Refer to: FAA APPROVED Gulfstream, Aerospace Corp. (GAC) optional Aircraft Service Change (ASC) No. 166 subject: EXHAUST (ATA-78), THRUST REVERSER SECONDARY LOCK AND WHEEL SPIN UP-- MODIFICATION dated August 17, 1990; GAC G-IV Wiring Diagram Manual drawing L159AV40137, Landing Gear Indicator System (sheet 1 of - 1) 32-6-1, Page ), dated January 19/90; GAC G-IV Wiring Diagram Manual drawing 1159AV40108, Thrust Maintenance Reverser System (Sheet 2 of 2), page 3 dated August 31/87; and GAC G-IV Manual 24-0-1 Page 5, dated August 8/86 para 10 Bolted Electrical Connections - Torque values. with This ASC adds circuitry which ensures prompt thrust reverser deployment wheel spin up. In addition, it adds a time delay relay to each thrust reverser's secondary lock solenoid circuit to prevent burning out solenoids due to exceeding the duty cycle. Complied with all of the applicable instructions contained in the ASC,. All installed parts were installed new and comply with the appropriate parts of FAR 21.303 (b)(1)(2)(4). Successfully performed the ASC's operational test: Returned the aircraft to flight status, recorded compliance with this FAA form 337 and ASC in the aircraft's maintenance Secords, returned completed compliance card- to GAC. It has been determined that the interrelationship between this change and any previously approved configuration .will not introduce any adverse effect upon the airworthiness of the aircraft. Thik,determination included, but was not limited to; consideration that the workmanship that vas done, the materials-that-yore-J.18°d, and the condition of the aircraft after this alteration were equal to-or_better than original Certified condition. The effect upon the electrical load analysis vas an-increase of 0.3 AMPS added to the ESSENTIAL DC BUS (during Thrust Reverser Deployment). The effect of this change on the aircraft's basic weight and balance report was negligible. END s/n 1085, SDPIY G-0.4:017.542E7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241179 EFTA01326772 YAA AIRCRAFT REGISTRY e'l • CAMERA NO. .2 DATE: / 3 -ft RECEIVED FAA Di MAWTSONTCOIRMOOREATITI . ODT. 2.3 t$114^nAlt=f FEDERAL AVIATION ACATINFSTRAERte4 ' • • ateks VA 04-406a.t MAJOR REPAIR AND ALTERATION VNY FSDO FOE FAA USE OWLY (Airframe, PrverpTara, Propeller, or Appliance) OFFICE OBOVCATION INSTRUCTIONS: PSI or type ell entries. get FAR 43.9. FeR 41 Apptedit R. and AC 41•9-1 Cot uttsweeeet revision for sennections sad &galantine d nib theme° fora I /NOME • . • imams GULESTREAN AEROSPACE . A. G -1V SERIAL NO. e ' INATIONALTTY AND RENSTRATION AMIE 1085 ' I U.S.A. N88GA X MEI NAME (A. skein re reentref ontigane) .4001IISS (As thew. en nperroticet onsitgeerei BA Leasing and Capital .Corp.] Two Embarcadero Center .. San Francisco, CA 94111 3. FOGA* us* an . 4. EISIT IDEMMAIN)N S ME own Nail . ones sena to>. serait ante￾MION AEVEAME • (Ai &weal ma Aim I ahem) X FOWIPPEANT POOPEGIA APPLIAna not • . • .- • •6. 0)/0041AIT STATUE/I A. AGENCY 5 NAME AND AbOltESS Westarn Commander, Inc. Repair I. KIND OF AGENCY at ClefoliCatte ace... C. CERTIFICATE NO. 16300 Daily Drive - . 101.101.1 CIITIIIttlle 04CM...0 Repa RA3R80.8b Station No. Yan Nuys, CA 91406 X Cleetwerre WM. HAMM 0•10410401,0till A3 Serilti,42f, & 3 D. I certify tbet•ibe. weak. sed/or Jambs made te taschnewts hence Iwo brae made is accoadeace ends and chat the Wormedw haelsbed twat Is trite and the onitli) ideeti6ed is iron 4 above sad described cos the etyma or the requireeento of Pan 43 or die U.S. Fetna Aviation Itegolanicep comet to the beet cd ray knowledge. .. ' DATE October 24, 1990' SIGNATURE OF AUTNOW2D INDEVIDUAL (17- t AMEMO4 NU SU was ies &teratd a the unseen prewriteed by Pyrites to the sethedry_gewee reins specified below the van identified in New 4 irpz TD the Adsieleauto at the Fedeesl Aviation Adesantstruiese sad is Em APPROVED ra. ea AT. Moan d/W•fathIlel . .... tea ame• 0 .,, II . sea 00.01411.-- - X'. . &MA stArtOn fauvism Warabie co nasty nset otrICTOR CO MONT ' — • DAR .- of AffEIOVAL pa October 24, 1990 COMRCATI Oa DISIONATION NO. CRS NRA3R808I. SS4 1: 7 r irte UArt:e . . ... SDNY_60.4 02754258 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241I80 EFTA01326773 'FAA AIRCRAYI RIGISIIT CAVIERA PIO. gp DAIL: -- / 34/3- 9/. • - NOTICE Weight and balance or operating limitation changesshab bontered iri the ePtarogiate aircraft record. An alteration must' be compatible with all' prpwOOS.alteratIOnslo assunr continued conformity with the applicable ainyorthiness requirements. • 8. DESCRIPTION OF, WORK ACCOMPUSHED (If mare-space is required' attach .additional_sheets. Identity with aircraft nationalityand registration rnailtand date mark completed) • . • •-• • - Install ed Remote Heading/Courie'Conifols -on pilotand oc pilot control wheels in accordance witg.puPP1eliental Type. Certificate ISA5001NM, dated Aygust 1990.— Flight Manual. Supplement 008015004 NTO.- 'dated' August . 30;- 1990r Was, been •provtded: t" " • The effect of this iiicialtatib -p- citairciiaft—basic weight and . _ balance is wegtigible. Thls_kircraft continues -to mesa all „ • . . —airworthiness—ff.:jut rementsi- cifvo,r.1 Tina. 1--certifieation. . _ FAA AC 114904 IliinH ittiepr. Cu t. Govrtmurmt S`PJPIltur. Cr rcc.- 1144-€T .b SDNY GM_02754259 ---- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 IR! EFTA01326774 3 ISIMMIIERUIRP ,Lt .17M 1141STRI T CAMERA RD. 7, DATE4.02 /G4" 4/3I ,G- 1 O* fin Batt tNA ot-R060.i cfMtlete neentgrATON 1.,, _a ...n - MEW AvIATiON ADJAIKSTIATION .4.. r ‘‘' MAJOR REPAIR AND ALTERATION 0 -30 .a . TAPfroma, sowarplant, Propellor, or APP1h4F 5 FOR MA UM ONLY ONCE ofrancanoti . INSIRUCTIONS. foe lostrealos sad Print dliposIdoo al type of ell ristlici. Stil FAR CS, PAR 43 ApPidna 8. sod AC 4351 les Abatement adios dash this feat . •I . ROAR MAXI GIII.FSTREAR AEROSPACE MOOR G1V SOW NO. 108S , NADONALM AND atcaStitanom NARK U.S.A. 888GA 2. OMER Waif& aftwornmenthetotico terlilleoN) 8A Leasing and Capital Corporation ADDRESS Os rod on dyistrodo cesA0.0) Two Embarcadero Center San Francisco CA 94111 --., 3. FOR MA WE OW .. . ,, 4. UNIT IDERTIFIGTION $ TIN UNIT mast AMON AIRFRAME •,- do Dem X /4 cased le I eon) ' PM/RANT ANUANCI tin • • . • IIAMPALIVIIIII E. 1NIFOIIIP11 STUMM A *can we AND ADDRESS I. RIND OP AOENCf ' C. CIADACATE NO. WEStEAN COMMANDER, INC. 16300 Daily Drive Van Nuys, CA 9 1406 as aninuiva Aff00.4/41C 'Repair Station No. , I1A3A8081 - A3 A 4, Al, 2, 8 3 Ll , A .1 P mato« CtIMO•CMID iiitaeli K CICIIKARD Walt STATION IsutUFaCIIMIt D. east I cotify otats that bent* the npals be bees end/or made ahead°. somas to the waifs) identified is beta 4 above sod desalt.' es the tame ot Nod Is ettoolsoce with the ageless' of Part 43 of the U.S. Metal Addeo R.gviedo. that the haforthatioa fandthed herds is true ad canto to the ben of my honk:dot DATE PC/NATURE Of ALMIOALUE7400ADUAL August 24, 1990 ' 7. APPROVAL FOR AETUI soma-. Panda to the sotharisy_fibm eddied below tho Needled La item 4 ia the Adataban of the Mad dada Analog. die ratted the odder prescribed by Adalebetedos Midis (3 APPROVED IM OMR DANA, IT sit Pe4.0404 mastAssan IMPICTIMINTIOCCArOl 1.0. Men X WAR RATON CAPObt011 PIAXIMIM 0 9141.201B tWCOI DATE OF APPROVAL OR REJECTION august 24, 1990 ONITINCATI OR DISIGNA")" NO RS RRA3R808C • . 310 Uld Of AUER/NUM PCMDUAL Z .....4..c.o.c. 67 O.2%tes , ‘ tYib,-,NtOtters' • t f. SDNY_GM_02754280 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFIA_00241182 EFTA01326775 t • ASS rOLA Li/WELTS itIGISTIRI Clint* FO. 02, rant -: 13 - NOTICE An Weight alteration and balance mint be or compatibie oar ating limitation with changes shall be entered in the appropriate aircraft •ecord. applicable airworthiness requirements. oft previous alterations to octane continued conformity with the L DFX(MPTION OF WORX ACOMPLIWIFO (If more space is required. attach additional sheets. Identify with bi￾croft ncdionality and registration mark and date work completed.) The following major Gulfstream Aerospace Aircraft•Service Changes have been incorporated: . . . ASC.#135 = ECS .PaCk Sequetielog',GuringlEngine Start - ASC #137 G-111 HMI Dedicated hydraulic Filter - Installation The effect of these changes on the aircraft's_ basic weight and balance are negligible. WhiY_GiAji3275#2031 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241183 EFTA01326776 FAA AIRCRAFT /dC1STIT CAMERA PO. a? DAM - /3 - 57/11 DIA01107 OF TWISIVIDAWNI 49 9 eO at • Fillasi AVIATION AOMPIISTUIDON- 2 44 . . Fa. - • e./j.. MO; 04- R060.1 o MAJOR REPAIR AND ALTERA1113i9V),,,, ." 0 47 0 'FOR PAA USE ONLY • (Airframe, Powerplant, Propeller, or ApplioneaVaa v OFTKE. IDROFICATION 'Y -C.' "C;_. INSTRUCTIONS, Pain of type all aught' See FAR 45.9, FAR 4) Appnadia 8, sad AC 43.9-I for nbsentene it Vilna diete00 fur en.ereaieei and dispo34104 of ibis form. .-1 • I. MtUAR MAKE Gultstrean Aerospace Corp. MODEL 0-Ill ( r‘ -j SERIAL NO. 1085 NADI:MAW( AND REGISTRATION A99/RR . OS& N880A ..- 7. °WWI MANE (As 'Lawn en snistersPop affilicetel . BA Leasing and Capital Corporation ADM-SS (A. .bon au Nipidtalicia cunt motel Two Emhargadero Center San Francisco, CA 94111 - 3. FON FAA ME OM 4. UNIT IIIINTIFKATIMI s im Mitt MAO . 1 Ø 'is, . NO. ilt/sill WO. ' JØ A2MAla ••••••••••• (A ~lied il Ova I Sore) POwTOLI•HT PII01111ER 'YU Cockpit Voice Recorder MOO , 53674 V , - x APPLIANCE SW4WArnitall Fairchild F. CONFORMITY SIATEMDIT ' . A. AGENCY'S NAME AND ADDRESS a. KIND OF AGENCY C. CERTIFICATE NO Western Canaander, Inc. 16900 Daily _Drive ' Van Nuys, tit 91406 . tit. Cletif CAM KIChanK RAIR808L APR. 3, 4 Radio 1, 2 å 3 . Limited Powerplant, Instrument & Ace. • Canis a BletICATIO MIONSC < E' nitonart RIME li mion mu.VIACIVan D. I «nit( Ow On awls end/o• alwidon ede to the wigs) identified in hem I non sad desnind on the titer.. oe anarbennes hereto lave bien node In nowinace with he feqoineenta of Pan 43 ad Jr V.S. adinl Aviation Regobona and dui the inketaatien furalnal barren ia we atill nation act ne bed of an knowledge. DATE . 5 7"'" t• 8-TO • =NATURE OF AUTHORIZC Lel. • N t J. Arno FT FOR UM TO Siena P aaaaa na to Ion anbority In ponninecited bond the oak Egynainal i. Item 4 -a inward n an'tnanet pennant by tbe Annie, o( es. Federal .A.istna A.Wittiacrneo and is al. APPROVED R EJ ECI RD SY in Tu. StAtnArs oMclot mAndmausta. Onteacea ALITICOLTAMM annfl." 1 1 MA 04SanaTA , c Wm» Dane• " " ' t o o tpØ IN CAMPY. btrAttady41 tnestOn ~KIM • DATE Of APPROVAL OR . REJECTION , 9 - 28-90 CERT111CATE OA DESIGNATION NO . . SIGNATURE Of AUTHORIZED INDIVIDUAL , ...i f . -4eae.- CP CZ.1 / FAA Form 337 then oast do O. moo (83701 SDNY_GM_02754262 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241184 EFTA01326777 FAA AIRCP.AFI REGISIIT CAMERA 110. _ Malt ea— /Or n, • 14CitiCt • Weight and balcince or operating limitation aangesAoltbi inroad in the ppisfopriote aircraft recent may - An alteration most be compolible‘wills all previous allproliiins (reassure Coatipoed conformity with the , --. applkabli critworthiness requirententw ... . - • • . 8. DESUITT1OR OF WM AttOlAtt1140 (II more secant illeitilred, attach additional sheets. Identify with air. croft nationality and registration' mark and date work completed.) • . • ; Added Dndereater GocatinO1Device to Fairchild Model A100 Cockpit Voice - Recorder, Serial ylvieber_53614,. hi' complying with Loral Data Systems, Fairchild Aviation Recorders, Field' ServiceiDulietin. Berber cvit•aSee Modification 7 hes beau marked oo..the Nedificatiop Plate. - . • - "• The Voice Recorder.inakellatiiiii-in this airplitoe Melts the requirements of, and easei1O withIPAC.91:605.. (dl)_: (e); FAR 25.1457 (a1),(a2),(6),(e),(d),(0), • • • tc- • 1 noe4;sto, q4aOfAtir 44‘ t - "N" SDNY G0.4_02754263- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241I85 EFTA01326778 I P. IF • \NM r,M-,AllteRATT CAI4TILA w0. ap DATE: e2- /3— 9/ . • MAJOR REPAIR AND ALTERATION us moans a sastateen (Airirame, Powerplant, Propeller, or Apparent) . Podert•••••••• ilerfeeswelke Keen *moves — OMR No. 120•OZD FOY FAA LINO* Oros kleleteketien S2) I- — rst> INSTRUCTIONS. Print oe type all entries. See FAR CA FAR 43 Apparel' Et. and AC 4194 (or subsebuent revision thereof) for instructions and catoositionol this loon. This report le illaulflid by taw 09 U.S.C.1411). Future to rayon can resist I solve penalty not to estee211.400 fat each such notation (Section poi Federal Aviation Ad of 1954). . 1. Astro Make GOLPSTREAM AEROSPACE CORP. Model . G-IV Serial No , i 085 Naisoremywern 11 Merit . &Owner Sens Ms short on topttrigke mellow ' BA LEASING A CAPITAL CORP. Adder; Ma shown ms repiatratlon Cerlfdeetel TWO EMBARCADERO CENTER ' SAN FRA:NELES130 - 09c•-• •-•94111 . • 1.ForPAAUse00, • • 4. Unit letantlecaton S. Type Unit Make Model I._ Senal No. i Repair Aittration AIRFhAME . • (As darned' Item I above XX POWERPLANT PROPELLER 1 ' I Aetna Type ..,- i . Maistachne• 6. Contomaty Stliallallee A. Agency's Name end Address ). Kind ciAPR*•• • : i•• C. Ceara' No. • LANCE A. MATTESON • 3015 NORTH BUDS ROAD SCOTTSDALE, AZ. 85251 • . . • AP 1864049 us cenegasseMicaesic F ame Carelialei Mann aninetned flaw Samos kraniAaner .i i D. I certify that the repast and/or alteration made to the urn(s)elsotsfsed in AIM 4 above end described on the resat. 01,1Llautienta Patti: Mn bola maws in women« wan ins nowemenisca Pan 43 of me DS. Federal Anabon Fleautsbons and that she infaimatem turneshed lino is two arse Cereal to the but of my rowledge. Owe 4,...7, /5,qto•L Regnante* of A ividualz . "5.0— .-.f SitastLLstient,... t'APPreval tor Rant To Sande - . Purloin, to the atahontY yetipens'absented belOw. IMt identified in tleM 4 twn inspeeted in the manna emcee by the ACIII.MalratOf al the Federal Avow Administriban ono is APPROVED - 0 REJECTED FAA Fe. Stittsfaras etsdeCke let u•nosautx i wspactianAUlbOriZttiOn Opt (Specify) BY FAA pewee Rae Station , . . Pawn nopand by Tension osia oi Approval°, asecnon Alt CI 1 Of I 9 ID canna* Ot neon No. °511705484: . '' . Signature of nelnid FAA Furor 2 7 Michael y -- _ - 1:W4in- . • ••• SONY GM 02754264 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241186 EFTA01326779 • ; IAA AIRCWOMREGISTRI CAMERA RO. Q bATL:4,- NOTICE Weigh! end balance or operating linUfation changesshail be entered in thiaapprOpriala airmen record. An'arteration mut t be • compatible with all previous afterabona to &nun continued conformity with the applicable airworrhinen requirstmillt. I. Description et ork AO>teeplbrie0 in mon space le Moroi attach additional enema klerwly with rain naaywwy one regotnicen wad and 0at@ *Ore COntOtelett) Aug. 08, 1990. Gulfstream.Aeroepace Corp. Model G-IV, sin 1085, NO8GA, Aircraft Type Certificate Data Sheet Al2E.A. . Refer to: FAA FORM 337 dated1-1S-90, for the-above referred to aircraft. The purpose of this alteration--is-to-remove the-changes that were incorporated to the Auxiliary-Power Chit (APO) Surge Valve Control circuits, as detailed on the above referred to FAA FORM 337, and return the Surge Valve's circuit to it's original.certificated configuration. In the Aux Power Relay and Junction box (39A1) performed the following wiring changes: Removed vire H70C20 from relay 339A1X1115 position B2, routed the vire along existing vire runs to 339A1TJAN position C, cut the vire to length, stripped the insulation from the free end, crimp installed a new CTS-520/20 contact onto the prepared vire and inserted the wire/contact into TJ1N position C; Removed and discarded wire H77MF22 from 339A1X115 B1 and 339A1TJR position Er Inserted a new CTS-S16/16 contact into 339A1XR15 position B2 and position Bl; Secured all of the wiring, components, and access of the 339A1 Aux Power Relay Junction Box. . All installed parts.vere purchased new and comply with the appropriate parts of FAR 21.503 (b)(1)(2)(4). Tested the alteration by :rising the FAA Approved aircraft flight manual procedures for starting, rift:ping, and stopping the APO'and noted no abnormal operation, indication or performance. ' Returned the aircraft to flight status, recorded compliance with this FAA FORM 337 in the aircraft's maintenance records. It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The effect upon the electrical load analysis and the weight and balance of this aircraft as a result of this change vas negligible and no changes to either report were made. . END 08/08/90fted/89mf"" 0 Additional Sheets Am Allacttl. • SDNY GM 02754265 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241187 EFTA01326780 FAA AlliCtlar 110187 • CAN1RA N0e7 N Dills ft - 2040 al alarm. MAJOR REPAIR AND ALTERATION a kneroshof , (Airframe, Powerplant, Propeller, or Appliance) i ildliSININSR . 1 roan hltreved OW No.2120-0320 Por FAA Use Ordy INSTRUCTIONS: 116117864ran Print or type ell trees. See FAR43.9.FAR 43 Appendet El. endAC43.2-1(oesubeertuent and dispowlien of nu . rerbionthereo0fOrInelructIons form. This reporttsi•Rufreebyisw(49t4S.c.101).Failureto repent= npeelOn 4 CBI penlitynot lo evad$1.000 for eacn NIA violation (Section 901 federal Arinion Aa of 1964). 1. *boron Mane • GOLPSTREAm AEROSPACE CORP. Moe* G—IY Serial tex 1085 taboret*, ono Refrotretion Min - N880A 3 Oar Name (As shown on mgestrionetakeete) BA LEASING 8 CAPITAL CORP. • hocIress (As Uptown on nvierwan awakes) TWO EMBARCADERO CENTER . SAN FRANCISCO CA. 94111 3. For FAA Use 0 I. UM kliontlikstlan , a Trot tem make mese Sens NO. . fterau Atieralion raFPAIAE •• • ,, ' . . • Ms clasintiel In Rem I Send • XX . PONERPLANT j.." . , . PROPELLER •Type • I I • , a CorionarlySleleinel A. Agenets learns am A600121 B. Kneel , C. Gramme No. LANCE A. pairssow -- • 3015 NORTH HAYDEN ROAD SCOTTSDALE. AZ. 85251 AP 1864049 . '0.ieermymmummeerammeweneemeaftioew4 tad on Ine reverse or &Revenant nereio here been nude In acoyedence fen the refenteart44,4 ligterons and the, the tnforrimbert funnels) tete Plea ancl Oyenlo to the best ol flyer Date S .... - r Anis. kw - -pt. of Maintenance Pas* to the Sae* Shen ;Sans specitiett beet Orkplet4dentefee fa de 4 hes Women Sine manner prescribed by Me AdTabittlitit of the ',Clem, Mt° Ataseustraka and b AD APPOOWIO . 0 REACTED - Fizellarniforris r woodmen. x • - - bispectanAgoineczeon Otte ISPearr) BY FAA Deephee. Repay Station tBetNANNIWOOtensmom I lainemeAtroronlass Oats 01 443900WIlor Resection 6 -.1.8 —RO cemlate or Daignaaenwo. 126705494. SWAIM, AA Fora aA fo Michael D an Ily SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241188 EFTA01326781 SDNY GM_02754267 e. .tAtit,(1):SW￾I FAA AlICRAFF *Emma : • CAMERA WE./ DATES 12 NOTICE • Weight and balanceor °panting limitation changes shall beentered in theappropriate aircraft record. An alteration Must O• , compatible with all previous alterations to mute continued conformity with Ma applicable airworthiness requirements. 0. disMpbort of Wmt Aacoi.eSMd in more space is emoted. atoo astrhbansf shifts. Identily Win eltaWInationentyyna registration man and daft work computed.) June 28, 1990. Gulfstream•Aexospace Corp. Model G-IV, s/n 1085, 688GA, Aircraft Type Certificate Data Sheet Al2EA. Refer to: FAA APPROVED Gullstream Aerospace Corp.-(GAC) optional Aircraft Service Change (ABC) No. 131 subject: LIGHTING (ATA-33), TAXI LIGHT POSITIVE CONTROL-MODIFICATEON,.dated February 26, 1990. sheet 1 of 3) 33-1-3, page 3, dated January 23/88. This ASC modifies the taxi light circuitry to ensure the tax( lights go off whenever the landing gear is raised. . • Complied with all of the instructions contained in the 6SC; except as noted herein: (Refer to figure- 2, page 7 of the instructions) instead of the in-line diode module part number 1159SCAV-903 utilized an existing spare rail mount diode assembly Deutsch part number CTJ420E011 and connected the wires as follows: (a) Wire L9001A20 to position A; Wire L9000A20 to position B; Wire G66AA20 to position F; and vire L9000B20 to position G. Note the existing rail mounted diode assembly has identical ratings as the in-line diode furnished with the ASC and, in addition, offers a more secure mount, spare parts commonalty, and a neater installation, (b) Figure 2 shows 326A1J4 and 324A1P4 incorrectlY,'Vire number L9000D20 is connected.to 326A1P4 position small Fend vire number L9000C20 is connected to 326A1J4 position small P. Note 326A1 is part of MAIN JCT'AND RELAY PANEL i2. - -- (c) Wire L540A20N vas removed from 823 position H, the drawing and text - list HIS/position - - All-Initalled parts were purchased from GAC and comply with the appropiiate parts of PAR 21.303 (b)(1)(2)(4). 'Successfully performed the ASC's operational check after replacing the defective left taxi- light with a new GE 4587 lamp, returned the aircraft to flight itatus,:recorded cempliance with this ASC in the aircraft's maintenance records, and returned the completed ASC compliance card to GAC. - • It has been determined that the interrelationship between this change -and any previously approved configuration vill'sot introduce any adverse effect upon the airvorthiriess of the aircraft. This determination included, but vas not limited to, consideration that any deviations to the original. ASC- would - not change the intent, operation, or test procedures. • _ _ The effect upon the electrical'load analysis and the weight and balance of this aiccraft'as a'result of this change vas-negligible -and no changes to either report vere made. - . END ❑ Additional SIMMSAn .AttiChld SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241189 EFTA01326782 1434rDt ,fl :•:3.4 FAA AIRCF.AfT itEczrat CAXLP.L PD.i N DATES 72 MAJOR REPAIR AND ALTERATION . uSononeen Asaeoneen (Airframe, PowmplarA Piapolier, Of Appliance) ii............ - HarassHarassHarass , _ Fonn AOINOvild owe No. 91200020 °Moe IdentificAAatioUnm** tForuF PO 7 - INSTRUCTIONS: hrint Cirtype all *nue.. Sear/ACE FARMIAppendia El. m0044394 (or sitteepirant Mahan that/1100 Mr inshudinnt and disooNtion of anslorret.PM raper is required bylaw/(49U-S.C. 1121). Failure le tepottean mann In a chid penally not to exceed 91.000 for each such violation (Section 901 Federal Aviation Act Cit INS).. - . . 1. Aka* Make GULFSTREAM AEROSPACE CORP. PAWS G -IV Wel No. r 1085 - NFIFFISFY and Fleantration Mark N88GA tower Nemo (As shown on icestranon onstPCO) BA LEASING 8 CAPITAL CORP.. :. Midas, (AS Ahern On IlpiglatiOn Candlelit*, TWO EMBARCADERO CENTER SAN FRANCISCO CA. - 94111 •3; ferFAAlls•Oida .... a. Unit identdAmion S. Typo Unit /Asks Mode Seal No. Repaa' Alteration MRCAAME ONO NO It show,' XX (A. POWERFIAM ,T :.• , AMPULLA b a APRJNCE • Type Manuiscaens - a. Conlennily Satan A. Agency* Men' end Addams Kind of ArienCy - C. Corolicat• No. LANCE A.,MATTESON - ' . . 3015 NORTH -HAYDEN ROAD • 'SCOTTSDALE,—A2. 85251 . Ca u.S. Genera. illaCtsVC . AP 1864049 'wain Glin4001,10.4•OUSC conarammasesimen Minutattair -0. I Wrote that tharepaa antIAN altaraitomnade loth, Lineal tdonulied in demo ahoy* and agameed on the mangy:gamy-Anent, hemp have been nada in atelNelanel with me requirements ol Pan a3 elm* U.S. Federal Aviation Regulators and that ma ntormation luenished herein C Ma and Canna to MeatN of my knowl•d9ll- .,. . Ora 4.,C "1:2-7 If Pe • 1 ' c Yip L....-. C , ' 1 Apron' I it re Reba r 0 tormiceStiot . of Maintenance . purr Adminlalrator BY a) We autheety pen omen SPeCifted 0810w. ‘011 roil kit040•0 in item a was irameeteil In he mwr plasaited by the of Me Feint Milton Admintatrabon 'and is . , X3 APPROVED .13 REJECTED FAA FR. Stanclattb InWector / - t OlharISPOW Insincton Mithentarion - " . FAA NW*. i • 'Room SUNNI Pinion Arnroved hY C TranSOOn anada Mr.cordnesa is 1ii Dataeapproval 4, '03 as RapICIPOn ' 'Gotham de . iDestora,on l No. ' —cp • t26765494 - • Sionanot ea -- FAA Fenn DV arm. • Michael Doz.! Ily SONY GM_02754268 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241190 EFTA01326783 • 7 NOTICE Waive and balance orOperating limitation cftargeaahNr be 'Mead M the eillX0Prlati !Ur felf ler rd. Anal:oration must oa compatible with all previous alteratoons to assure coittlnued curtormity wish the aipl.cable einvorthMen requiroomon￾a. Deatplion of Walt Accomplishes; Of MOO sons, Muiresl, anach adOilional fl ea wordy with 'IWO nallOrlibYr and nfriStrati3n enlist andtin *04 oaTemez/ June 28, 1990. Gulfstream Aerospace Corp. Model G-IV, s/n 1085, N88GA, Aircraft,Type Certificate Data Sheet Al2EA. Refer to: FAA APPROVED Gulfstream Aerospace Corp. (GAC) recommended Aircraft Service Change (ASC) No. 130 subject: ELECTRICAL (ATA-24), Provisions for Standby Engine Instrument Signal Conditioner (Watch Dog Timer) Test Citcuit-Installation, dated January_30, 1990, G-IV Wiring Diagram Manual -draving 1159AV40192, Standby Engine Instrument Indicator (sheet 1 of 1) 77-3-1. Page-2, dated January 19/90; and G-IV Wiring Diagram Manual drawing 1159AV40129 Annunciator Lights dim and test (sheet 1 of 3) 33-1-3, page 3, -dated- January 23/88. • This ASC adds PROVISIONS for a test circuit for. the standby engine instrument signal. conditioner. The 1159SCF412-17 signal conditioner viii be replaced through attrition:" This ASC may be accomplished in its entirety and the 1159SCP412-17.signal conditioner may be replaced at a later date. Complied with all of the instructions contained in the ASC, except as noted herein: (Refer to figure 2, page 7 of the instructions) utilized the existing GAC835101205 contact for the connection to the Standby Engine Signal Conditioner -(92A1) connector 92A1PI position 53. Note triangle 5 lists an incorrect part number for this contact; utilized spare position V instead of. A forthe connection of wires W888A20 and W888620 at connectors 325A1J51 and 325A1P51 because position A vas occupied by an existing.vice.. Note the effectivity listed on the figure for the connection at P51 is incorrect (a/c 1006-1054). The correct effectivity -is (a/c 1006-1095).as listed in triangle note 2 of the G-IV' Wiring Diagram Manual 1159AV40192 referred to above. Ail installed parts were purchased from GAC and comply with the appropriate parts of FAR 21'.303 (b)(1)(2)(4). Successfully'performed - the ASC's continuity teat, returned the aircraft to flight status with STANDBY ENGINE INSTRUMENT SIGNAL CONDITIONER Part No. GAC 1159SCF412-13 s/n 05891020 installed in rack 92A1, recorded "compliante with this-ASC in the aircraft's maintenance records, and returned the completed ASC-compliance card to GAC. It has been determined that the interrelationship between this change and any previously approved configuration will.not introduce any n57ersn effect upon the airworthineis.of the aircraft. This- determination included, but vas - riot limited to, consideration that any deviations to the original ASC-would:rioi change the -intent, operation, or test procedurei. The effect upon thrplectrical load analysis and the weight and balance of this aircraft at a'result.oi this change was negligible and no .: changes to either report were made. ,„, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 104,7;,°754715-17 EFTA01326784 ta, 0 . MAJOR REPAIR AND ALTERATION . lel Orconin ' Ada APProved OMR No. 2120-0022 . fa FAA Use Only al ereAla•A (Aid tame, Powerplant, Propeller, or Applianinl) lealeh easvebasils. s :. Office Identfiketion 0 P (97 ' - INSTRUCTIONS:Print or type MI entries. See EN241.2. FAR a Apperax41.arl AC atkt (or eased ant Raton thereoftforataxans end Peptones, of "tea. las mond naiad bytadatitUSC. 142u. Falai° report cannon in•arilyenaity not battaal DISCO ley nee well viol:bon (Section -' 90I hoes Aviation AO of 1958). - Make GULPSTREAM . AEROSPACE CORP. G-IV I. Alava Sad No. 85 '. • - 10 0770afiy NBEIGA ad Regleardion teat 2. Caw New (At Seem corefitlratilineetlileate) • . . . . BA LEASING & CAPITAL CORP. . . Adam OF Mown On registratlen TWO Irliellel 'EMBARCADERO CENTER I. feria Use Only- & Una tranducation ' 5. Type Unit areal Saud No. Amid AtterA.zn AS de 4 000 born XX POWERPI.AKT eaeOeFtLf9I . . APSUNCIE Type I IlIaleiSaetwer S. A Arca ,* Mane and Mitten 9. Rind of Mara 0 Ceara Na LANCE A.- MATTESON SCOTTSDALE, 3015 NORTH HAYDEN ROAD AZ. 85251. _ A VS.C.reseed44.41:Aarae • AP I664049 leareeGelikele04140IY ANY A4 Oirtecaleci 0. Slaw I ands mat the ropes estypor SRrneon math to the tin to) stenetrntho epee mote and described on the ~soot MUChenents Motto Met been suet in accedence we me adAreeriera at Part 43 at ihel.A.S. Federal Avaeran Regulation and hot the elletenaLed lueraill ISOM is dee end coned to IN, best at My ritae14090. One Jrreerer 7./ "f eta - ' I • ' • FC' . 7 Aprotalke Rave TO Spree. WF us no IF1t4mo rl,- v Ant ant to me eulhOries Whin pistons specified bar. the ea Iodated in elan 4 an inepeeted in the Tanner preicritted by the antinistrator ot the fan Aglaia atraistranen add " 0, APPROVED 0 REJE-C11912. ' . - FAA fit Dattala Inspector . , • -. Ote4MISDOOFF1 BY FAA Dileers. Pepin Seabee Pasonleiworel by TeSelipon Gera Aireardenen Grove Oen of Approval Or Martian . 6 -,z 7- 9)O Certhate or OlOgnatton No. . 526705494 • at /4? .e. fel -rr' s- VOA 027542--r SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241 c•aissa;4 EFTA01326785 1 1'7 FAA AlwCTAYI XTGIHIAY CAmERA NO.! .N DATZI 12 - .r NOTICE' weight and balance oroperating limitation changes shall be entered in the appropilate ahcrak record. An a lleration AAnmat be compatible with all previous alteqations lonstnecOntinuedcoaformitywith theapplicableastworthenessrequiroments. L DoserLitlowel Welt ACconSed (II mere space at resold. much • SWIMS June 27, she :Sniffy *Oh strati netionafity and agitelyttion rivek and date work completed.) Aircraft Type 1990. Certificate Gulfstream Aerospace Corp. Model G-IV, s/n 1065, NEIAGA, Data Sheet Al2EA. Refer Aircraft to: Service FAA APPROVED Gulfstream.Aerospace Corp. (GAC) recommended Cockpit/Cabin Temperature Change (ASC) No.. 170 sub: AIR-CONDITIONING (ATA-21), 1990;. GAC G-IV Wiring sensor power source-rebus, dated March 30, DISTRIBUTION, (sheet_1-ot-2) Diagram -Manual drawing 1159AV40103, DC POWER^ Military 2475-1, Page 3.,_dated annuary19/20k_ Standard MS35336; and MS51957: system This ASC from moves the the right power source ofcabin and cockpit temperature control hue. main • 28'Volt DC Bus . to the essential 2U'Volt DC . . noted Complied herein: with all Wire of P615AB14 the instructions contained in the ASC, except as discarded, a new vire was removed from the aircraft and between CH212 and 08292 was stamped and identified P602AF10 and connected connecting the vire, and a MS51957-43 acre:, vas installed at CH292 P603AD10 vas removed bus bar and circuit breaker together properly; Wire stamped and identified from P600AG10 the aircraft and discarded, a new wire vas and a MS51967-43 screw and connected between CB214 and CH256 bar.and circuit breaker vas together installed at CB256 connecting the vire, bus P615214 were not removed . properly; Wire P615AA12 and Wire original ASC were done to from conform the aircraft. These deviations from the incorporated in aircraft s/n to production changes that have been wire/circuit breaker matching; 1120 and subsequent and provide for•proper • see:.FAA AC 43.13-1A para 429*, b., c. . parts All installed of FAR 21.303 parts were installed - new and comply with the appropriate (b)(1)(2)(4). Succeisfullyperformed to flight statue, recorded the ASC'a operational test, returned the aircraft maintenance recordi, CoMpliance'vith this ASC in the 4ircraft's returned coMpleted compliance card to CAC. It has been. determined thatille Interrelationship and any previousli, approvedTedef between this change effect upon the aitiforibineei igOration vill.not introduce any adverse included, but was 'of thw:aircraft. This determination to the original ASC -dot would limited to; (a) consideration that any deviations procedures, (b) Aircraft quality not chinge.the intent, operation; or test vire vas-used that vas the correct size for the current reqUiremelitd,-operating conditions, and (c) the temperatures, -and environmental that will not interfere'vitfi installed equipment will function in a manner OthiadVersely effec't the safe operation of the aircraft.. The effect upon the electriCal.load analysis and the weight and balance of this aircraft-as a result of-this change vas negligible and no changes to either report vere'made. ArialionailloitaAni AttaCted 2 : • a t 41,— :an ts . SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241193 EFTA01326786 FAA AIRCRAFT REGISTRY. CAHERA NC. 3 N DATE: 70-23-90 MAJOR REPAIR AND ALTERATION - • rroarocooNo (Airframe, Powerplonl, Propeller, or Appliance) federensist MINSIanaie. roan Approved-- oue No. 21204320 For FAA LW OS! Mop loomilication g.--D L—Pra"DO INSTRUCTIONS:POW ortypfli entries.Se•PAR43.9.FAR43 AppenomB. and AC432-1 (orsubsaquarandslon thereof} forinstructionS and disPosition Ofthis form. This nowt 4 rewired try law (49 U.S.C. 1421). Failure to wort owl WW1 Macivil penally wit to Mad 91.003 lot each such violation (Erion 901 Federal AvWion Act of 196$). 1 Alectill MSe GULFSTREAM AEROSPACE CORP. Modal ' G —I V SSW HO. 1°85 Nationality and Jr Mart • - N88G 2. Owner "awitlitatfirg2Irt Catch CORP. .—i Ana. (Al a wnEhtDrEtergE aRt it aNIT ER - SAN FRANCISCO CA. 94111 3. For FAA Use Only • • • 4. Unit Idenbfeation . 11 Type Unit Mite Model Serial No. ENS Allegation AIMS/4 ' MS ti• NW wove) XX POWER/I-Oa .. PROPELLER APPUANCE Type • . I. Canfonnity St.te'wca A. Aroney'e HAM and AWNS ft Kind of genet C. Canifiewa No. Z 11.1.C—ertecated Wenn.< • • AP 1864049 \ - LANCE -A. MATTESON . ' 2407 EAST SHEA BLVD. . PHOENIX, ARIZONA 85028 Fan. Canaan° Lot-n.4 ' Congesiad Remo Simon Menotarkeee . D. .../ I comfy thattWi101it andimaltanton maw to me °win ciontareo in non • now: ono oltalloa on too . ererseoraltacomeus onto Pave been made in scoivtlarca with the tileenceineKAS a Pert Cot the U.S. Federal Aviation Finulations and that mile inlormation . • furnished herein it trims and cornea to the beat of my Way/ledge. - Dee — 12/27/89 --- Eismatontol t........— i . . 7. AppenW fee Pan. roterviceSupt . of Maintenance PurSuant tO Ole atietentr Peen Pimae specified below the unit Melded In Ilan 4 erne inspected in the manner orescnbrel by the Aeounistrwor or the Foam ANolke Arinistrabon sore X c APPROVED 0 REJECTED FAA FILSiondatds Instlede44 Manutoceat 2 Ic . Other (SPOT/ InedeCbco AuthOnZabOn eV : FAA awn* . spur Station Anon Approval byTningerl Canada AirmOrthinala Group Date of Approve or Ropcoon ConNoote or Dosignatal No. / 2-27.4? 526705494 FAA Form 33) At. • SDNY_GM 027641272 Michael Donnell SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFIA_00241194 EFTA01326787 FAA AIRCRAFT' REGISTRY CAMERA MO. I N DATE: 10-23-90 'NOTICE • rea.giu and balanCtOf ore. sang amaahon chendee quill be angled mine appmpitata fulcra: t record. An afternoon must:* compatage with au preverica atm 'ie.ons Ao attute continued conformity wan Ina app4e4ble Stewart hin•SS 100010 111011/. I 046600100 of 060 HI win t1tC4106100110 space As mewed inethetilettionet snails ;Sway with ancsala hation>lity end reptsfrab0n mark anctOent croft DECEMBER 27, completed) 1989. cpizsiltAx AEROSPACE CORP. (GAG) MODEL G-IV. s/n 1085 N88GA, Aircraft Type Certificate Data Sheet Al2EA. REFER TO: FAA APPROVED STC No. SA111NE, dated November 24, 1982; GAC. Maintenance Manual ATA Chapter 49; Garrett Turbine Engine Company, INSTALLATION HANDBOOK AIRBORNE AUXILIARY POWER UNITS, TURBINES 31-0251A Second Edition. e>33 -... The purpose of this ?Iteration is to provide a separate sourc - cooling air inlet that is entirely separate from the compress° inlet, thus precluding the possibility of cooling system starvation and, any, interaction between cooling airflow and compressor airflow. Inatalled A new PATS FAA PNA p/n 430206-9 LOUVER assembly ontcpthe APU's inboard enclosure wall. Attachment was accomplished with S each NAS1103-3 bolts: 5 each AN960C10L washers; 5 each MS21059-L3 nutplates that.vere attached with 10 each Ms20427M3-3 rivets. • Fabricated a blanking plate using 4304 Stainless Steel 0.040 inches ' thick that vill cover the existing p/n 3708913-101 flame arrester. Installed the blanking plate to cover the original compartment inlet source using existing har4vare. Secured APU compartment.. Performed operational test of Auxiliary Pgwer Unit using the procedures contained in the aircraft's FAA approved Aircraft Flight Manual and noted no abnormal or unusual operation before, during or after the operational test. Returned the aircraft to flight status. No flight manual revisions or su?plements were reguired -Or-thAtaIied as a reIblt of thin altaratior￾It . has been determined that the interrelationship between this change anC any previously approVed configUration will' not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to, consideration that the design of the APU compartment and accessory cooling arrangement will not allow fire migration into other areas of the aircraft thru the use of a fireproof check valve and an identical louver has operated satisfactorily since .2982 one G1159 aircraft and since 1984 on a GI159A V5GF aircraft. The effect on the aircraft's weight and balance report is negligible. END OP TAIS- SHEET" "no additional sheets are attached ❑ Add, tA503/ Streets Are Arlalled SONY _can 02754273 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 Ems'* 0024 EFTA01326788 Yak AIRCRAFT REGISTRY . CAMERA NO. 3"41 DATE: /0.;23-',0 • 0 . . • 0/413 .21200CCO . MAJOR REPAIR *100 ALTERATION of Oecomen For FAA Use Only Oterecorine (Airframe, Powerplant, Propeller, or Appliance) Mai Padteh•Sa Ateelebinette e Identleateht 59- F5D0 - 1.1 INSTRUCTIONS:Print or typo ell emnes.See FAR 43.9. FAR4i Appeams EL enp A. -13.9. 1 wa teeetwent revision thereof) tot tneeeehons . and ditposniOn Of MIS Item'. This tenon is mquirad tnitlw MAU S.C. 1421I. I' allure la reoretcan Mutt In annopenany nOt toexceedS1.000 'or etch yeti% wciatiOn 'Wean SO, Federal *moon Arlo! ,jaj. •—..— ' I. Akeratt . Nee . L GOLFSTREAM.AEROSPACE CORPORATION Mold GIV • • Sena' Na r 1085 .. Nationaltyandflegisuation HUM • N449GA 7_ Owner Namnr=i1118"ffigint CORPORATION "- citettaintigteriltili n • SAN FRANCISCO CA 94111 _ .1 For FAA Use Only 4. Unit IdendlleatIon r OVe • Nadel • l Roper Metals:a AMERADA --Th • deketted in nem I ' • CAI aporey PCNIERPLAIif rl PR9PELLER JAN 04 990 APPLIANCE Type - tAID-SOUT ATLANTApA. E. i F:S00 • laansdacturr, • A cennnety swam* A. Agoney's Nears and MIMS B. Kind of Arley C. C;rbeAllItio. US. Centeetea lehawee • GULFSTREAM AEROSPACE ?CORPORATION • . !nen CerutcalldIalquali GR4R216M P.O. BOX 2206 - TRAVIS FIELD Cenorsteo Aeon Storm SAVANNAH r GA i1402-2206 WalolettUre, . CA! seemlythat'll, repair andior alteration made to Dion hal itlentele0 In item 4 neon smadescntred on the revealor atiaehrnents hereto ben at" made in accordance will the teelterentents al Part 43 of to DS. Feoend Aviation Regulations and mat the information turnoned herein n. true and coma to ter beet 07 tort hlehafee0h. . ' hate 41. SOIWtire iel AuthOrhe 3 Irelledual • ' 12/01/89 • . . PATRICK J. LYNCH Ger...g • .......a... ... 7. Approval ter Return Ye Enke Puritan. to ine bt/Mority given persons speafied below. IM unn identified in Men a wee laseletteel Si the manner pr•SCebett by OW Administrator of dm Feders1 Aviation Administration and is X3 APPREV.0 ['REJECTED FAA Alt Standards iltoaCtei I laaniAaelwer lOther (SPIelly) . insmiction Aumonzation • • I BY I i F" Deign". Repot StibOn T Pete AVOrched bY hlettOtel I. Senjoiiterwettlerellt cite.* I • ' (Mehl APPrOvill or thejeCtiOn 12/01/89* Certilleate or De4ignabon No. GR4R216M httAittire ol Atith0,40 labVidal •• PATRICK J. LYNCH Pa. • . ...--e.-4.. FAA Pena 337 neap ....II, • • EZt •(:410 SONY CM_02T54274 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241196 EFTA01326789 FAA AIRCRAFT FEGISTRY CAMERA NO. 3 A' DATE: 1072i-PO NOTICE Weight and balancer operating limitationchansesshal I be entered in the alitirOpPale airCraii recurs!. An alleratiOn must f. compatible with all previous alterations tO assure continued conformity with the applicable airworthiness requirementa I. OesalOCM of Wort ACMTIVIWVW • ill more space IS flptteol. 'Mach addosonal Sh•es. identity with aerial', nationality and reps:reit* mar' *AO Cate walk completed.) • ACTT: 153 HOURS ACTL: 93 LANDINGS REFERENCE: GULFSTREAN AEROSPACE CORPORATION WORK ORDER NO. C04-108&2089-4486. 1. • INCORPORATED GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGES LISTED. NOSE GEAR DOWNLOCK SWITCH BRACKET (RECOMMENDED) 1000-1059 GROUND SPOILER HYDRAULIC, PLUMBING MODI 1000-1109 EXCEPT 1039 A/C - WATER SEPARATOR DISCHARGE - TUBE INST1N 1 LG/NLG & WHEEL WELL COMPONENTS-REWORK/REMOVAL (PT 1 - 6) MODIFIED NGS FEED BACK MANIFOLD, 5150-3 TO 5150-5, UNIT PER DOYITY ROTOL BP 05100 AND GAC DWG 0 1159L40400, 50 DI AND D2 PER MOO., ALSO MODIFIED NOSE WHEEL STEERING UNIT, 1159SCL200-41 TO 1159SCL200-43. • -END￾SDNY_GM/12T5 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFT/1_00241197 EFTA01326790 FAA AIRCRAFT REGISTRY CAMERA NO. ? A DATE: 1J-23.90 . _ DEPART Len OF 57 at 0, 41.10601 11WISPOIRATION—FEDS:12/ . AVIATION ACYJNISTRAIION • STANDARD AIRWORTHINESS CERTIFICATE INATOWITY 2 wayeACTIAWRA,OOODO. 4001AOT 1 4 ZAMICA. 111.04,114 4.4.1.41.5 • 2085 Inseam Seal mom-arvomonmasico asuma Unto. • *Nal O.-rano tw roar AWO.A.a.091514AuriOorAg sane onOo....on secrat ur...-Oe....c no Leen au. ag to to. Li Po rot or.A:06. awl> re +=role. to la • cowman ras Tl toe.. to Iwo ••••••• Dr....ma inirtoorolitron...7.42144•1.‘toon•dorato.teOn•noS••• ••• Cr...' .O A.:zoo. MKS n moo owe. Lavin GRs no COO Una.,vuWam.yFY **an PI 7.P.W.r. OM • 0O4ri It Sault[! a• •• • •••Z• ; • • • • ••••• •••••• • arrow as agai ve ann.% ThoOur.• ft.o.win.P00 OOP.Ore• iltly••• • iry. ooet•a•WA.......,0 7.16W• 11.03.:44et W v•Onost•••Onn4 • r•O'A•2 O.r. i OA i s iaii r toity. vs .( 444— DISIGYA WOW ..7 t• ...,Aigt;".4.40L......eao cnitOomay WU...OW In etalg ibio•CAaO :40 c.op.. .N., .......;•.••••••03 r MP AR- VOW intro I ,..a Y tea O.* CIRFOICAlf musl tm oommnizo at '.1 ANCAAIT OA AOODOOAM,O Oen. . 0000M; MEAN Aviacir ottootaroCea • FAA Fawn 8100-2 mmh Gam tn.' 04 vr￾SDNY 027S4278 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241198 EFTA01326791 ' FAA AIRCRAFT REDISTRT CAMERA no:3 N DATE. t0-2J-F0 • SbilY 6402754277 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241199 EFTA01326792 WADTAMN MiSlike-a • DEPARTMENT°, TRY.SMATATION —FEDUIAL AVIATICOIADMINISTWips1 • STANDARD AIRWORTHINESS-CERTIF(DATEI , stWirm WALOCTUPOI0.0140EL 13 30000 IOW I • CaG.:av apd. •P‘Pat I MP N4A86A 'CULFSTREA11 / G1V. 1 1085 (TRANSPORT !.1 A911.0;01, AK 1 MK. 'O *SWAGE • • • Th........wousenicapts...•espwramer•••semeanoosicief tt recs - 4•10, 13.1•011W (41•440.1.,.• ..we 0.030 t-W2 sateen npsoreane 110003* M ton tellam Vette . Is b• 031401 IP uw awnett /Atha te .0•0•••10 eta VW MpareaWat =WWI wwwww• aM wars •nornang c, trevas• J ra NONE • Tema kaccacenons M.W. POW ialana laWWW11 OPOOC PI 10.3.300 fa it 01010•0 fp AWWWW. fa PWILIAN4 OP00/* eigIne Wow Pe nanny. ilweflaf cianunano. w.• !MOWN WICAPIO CCOWNIPIWPW•31 0 arcOnttinawil Cytaaseareatcr.n•fournente.....tec Vain DATE 0 , SalolfaCC Of-9424.004.0villa 16 DEC 88 VI F.. L VA • JR. bMIR ACE 1052 I AP!0.03 owfaCtal In elmiceentawnarttnanearay•WInnfillieen3S 1101cogrowcw-nm.menCf0 r•••• CfstiFiCalt WT Mt INSPvivra IN 704 har-A0/ n. sCCOADAPett nit. arta! riCan 33300.03tefe-ATIOPS - FAA Form 8100-2 042. • ••• - , . • • . • SDNY 0.4:027§12i8 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241200 EFTA01326793 FLA AIRCRAFT REGISItt. • CAMERA NO. 3 N DATE: 70-23-90 • ',Z.\ • !'s • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241201 EFTA01326794 PAA AZACILAPT REGISTRY CAMERA NC. 3 # DATE: — 23 90 O. - . u1Dirsons MAJOR REPAIR AND ALTERATION orerresonain (HInnume, POiterplant, Propeller, or Appliance) Asisseaes. *arms. " Form APPremr4 • OMB 2120-0120 ..• No. • . • ter FAA too olaiv OtSop lesteNtatIon 5.01— PS00 INSTRUCTIONS: Pant *MP'S,' entries. See FAR pg. FAR 43 Appendix tang AC 43.9-1(ortoesseemeArreilier. tenon ter leSeuilhoesT anemspolillon el ells for re4Thiareport is frawhed by nra tag U.S.O.1421). Failure to Ripon an mutt In a chll penalty nem* execs:MA/0 ' foe each such dolalion (SecnOn Sal federal Menke Mt of 1966). . t. Alma MMus GULPS/REAM AEROSPACE CORP. Node G-IV . , 1085 : . Flefinnelitt and Flegetradco SW' NBEIGA . • ' LDS Mane (As Mean on ANN0NANA coliNGINN BA LEASING A CAPITAL CORP. Addnes (As shown on regisaarion cieretteffe) TWO EMBARCADERO CENTER SAN FRANCISCO CA. 94111 A.• No FAA we 00/ • S. Typo Ural Mae Model renal No. Reiner Anersiken AnIFRAME ' i Orsonbod in nom 1 abOvel XX (A S I PR0PD.LER ' • . I—..— • • Menutacearer S. Confortetty Stalarosat C. Grooms A. NooncriNorno and Aldan* • LANCE A. 2407 EAST PHOENIX, B. Kind of Agency : No. MATTESON . SHEA BLVD. ARIZONA 85028 X US. Colofraist I ilbref *Mc . AP 1864049 • Pomp on:nig:4 iihicianic Ownliciten nest Siouan Want Uttar D. I cirelylhat the reedit androt anion made totne un IN) klentified in item 4 'bon and deecribed collie or atteehineets hereto hare been made In eccordanca wren ht ine nen of Part 43 of the U.S. Arians the information Waned heroin in and correct to bed ol mytugowledgo. DO, .- Z(V0-117 • f 'Supt of Maintainer.. . T. App.:miter Plan To Sena Pursuing Aderanletrator Br biltiiiiittnOntf *An 0041441* 0 444144I tenni in/iBrin klignnrinil In IP44i 4 wn4 Inslineled in the manner plegaited he me of the Federal Ariadon Adirefelatrehan end es net APPROVED 1:1 REJECTED FAA nt.Siondures IINC4CW . M anufactufer leil ., lothenSprory/ Inspactan Authorization 4 . FM Designee Reedit Sulam Person /Wend SY Tra, l3c/n Canine Ainsoninnen ....sr EssoolApprovaleratelectiOn 11- 1 0 751 Certificate or : , Designation No. 526705494 Signature of AellhOnted r ici c-Nortgazir----- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00241202 EFTA01326795 `Cyan FAA AIRCEAFT REGISTRY CAMERA WO. 3 N DATE: 10-23-90 'd NOTICE Weigh: andbaMnceoroptttllfl'g tamsiation ctian pea sMllbe entered in the appropriate aircraft record. Anelleralionmust be compatible. with all previous alteationS to man comintilM conformity with Ma applicable airwOrthintss requirements. IL Descriptor% el Work Accompisind More space is required. Nisch addelional slyest Identify with aircraft nationality and nogistraton mark and date work completed.) GULFSTREAM AEROSPACE CORP. MODEL G-IV, s/n 1085, NBBGA, TC Al2EA. refer to: Gulfstream Aerospace Corp. [CAC], FAA APPROVED, Optional Aircraft Service Change [ASC] Number 87, subject: AIR-CONDITIONIN2 (ATA 21) Cockpit Display Unit [CDU] - Modification-, dated Octolird 5, 1989; GAC G-IV Wiring Diagram Manual, Drawing number 1159/140,71- effective for A/C 1060 & Subsequent, 30-2-1 Page 3, titled ENOIHE COWL ANTI ICE SYSTEM; note: this aircraft has GAC ASC 49 installer. The purpose of this alteration is to modify the Display Unit: [DU] fan circuitry to disable the fans when the pilot's, co-pilot'S, and Engine Instiument/Crew Alerting System [EICAS] display master stitches are all in the off position. This change also modifies the ?ewer circuitry for the display controllers [DC] so that th4y will not come on when the above switches are all in the off.positiol. This modification's design is only capable of disengaging the DU fans and shutting off the display controllers during ground 7peration. When the aircraft is airborne ASC 87's circuitry is locked out and the fans and display controllers perform their intended fwActions. Removed vire No. 2H31A22 from 318A1P10 n which is spliced to vire No. 2028E22 and then removed vire No. 2H28E22 from 318A1P4 X. Removed vire No. 1H31A22 from 318A1P9 GG which is spliced to vire No. 1H28E22 and then removed wire No. 1H28E22 from 318A1P3 H. Removed vire No. 2H31B22 from 318A1J10 n and vire No. 2H28D20 from 318A1J4 X and connected them together with a crimp butt splice. "Removed vire No. 1H31B22 from 318A1J9 GG And vire No. 1H28D20 from 318A1J3 H and connected them together with a crimp butt splice. The above wiring changes to the engine tool anti-ice circuits were done to remove unnecessary vire, connections and spices from the overhead console electrical assembly and free up electrical connection for ASC 8.7. Performed all of the applicable modification instructions contained in the above referred to ASC, steps A thru E and tested the ASC in accordance with the instructions Contained in steps Fl thru P20. Returned the aircraft to flight Status by recording compliance with this FAA form 337 in the aircraft's maintenance records, computerized maintenance program and retorting the ASC compliance card to GAC. ' • All parts that were were new and purchased from GAC Product Support. There will be no cockpiw procedural changes due to the incorporation of this alteration. ?Etre are -no changes to the aircraft's electrical load analysis. The effect of this efiange on the aircraft's basic weight and balance is negligible. ***end of this greet noCielhez sheets are attached *** 11/10/89 med*** \LI AtIdalOnd Steels MAaaclwd • k •ez:v - • ! sbNyG-040os2er SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241203 EFTA01326796 FAA AIRCRAFT REGISTRY CAMERA NO. 3 A' DATE: ;0-23-70 ;ll? v. - ' .r- /441-44%, U S COMMENT Of TRINSIVRTATION FEDERALAVIATION ADMINISTRATICN 4 t o.., I :'' - - -. MAJOR REPAIR AND ALTERATION (Airframe, PoweeMent, Propeller, et Appliane. r r .LA.. From 2a4m.r4g:::fpD. PI-!060.1 CS • FOR FAA CM ONLY OFFICE CANTFICATION WP-FSD0-I . INSTRUCTIONS: Print or type all murky Sn VAR 0.9. FAR 43 AppeoMit O. and AC n).9-1 lot tabromem envision Mena) for insumemins and or this form. . .. NORE . . . ICat • . -• I - rear tar e apar. 0. v . 1. SJK1AR I. Lone mm - - MMTIONAMM AND REGISTRATION MARA . . ' 1 Wit I vitCa 'NAAR 04mn 4W NgioNslion dwORRI6) ! M0INM SS (At Amin 9, molortrhon nnsignon) (Al 1 n I BA Leasing and Capital Corp. I The Bmbarcadere 0tr, 10th Floor CA 94111. 3. IN NA USE Oi l I.13" Pi.. "‘""• 4. BIM lownionox S. ME Men a Atha , wow I ' SINu4 b. IMAM AttINI￾snow is I AIRFRAME N Am Apoied X a s. ,bon) POSVIIIPIANT . PROMS ANRUO43 nol 03•NINIMMIN 6. pommuun STOWE, ' A. AOSNCV.1 NAME AND ADOUSS L MNO Of AGENCY C. MINICAR NO. • Western Commander, Inc. '16301/Daily Drive ' Van Wuys, Cl. 91406 - uA. COMPKete aiNmwmE ROAD STATION RCM A.3S4IA,M. 3 LLAit 104110.. UNIIICATO ithOW4IC is - afroxANO IIIMI NOON A elounlfaCTIPUIR D. I catnip, throe the repel. sod/or Otermion made' to the lank la ideotiMMI in ices 4 Awry sad desnibed on the man or MthetthilM3 Mono Lim beet made in accordance with the nnpairemems of Put 43 of the U.S. hilinst Avian.. Resubdoes . ad that the WkweestIon (*unshed Moneta Is tree Ind corm, to din bog of m knowledge. DATE . PAM m , September 8, 1989- - 7. AMC At KM REIM 10 SaViCE room" to the eelbeelffirmtel. Pun Dee optui6ed below, the unit :Manned is item 4 ruktsgted W she mum, pmeribed by . the AdtaInieautor d dm Mail ANatio* Administration sod is APPROVED RFJRCiFn the "M UMMA* Pala ... .;;Jithyilyeth beiPICTONYAIS/A11011 0101 pee*, ST rnt Mice a OM POOR Coltat. Manisa 0 1Weilthrt PIVECItht Don OP artoteL OR Marriott cattocut a - • DESIGNATION NO: RE or AOTMOMZE 0 INGIVIOUAL • e 9-8-1989 114 21 . ....Y FAA Farm 337 tt-en 71;ori, ' Walt. • ;p t.• • SONY CM 02754282 o _ SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241204 EFTA01326797 • FaA AIRCRAFT REGISTRT: • . "CANERA.NO. 3 M DATE: 70-2J-90 Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration-must be compatible with all previous alterations to- assure continued conformity with the applicable airworthiness requirements. 6. DESCRIPTION OF WORK ACCOMPLISHED (It more ';Paco is required. attach additional sheets. hientify with aircraft nationality and registration mark and date work completed.) Custom interior installed in accordance with Gulfstream Aerospace . Report t1159C-GER-023, Revision 12 dated November 14, 1988 and the ;following reports as listed in Consulting Aerospace Engineers, Inc. reports approved by DER INN-442 and Aero Interiors, Inc., Drawing IAI-G-1085 dated August 28, 1989. The following major components installed per the reports and specifications as listed: 1. L/H Bar Installation CAE AIN-52-2 2. R/H Galley Installation CAE AIN-52-3 3. R/H Fed Crew Galley CAE AIN-18-3 4. T.V. Entertainment Installation CAB AIN-38-8 5. Vanity Cabinet Installation CAE AIN-41-4 6. L/H 6 R/Ii Stereo/ Storage Cabinet Installation CAE AIN-41-8 7. Bulkhead Installation CAB AIN-33-26 8. 539.75 Bulkhead Reinforcement 6 Net Inst. CAE AIN-GIV-1 9. Aft Toilet Service Panel Installation CAB AIN-GIY-2 10. Floorboard Replacement CAE AIN-GIV-4 11. Water containers 6 Pedistal Installation CAE AIN-GIV-6 12. Aft Baggage Shelves and Net Installation CAB AIN-GIV-8 13. Drain Mast Installation CAE AT!-GIV-9. 14. Service Ladder lastalation CAE AIN-GIV-10 15. Aft Toilet Installation CAE AIN-GIV-12 16. Service Tool Box Installation CAE AIN-GIV-13 17. Seat Track Installation,; CAE AIN:01V-le Insullation and covering materials meet the requirements of FAR 25.853 Appendix P part 1 paragraph (a) through (d) as stated in Aero Interiors, Inc Report IAI-1085-FR-45 dated September 7, 1989 and substantiated by John Cale*, Inc. FAA DER-INN-682. Aircraft aligned on js-Les upon completion of outfitting. Equipment list and weight and balance reports revised. All workmanship accomplished according to A.C. 43-13-1A Chapters 5, t• 6 7 end A.C. 43-13-2A Chapters 9, 12 6 13. END f*vs do wimples nnnnn sia or nem 1.44.411-121 /AM° SONT_GM -2154283 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,_O and 17 EF-EA_00241/05 EFTA01326798 EFTA01326799 - FAA AIRCRAFT FECISTRT ' • CAK6',4 NC. 3 A' CAls: NOTICE • Weight and balance or OP00564 limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. DESCRIPTION Of WORK AMOMPUSHED (If more space is required attach additional sheets. identity with aircraft nationality and registration mark and date work completed.) Installed Cabin Entertiinment System according to WCI Dwg. $08069137 N/C dated 8-20-88, -'approved by DER 0N74-476. Video Monitor unit located at Horiz. Arm 142.0; other system components installed in cabinet at Horiz. Arm 172.0. System installation and Operation meet requirements of and complies with FAR 25.1309 Pare. (b), (d), and (g),. Far 25.1431, FAR 25.1309 Para. (a), (b), (c), and (a). Radio frequency interference check accomplished. System operation causes no interference with aircraft communication or navigation equipment. Television picture tube meets requiremegts of U.L. Report 01410. Aircraft Weight and Balance Report and Equipment Lists amended. All workmanship accomplished according to A.C. 43.13-1A Chapter 13, and 15 and A.C. 43.13-2A Chapters 1 and 2. END v.1. covensweier Iona rots of nCe isn-419.1:1/491.0 * e f t 9, 10, 15, and 17 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, errs 00'4) EFTA01326800 L I- IAA AIRCRAFT FEGISTRY EAMEFA NO: i X DATE: ;6-23-90 irse**Iti611 RE mm FEDERAL AVIATION ADMINITTRATICM ' STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION SERV:4190S • • • August 17, 1989 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION Nat MODEL NO% Gulfstream G -fr TTAD Data. Asa. MADDIATA a., Airplane ' • DANZ 3 a...DAV Nesternammandep, Inc Lin OF DATA . • IDENTIFICATION • WW1 Drawing. Number 408069137 NC' Dated 8-20-88 . . ' • . .Wiring Diagram - Cabin Entertainment System. -.- . - kt. • . `-... r. . . . • 'Vaal OF DATA • • To substantiate Cabin Entertainment System Installation in Gulfstream Aerospace G -IV. S/N 1085. ' maLicaLt Rauffitsaivs (La watt Rasa FAR 25.1301, 25.2309, 25.2353,..25.1357, 25.1359, 25.1431 • . • CERTIFICATION - Uglier sethoelty Al °mamas sat Pin ISA ium veld by &take al the Admisienter sad is ',conduce with coodIclete ad linhatleso of the retinal AvistIes ?kakis's,. dote Void elite sad cc attached theme osethonAl --- bees omaltted In accordion with wetabIlsiod preeedimeo and lend to comply with oppIkalle AwtotIett Repletion. Were! el these data them a. requInothons of the Faint II Foosonond I Nom Theroforo PI Amen SIONATuRECSIOFTAMONATEDIENGINEERINO /r REPReartAlTESTO DEPONATiOlt Hula MU CLASITFICATIOND Raigta •'NM-476 Systems 4 Equipment 7 John R.• Chambless ---._._• • • . • - _ • SESM_02754288 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241208 EFTA01326801 L FAA AIRCRAFT REGISTRY CAMERA NO. 3 N DATE: 16-23-90 --L.,...z. SDNY GM 02754287 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241209 EFTA01326802 `AA A.'3C AF7 REGESTRV ::---- L4 :1.ASERA NO. 3 N DATE: • . it_ ‘.••-i • . US DEPAMMOR & DIAIDR:MADCA • / FEDERAL AVIATION ADMINISTRATION ha. A ”.....je Pante WeeMe No 0.-S060.1 / 47 ' FOR FAA USE ONLY MAJOR REPAIR AND MSERANON (Althorns, Pewerplent Propellor, at Appliance),_, - ..._, 'OFFICE ODENTIOICATION g —L19 -O1 INSTRUCTIONS: Print or type all • he FAR 45.9. 44R 41 Appeadis S. sad AC 43.9 I 'tot valmeeptent teeision thereon ' he iniubmions aml diepoinion of mit (cent. oot Gulfstream Aerospace G -IV • "" ;MI I. NICAMT SEW/ NO. iNATIONAUTV AND itectswAson ?AMC . 1085 1 NSSCA 2., "I" NAME fee Aeon on e•444.0144 coliAtoft) Ifrstess (At 0~ an isegetfroNon aveihree) V Embarcadero Ctr, 10th Floor BA Leasing and Capital Corp. AD ' an Francisco, CA 94111 . FAA Dar • - A. OM/ IDNIMCIA0S $ nn LAM Aaal I Haw u0. ten."' VIM .non ' - I X AIRIIIAME (4 domeetnef atmml POWERPLANT I floras Me APPLIANCE anwPAC711.• 6. HAIM DATUM A. AGENCY'S NAME MO ADOILSS I. KIND Of AGENCY C. CERVOICAN NO. _, 41..... 04110C4IIP rI(WOIC Western Commander, Inc. MIMS CIIIII10.1.0 mICOLINC REPAIR STATION :4121 16300 Daily Drive I. CiensicanO tttttt moth. A.344.t.-1,2.4.3 • LI, A &I Van Nuys, CA 91406 sAinleatryatit D. I way that the '<AAA and/or al lea merle to the unit's) identified is Item 4 shove and hicribed on the reverse or casehmence berme Ian hen mode is accordance with he requirements of Pen 4) of elst U.S. NUM Aviation Repletion) mad that the futaisbc4 -herein 1, inn • 4 conga to the ben of eny AsoAlt4Se. DAR September 7, 1989 SIGNAT 1OF AUT/4O1IGLO INDIVIDUAL Z i : ..--, 7. APPROVAL F WOO TO CUE Stuniam so tee asebotiry pen paeans specified below the unit 'derailed in item 4 was ins ed in the matinee prescribed by the Aeltnieshemot of eh Perked *antic° Ad/shimmies sad is GI APPROVED O REJ ss t . NA RI ID•044145 ~MOO awA4401.44A •41014404•141•444AtON COMO flowan lif Al MA ODidedet x Strom SINUICHv Rusanno. otembeEnt 0 MAIWOIT 8•1•10011 of VAR OP APPROVAL OR CUTIFKATI OR SIGMA OF AUDlowe,,, ,y.,..yd:...... i. ..„ RVICDON 9-7-89 .._.r DESIGNATION NO 64221 - ..e , D ny C. goicnham, Chief Inspector ...... .542er SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -S0N-C15, GS1-0-27and 17— EFlik_00241/I0 EFTA01326803 FAA AIRCRAFT cct,/,STRY. (..IMERA No, 3 A DATE: 10-13-90 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued con fomity with the applicable airmorthinass requirements. • 8. DESCRIPTION OF WORK ACCOMPLISHED Of more space is required, attach additional sheets. Alen* with aircraft nationality and registration mark and date sack completed) Avionic and Electrical modifications installed per drawings listed on Western Commander Top Drawing 108000012 N/C dated 8-8-88 and approved by DER 1NM-476. Installed Sundstrand Mark V Ground Proximity Warning System per data approved by STC SA218880. Minor deviations performed per Western Commander drawing 108069091 N/C dated 2-8118 approved by DER 0114-476. Installed Honeywell L5Z-850 Lightning Sensor System in accordance with data approved by STC SA238850 and. Western Comraadner Drawing No. 08069157 N/C dated 11-14- 88, approved by DER 1814-476. Installed De Yore Logo Lights per data approved by STC SA4749SW Rev. *3 dated 1-21-88. Installed a third Honeywell Inertial Reference System (IRS), a third Honeywell Plight Management System, NZ910 Navigation Computers (3), and a Single Honeywell VLF/OMEGA Sensor in accordance with data approved by STC SA3774NM. Flight Manual supplements provided and Equipment List revised. Aircraft weight and balance report revised. END • (LC GOVCOINI4Cier PM* TIM° Of nct• 1>IS.W.121/02.0 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,Y:o-k 15,bfil4211- and 17 --§bN EFTA_0024I/II EFTA01326804 rzt, FAA AIRCRAFT REGISTRY: CAMERA NO. 3 N DATE: iv- 2,.;p RFCE1VED FAA May : '- FEDERAL AVIATION ADMINISTRATION ' STATEMENT OF COMPLIANCE win' THE FEDERAL AVIATION REAULATJotti August -17, 1989 AIRCRAFT OR AIRCRAFT COMPON INT JOEKTIFICAT101. MARC Gulfstream NODEL NO. G -IV Ty re (uma....n.a..H.riamorn, N.: N Airplane NANA Or APPLICANT Western Commander, Inc LIST OF DATA . - IDENTEDEATION TITLE entwing Number 408000012 NC , Dated 8-8-88 • • Top Drawing G-IV Sill 1085 - N • PURPOSE OF DATA - To substantiate electrical and avionics modification in G -IV Aircraft, S/N- 1085 only. APPLICABLE MEOW (Lie. Anne antAm.) FAR 25.1301, 25.1309, 25.1353, 25.1357, 25.1359, 25.1431 • CERTIFICATION • U.S.. Jodie of appolytwyonsider Pan 113 ban teotid by /Erection el de Adstiyiairytot cad Is acenduce with condition-sad limealloae of be Fetal AChaloo Ragslathey, data listed att. end ea numbed obest• elieberod byes cashed h steatite. with ostabIlyhed plocetres sad head to tooth .1th applicably Avalon Rogoletleae. • approval el than deet these dais roopleysysta *I the Festetill I Oat news. FillReopened Amen 'TOMATO/1th/ OF DISIONATE0 MINI UAW) REPRO:ROAM= DEROSATIOW PILIYIBERSIT) CLASSIFICATIONIR . _ - .NM -476 ' 'Systems 6 Equipment i i....erip,z,.......7..i.s.t /-John R. Chambless FAA Form 8110-3 till-101 31.IPERSCONS PREVIOUS COITION. SDNY_G0.4_02754290 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241212 EFTA01326805 FAA A IRGRAYT REGISTRY CAMELS -No. 3 k DATE: ii:-23-Co SDNY_GM_02754291 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241213 EFTA01326806 !AA AIRCRAFT REGISTRY, CAMERA NO.3 le .DATE'. 70-23-90 • ••••MS.. . • 710er, . y e ' US DINATIVAMT Of. RISKSPOUSIICot ' FEDERAL AVIATIC41 ft sANISIRATON — Est A W.04-1000.1 • MAJOR REPAIR AND ALTERATION Vnif FSL70 FOR FAA USE ONLY • (Aldrome. Poweadant, Propeller, or Appliance) *., OO G CENTIFICA IA —O1O TION INSTRUCTIONS. Plias os 9.pe ail be ;win. See FAR 43.9. TIRO Appcndix Sad AC43.9 I Ica tobantwat m um Smog) iestrunions sod dispern of this fora, • I. WOMB MA Aerospace I mODN. G-IV • . S AL NO. !NATIONALITY AND PROISTRATION NARK 1085 I MEGA 2. "IS NA.ol IM shwa on tesonnntan mAifsecA0 ‘ LODRESS (AS itomm w• roptiennke ontiAtole) BA Leasing and Capital Corp. two Embarcadero Car, 10th Floor . /San Francisco, CA 94111 3. COI FAA USE. OKI 4. NIS IONTIFILAIION S IIII VIM .. mail m0Olt NOY MO. -AM a4 1 0. non mytuit •••— r - (Al allesdnet n item I wen) POWIIIPIANI • •. PROPRILIN • ' • ANUANCI TM MAMO/MOVel 4 LOSMIsITESTATIABIT A. A0414CrS NAME AND MOMS I. MHO Of AWACS C. CERTIFICAD NO. Western Coisznandel, Inc. 16300 Daily Drite Van Nuys, CA 9.1406 U.S. Corinscans .1Oissiele ROAM STATION #472I An A 1'0,13 IA. A & P IOUS. OMMICATI0 a/PSC A cern/Kane tent nano« •••enecniur D. I candy Mat dm mole antUot dictation made to dm ileitis) Noodled is item 4 above and ataibtd as the nevem or tastharatou sod Innis betebets made its stasedanoe sibthe tennimmenas of Pan 43 of the U.S. fedora Avinies RaSulation: that Or kforamalie ("NAAS hamin is ran and conga to the ben of my knosoledge. DAM. AUTHORILLO INDIVIDUAL :September T el 1989 . ., . „„-- e. _, .. .1 7. *MOM POI MUM IS SttinCE do Eris AdosiolaneSt to des AschoAry p•bb persons speasetbdo: the oak AcessiSed ' item 4 wee Uspaad I•the envier presaihed by of the Ideal MatitH Admibintstima sad is pi APPRAD (^ RS) TID . . faa a ifiveaS .40yobowlyy IHMKTOMMMOOMZAMOM One Owe*) : .F1. . • • to.COINTROR - , x NNW States. • CAMSOmM Oftakbobet ot rturIPOIT IMI•KbOt Of ✓ . CAN AMORAL OS CERTIFICATE CS ' eaSKINAriON NO I VONA RE Of AUTMOV(O • ....IN"2 . a .....) 9-7-439 _ f_ • #4221, • Dafaa-1 1-A t C. --- n C. =ham, Chief Inspector W320) •..% • - BDNY_GM 02754292 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241214 EFTA01326807 L FAe AIRCRAFT REGISTRY '74MERA NO; 1.4TE: 10-23-90 NOTICE alteration Weight and must balance dr operating limitation changes shall be entered in the appropriate aircraft record. An applicable be compatib:e with all previous alterations to assure continued conformity with the airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED 7f more space is requh'ect attach additional sheets. Identi ly with aircraft nationality and registration mark and date work completed.) The following modifications were performed in accordance with Elsinore Aerospace Systems, Inc., engineering reports as listed below: 1. Skyphone Antenna Installations Report 41-24 dated 10-26-87 2. 43 Comm Antenna Installation Report 41-19 dated 07-28-87 3. Pressure Bulkhead Feed-through Doubler Installation - P.S. 85.5 and P.S. 596..0 Report 41-22 dated 09-16-87 4. Auxiliary Radio Rack Installation Report 41-23 dated 09-09-87 5. Ice Detector Mounting Installation Report 41-14 dated 02-07-87 Above reports approved by FAA DER 4N/47492 and #NM-494. Weight and Balance Report revised after completion of modification. END C • FAA AC/141•4 • O •COTIOtml. SICE1S PAZ ATTSCHLD GOVCIPOICNT PromTING or ma In, -eiss tritaozoo SDNY_GM 02754293 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241215 EFTA01326808 FAA AIRCRAFT REGISTRY CAMERA NO. 3 4' DATE: 10-21-9° I :sit RFtn\f - O FAA FEDIALAvisro==1; STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 19 JULY 1989 AIRCRAFT OR AIRCRAFT .. Slow/A. IDENTIFICATION KA'S - moan... r---.:7-.--'-r--- r ""400W vaVLAIHAM G-IV ( AIRPLANE i COMMANDER, INC. - • LW OF DATA OVITICI.TATIO. TITLE •ELSINORZ pOCUMENTS: .DOC. 1-14 • REV. A DOC. 1-22 REV. NC DOC. 1-36 REV. NC DOC. 1-66 REV. NC STRESS ANALYSIS OF ICE PROBE MOUNTING INSTALLATION SUBSTANTIATION - PRESSURE BULKHEAD DOUBLER INSTL 08068007 - 08068008 SUBSTANTIATION - NO. 3 VHF ANTENNA INSTALLATION • SUBSTANTIATION - PEDESTAL MODIFICATION INSTALLATION .... • (DETAIL DESIGN AND STRUCTURAL APPROVAL ONLY) .""mEDF w"A TO SUBSTANTIATE INSTALLATIONS IN LISTED DOCUMENTS FOR G-IV AIRCRAFT S/N 1085 LopLicsoLe mmv. an, NNW. on.....? FAR 25.3,03, 25.305, 25.301, 25.561, 25.603, 25.607, 25.609, 25.615, 25.769 CERTIFICATION • Cedar meant, vaned 17 discus al Se Arisistswarm sad a magmas with sodium and ianteurwe el eppaisaast Wits Part Mot Se Foie& Aviska Raptures'. Is. Goad Oise sad eci surmised Sens moire ed --- kis ben embed S steteedeaco MA asaalOsieed ponders ad lend ter semi., whb applicable ngeimemsto el dm Featal Ailaidee RepUtims. MReasoned approval tithes data I Opt Then km =Approve ase Su ROmMtuRMMOF DESIONATIDINFANEESMO RSIONNUTWIM IDISMetATMA mASEAstMl CLASIFICAIMMO eFealc4, 1 I NM-494 I, STRUCTURES . ROBERT E. POTEET I . I I FAA Folm 8110-3 I I l•ft" • SUPZItlEOLS PREVIOUS CaTION • . . • ' SDNY_GM_02754294 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024J2I6 EFTA01326809 EAA AIRCRAFT RECISTit. CAMERA NO. i A DATE:- 10-23-90 SDNY OO2764295 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241217 EFTA01326810 Cal:17/1 SDNY_GM_02754296 FAA AIRCRAFT 220%N :it CAMERA NO. 3 f? DATE: •:0-23-90 R7-C:Ftir:r, . US. DEPAIRMIle 0/ TRANIPOTTATION • FEDERAL AVIATION ADMINISTRATION 7 Fa Aper, mod 8.4., Eats. Ns. 011.4060.5 MAJOR RIMS ALTERATION AND FOR FAA USE ONLY yet, , ,..:,‘,L,,, (Airframe, Powerplant. Propeller. et Applian?) Dina oepaincAnoN WnSOCT*2 INSTRUCTIONS, Prim et IOM eII retries. See FAR 435P.FaR 43 Appendit a. mid Ar.45.9-I lot memo:hang resibicsa lot kernsaions sad thereon dismission a des form I. /MGR mm,Gulfstr eam Aerospace ImCos. I G -IV Sam NO. .OrTATFINALITT AND REGISTRATION MARK • 1085 i N88GA NAM (4 Arms en fodffMs. 4•491NITAI !AODIESS Mother r mgetrenon ceetifer00 7.048 BA Leasing and Capital Corp. • trim Embarcadero Ctr, 10th Floor ;San Francisco, CA 94111 I. BM FAA DIE ONLY - I. INITMOMOTION S nn wen -a Mott I lam no. ',SAM "".. Atio. AIRFRAME Me *tease wo neen I Aso) X POWER/LAIN PROMO APPLIANCE SIIMI/PACTI/Ol • ' • A. NIT MINX: A. *Cerra I NAME AND. ADDRESS I Epee Of AGENCY C. CERTIFICATE NO. Western Commander, Inc. 16300 Daily Drive Van Nuys. CA 91406 MS artisans meanie %. WAIR STATION E4Ol AI & 4, R.I,2, 13 L-.I. A II i rowan cen ICA 11. 0404 c a Ct mane rum. neater. immumation : D. actschisme Len t* rho the repair aadior serration made to the lodes) identified in item I 444 and described on the re-Nme cm sad -Memo Ism been made in accordance mid% he requitemeno of Pan 45 of bt US. Meal Al. iii I i0O Ritzy Laic,' . that dm inreetamies foritialied beteg is we s 4 maven to the best a my knee ledge. DATE . . . September 7, 1989 SIGN At OF AUTHORIZED INDIVIDUAL ...c ./.24-rart-r3 1 7. ANIONµ 04 tElleaSEIVICI . WAdmisirauot hill Whet to the incleney of pna peneas specifies' haler the sem Identified is imis-4 eu inp.naa is the mass.resc p ribed by the Peden' Minim. AdsaMiseseers and pi, 4 AP PROVED la REJ itornACIven Partner ALMOMILITIOM ones isaew -adt• St IAA CIIMINIt x mu, w PSI Camemse Melfalta a W.01300.1 INIPICTeo DAIE•Or Mesa Ot I IH CeirOSCAre OA DESIGNATION NO . SKI se or sursOet,..720.0.ni #4221 ' Da ny C. arnham; Chief Inspector. II320) s: try SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241218 EFTA01326811 f FLA altitid.F.T.RECI.STiY. 1 CAMERA NO. 1 N DATE: • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED Of more space is .required, attach additional sheets.- Identify with aircraft nationality and registration mw* and date horn completed) Repositioned Emergency Park Brake Control and Flight Control Power Shut off Valve Control in pedestal. General location remains the same, (forward, left hand side). All of the GAC Park Brake Installation remains the same, with the ex￾ception of the cable being pouted in a different manner at the pedestal The GAC Flight Control -Power Shut off Valve installation remains the sage, with the exception of: 1. Factory handle (PN11591240386-1) replaced with a modified handle made of stainless steel materiel. 2. Connecting Rod Assy (handle to lowei control arm) P/N 1159F20780-11 replaced with modified rod made of stainless steel. Both handle and rod replace original parts made of aluminum, and have been modified to allow handle to be pulled up and aft instead of up and. forward. ' • Soth Emergency Brake and Flight Control Shut off systems function and operation remains the same. Rifting and system functional checks performed in accordance with Gulfstream Maintenance Manual, Chapters 27-0-2 and 32-4-1. N • All workmanship performed in accordance with AC 63.13-1A Chapter section 1 s 2, Chapter 5 & 7.Section 1. . . This modification has no effect on weight' nd balance. END ..-....o.s."Ge.vcotrokuty_•"temila w nee ne. 45. 1211.° 24° - - - . - . SDNY GM_02754297 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241219 EFTA01326812 max: ILA 4/ AIRCRAY: iEGISTRY i I' DATE: ;0-23-'3 0 sc. •:••• US ocookluens or titeithWATIOrr • rCOERAL AVIATION NRAINISTRATI0N ' , MAJOR REPAIR AND ALTERATION - ' (Airfromo, Poworplanb Propellor, or Apeliancie)• ' For. APP•rid &Agee Dana No or-Ro6o.i FOR AAA USE ONLY 0/1KI IDINTWICATION ANSTIWCylONS• WPPSD04: Print or type an twin-- Sn EAR 43.9. FAR 43 Appendix B. ad AC 43.9 I for tubsequens revialoo thereon - for an te...Tien. and disposition of this tarns . I INCLIST -..,, . . iateXf Gulfstream Aerospace L'CvAruota: a Grrr-IL I 8 Mint NO. 1085 mo' IsmAerv, MAR[ I N88GA ?Oaf (Ai she...,. reeparolies cortidtaeol I ADCOKS$ LOWE, IBA Leasing and Capital (As Ana esrogithogion antAtele) Corp. ITwo Embarcadero Ctr, 10th Floor I Wecli I San Francisco. CA 94111 MEOW • 4. Uhf IDEFMAIIINI u.i S ITN r.Y1 shoot I mouno. tent. oval amp AJVIAA.1 . ' doeastird - • X -. (A. sons labors) • POWUPIAM isoreurA • AMINO IWO sieurVOACTUOUI A. I. ry AMBIT -ACiffeal NAAR NC /ZOOM B. RotO OF AGENCY 1 t 5 .-- , C. CERTIFICATE Western Commander, . Inc. 16300 Daily Drive Van Nuys, CA 91406 U.S. O147.1C4Ite maCKANC tour. STATION 44221 A.3 & 4,R.I.E.83 L.EA & P - Porto. cinecore ...awn X artirsCARD Walt nohow oamowenr• . • D. I certify Oat du repair endsot detrain rook to the .......5) starlit.. to aces 4 stave and described on the reverse or intscheares beano have bog made In secordaiore bids the tequiteibent of Pan 43 of Ihe V.S. Federal Aviation Regulatinai nod that the information OAR. furahibed herein is ton sad roam so the ben of any 1; 600 44 4. . September 7, 1989 SIGMA E Cr ALITM040&i.. WINVIOUAL Purses do ET 7. MEOW FOE IIIIIIII 'WOKE co des eueborierioven prow aprairs1 Sky cbt unit 'W io item 4 naizigted ia the maim prescabod by Adsoltileageoe of the Federal Anode. Adaiiouunion sad is go APPROVED OMt P" Kr' naWP A" *MOOR WaNACTUMS ,.../ eareerceeAlfireeS;1O.4 011•4I l_4J MA MOM! X SWAM SWOON Onsaus DIPArlan 01. 11.0010.1 04...004. OAT! OP 04 APII.0XAL OR REACTION ,r 9- 7729 ' CERTACATE OR DIDONATION NO - :4221 OF ALITMOSIZIDIJAItte t„.... j . C.:-. M Paull A] v-0m ban C. rnham Chief Inspector . . • -- • . • 02754298 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF-EA_00241220 EFTA01326813 FAA .IRCRAA.,. 7Z011,511a CAMLEi NO. 3 p 'DATE: lr.- ) 3.-90 Weight NOTICE aid balance or operating limitation changes shall be enterer/in the appropriate aircraft tabard An alteration must be compatible widi all previous 'Herat:cos to assure continued conformity with the applicable airworthiness requirements. . 8. DESCRIPTION OF WORK ACCOMPLISHED (ff more spice is required, attach additional sheets. ldentifywAhaircraftnationalityandregigtradonmarksiddate workcompleterf) Complimiiiith the following Gulfstream Aerospace Customer Bulletins: Alert Alert CB CB 45 44 - AOA Stall Warn Computer P/N 96S-00,41-03.4. Alert CB - Engine Fire Extinguisher Systems/Check. 46 - N/L/G Forward Truss Brace Assy. A/N 1159I.M40802 Custoter Bulletin 46 -1 Customer Bulletin - Brake by Wire F.Bal P/N 6004903-2. Customer Bulletin 48A1 - FOB Terminal Lug Inspection. 410-- Inspect Outfitter Flourescent Lighting Incorporated Changes: the following Gulfstream Aerospace Aircraft Service - ASC ' 48A 43 Aux Windshield Power Heat - Temp Sensor Test Switch - Install - APO Fs.ry Test - Improvement 413 APU Starter Drop-tut Light 497 #49 Cockpit Air Cond. Display & Nose Compartment Fans - Replace 4110 Elect. - Cockpit Temp. Sensor Replace/Relocate Display Controller €119 APU Shut fl & 42 Wiring Modification -down Modification 4122 Take off Range Warning Ind. Switches 4132 E Battery Wiring - Adjust Modification rnsmalled Phase 2 Wiring per GAC Dwg. 41159SE42038 Rev. A dated 4-10-89. END C IAA AC /14•1114 ❑ ADOMONAL SHEETS ARE AnACHED nve.covemmewrommilwaArnct.OS-M-121/4020, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241221 EFTA01326814 FAA J.:SEE:at FECISTRY CAMERA NO, F I DATE: 1E-23-90 VS CEPARTeetert CA TRAASPORT --"ThASI- ----_; —Miorrem••• FECCRAI. AVIATION ADMINKMAUON • t r. v • - ' : -. Eider &am S.. 044060.1 • MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY .. (Abframo, Powerplant, Propellor, or Appliance) — DANCE IDESIVICATION • l7P-F5D0.1. INSTRUCTIONS: Print or type 'II mine, See MR 0.9. f ta 43 Appetit& R. aid AC 4).9 I Cat for inateaspano and diaptamoori of taanoiatftt revision ihmon the nem. • 1 I. MO NT mk"Gulfstream Aerospace imam I G-IV • , SERIAL NO. INATPONNITY AND REGISTRATION NAM( 1085 i N88GA 7. OWED NAME In New nu regietration arlifeade) !ADDRESS (At Amm en rosiseratitei corMomN) BA Leasing and Capital Corp. ?Frio Embarcadero Ctr, 10th Floor $an Francisco, CA 94111 3. FOE FEE USE OIST • 4. UNIT IDEIMIKAtt01 S TOE we, We moon Num ma. ware mret. area AIR/MME • I X (Au Ancand a An than) POWIXPIANI PIA2481111 • APPUANC1 nn •SMVICIVI99 4. DEPLOY STAT017311 A. AGENCY'S MANX AND ADDRESS S. (ND Of AGENCY . V.I. ClIng1CAnD anKaNte C. CERTIFICATE NO. Western Commander, InC. raglian Cfna.C.An0. .4CM•riC LIME STATION #42.2I 1 16300 Daily Drive r a oni..c.ne Mail ..... Om ie3S 4.3-1. 7r 43 !rd•A Van Nuys, CA 91406 sui....1.0Vent D. I fortify &at the repair tad/ot Al ttttt ios made to umebannta betno be.. bent We in &swim& midi tad dial the isformatia• furnarbed herein is rive sad the %man &nand io utgli 4 above and &scribed on the evert as the requireamots of Pan 4) of O. U.S. Total Minion Reftvletion3 Rouen to the Nn of my knot Mast DAR • September 7, 1989 SIGMA Of AUMORIZ20 INDIVIDUAL e ..,, a-----/ „ANIMAL Mt MUER TO ME der PiANIIN4 Admialemot to, dm motheariey of meta persitto sPerift4d below the mit iprosifird is imm 4 was ins ad ia the manner prescribed by the Paine Aviation Admiaiatenion tad it cE APPROVED REJ . f IT PAIL se itmebatty trOPIC701 pappartite& • OrKIR 509,0 ....:1 arancncee•OTFONIATIOM PIA MOM x Wu. sumps • CANAbtan prneogan pruarep00 SWIM@ 0 , DAIS OP APPROVAL 011 LENCIION 9-7-89 CERTIFICATE Oft DESIGNATION NO 24221 VONA Of' AUTHOR? INDONJUd a td ‘ zin j D y C. F nham,..tgief Inspector v.n 11320, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241222 EFTA01326815 FAA AIRCRAFT 1LGI5Tky cAmERA NO.. 3 At -DATE: 1D-23: 00 • NOTICE Weight arid balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all. previous alterations to assure coot, rued conformity with the, applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date sock completed.) Installed Smith Industries Standby Altimeter/Airspeed Indicator, P/N WLM101AMS-1, TS0 ClOb and C2b. This indicator replaces the factory (GAO) installed Aero Mechanism Standby Altimeter and Airspeed Indicators and is connected to the same standby static source. This installation conforms to Gulfstream 0 -IV Outfitting Interface Specifications, IliV. 2, dated 11-14-88, Section 7 and FAR Part 25 Sections 25.1323 and 15.1325: Aircraft equipment list revised. C ruvt•nwr 0 ADDITIONAL SHEETS WE ATTACIED it OA. 00.100/00.FT.PINNTING Cor sact: tm-its..aiteatte _ _ . SDNY GM 02754901 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241223 EFTA01326816 FAA. AIRCRAFT REGISTRY CAMERA NO. Y ,v DATE: ;0-ii-90 US OCOMciaMT Of IWISPORTATErs FM/A AVIATIONAONINISTPADON i5 Paw GAIDTAT:".71NA IliIal ,:. MAJOR REPAIR AND ALTERATION -' FO K FAA 0$! ONLY (Airframe, Powiaploni, propellor, or Appliance) pia • r 3,...i... ONKt sKinott 111P con 4SDar ': INSTRUCTIONS: ON Dative's/is end Prins diseAsition or type of all casein. She FAR 43.9. Fill! 45 Appall Dad AC 433-1 (iir subeequent revision Gess!) this font . ' I. krun Au ' MOOS sgCulfstream Aerospace I ' D701V . , • SOUL NO. INttIONALITT AND RECASTRATION MANS • . 1085 I NS8GA 2.00k3 tardefar Owen an sonesRericee .wades) !ADDRESS (As Jaen in neavosen ortriRcoro) ?Two Embarcadero Ctr, 10th Floor BA twilling and Capital Corp. ken Francisco, CA 94111 • • 0II • . 4. Mot INR7IIKATIOR S. ME mint ••••••1 .000 I Uiro•tr.O. awn Ana. I X ( rieweesf obees. POWEIPLANT ' J MMUS APPLIANCE • ansivraell ..- 6. (01006111/ STAIDIERI A. AGINCCS NAME AND App[![[ II. UP. OP AGENCY C. CERTIPICATE NO. • VS. CIIMPICATID aftliatelK . • Western Coomandeil Inc. , pen CIIIIICATIO MOIAMC WAN STATION 16300 Daily Drive. A Gensscanti rinse Hefei A,3 &4.2.-1,2,113 L.I,ASP. Van Nuys, CA 91406 Annettcwne D. I certify au she repair sisdnri jeered** aide to sttsehoserits Mine Uses here ark is *Gardena Ala sad that Etta isles...lice Asririased hangs Is inn sad Ow uollig) islestifseri is hen 4 shove sad described as the nen or he requires's° of Pan 43 a Si VA. Pah& Aviatige Rarektieny cents, to Elbe best of my Issowlerigh DATF Septedber 7, 1989 PONA RE Of AUDIORIMD INDIVIDUAL . • G. ...." . .7. AMOVALFOR IETUIN 0 Malt ft vat to ibe simony ono penes* eperified below h, sari id/nailed is i® 4 esamigzied is she =Snail preecribed by the Adokriseror of sty Nide& Atheism AdaisArystio sad is (3 APPROVED CLEW1 4e NA 49 NINOITOCANd , ' shuliP9Citleet - IMPtC1.00.a.M406,2AT04 cost inacrl . -.sr, •. 411.• r Y via MOON x ISIGISISIDes candwe Otrallet7 01 Sala NPICRilt a / DAROP APPROVAL OR 4 DESIG s 9-7-89 • cannNAon a - TION NO 14221 . . SIGMA 0 nt"cirrlia..41,../a..„---) D y C. w rnham, Chief' Inspector- - • .. • SDNY GM_02754302 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241224 EFTA01326817 . so.PCFAFT P.EGISTRY IAnitA NJ. 3 A DnE: '0-23-9O NOTICE Weight • and balance oreperating alteration must be limitation changes shall be entered in the appropriate aircraft re:c-d. Aa compatible with all previous applicable airworthiness ',iterations to assure continued conformity with the requirementx 8. DESCRIPTION Of WORK ACCOMPLISHED (If n-ore space is required, attach additional sheets. Identify with aircraft nationality and registration marX and date not* completed.) Installed Oxygen System in accordance with data approved by STC ESA.4416NM amended 11-13-87. Top Drawing SAI-G-32862:005 Reit 0 dated 11-16-87. Operational Test Performed, Weight 6 Balance and Equipment List amended. Flight Manual Supplement SAI-DIV-1012-02-001, dated 11-13-87, provided. All workmanship accomplished according to A.C. 43.13-1A chapters 2, 5, 6, 7, IT; 13 and A.C. 43.13-2h chapters 1 and 16. . V.5.. co VCMYEMI Pfbn T.C. Of fICt 1166.41S -1:'.'.'v SIDMY GM 02764363 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241225 EFTA01326818 SDNY GM_02754304 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00241226 EFTA01326819 • FAA AIRCRAFT REGISTRY CAMERA NO. / DATE: 3- 2c - 89 (cm Owes! 0 APPLICATION FOR • meSTMAIIONI Pas to wane in Micie eat MA — Sao atm/hese a ass. &or {slin gbastatso FLA awns Nal2040/1 WICM•1117.1 .111•Walmorl kr alinellip AIRWORTHINESS as ••1••••r CERTIFICATE Ore spiciatillgN pentescoapiablagell vt A ver as mama isstAlik•rod ofla N449GA LaillaWl lit•Lerf MA Mom GLIUSTREAM IL 411.01•111•Xti.COVOnraw GIV 4 Ala% 1988 11 ' 94.... AC, 7O1Ic• • I/ .. , .0 1485 L eficukt ilitabirtioat Maw ROLLS ROYCE 7.,mcnicatoosanom O. MAMA. 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Etta Os u•Aawcentrc•710TAOAct ....curt • Newer .......sal I Cis IMAM ON Liar , i III I P•XvcreOtia•rr lilac • CLISIL•Aft02•10aTIATION C INST. I q IAA CAA A. AfroSTERID samcorrfroas$ Cin eon 10..••••OW "••••••• 0••••••••"••• Snore. Cadet' a ass, Oal4 Men., et ••••14... GI In... w'.••• ,9 VOWS% Cat= OCIM I ••••* GULFSTREAN AEROSPACE CORPORATION ACCOLIS P O. BOX 2206 SAVANNAH, X GA 31402 .....*:"Arlaantavoil.4.141Caicliespoorraamegewoomnintanstom € X •a•pari are Saar. WO. Ns C•704 OK Mt C•201.C.ATI WM Pal MVO MI . Al2EA REV. 1117 X abliffiarnetlitettrirttrOwo ••• Ana) • 88-24-16 • or °Sams AP a un••••• ow...roma I N/A PAOU:111•11•4 rat C iDtt. an N/A C.••••ainn s VC •••••••• • C. PACM.P1 OPIT•104 no masatramlA WWI= g X <mat 0 Waft el min uaMin TOT 45AL 5 0%.1 Wan MOWS • 5:03 ,I o ,...., ngaidertm. seven Oar He ton lir. s..• •••• ••••• N/A &a:IRS:Ana - i hoer wiry ••• I a •• mgerime este in• • •• soma ~Ye Nem ••• ••• ese••••••••• mg a Ian./ ••••••••• • Oa' Anton nay •••••• a.m. •••••••••••••••• an c• Amscalnst 16 DEC 88 NAPA NC TPA ir••• • .an JAMES 0 WEST AGENT POIGCLOI• .a.---eta. 0- C410th • he •POWT OCianD JAW( my KM awn : C 7 a nap Kum namoirrsT I 2 22.2517 IC,sCaival• SO 0~ f 27 $001 SI ,22inpt IV OPthicAn rate res. 1_2 1 02m0CA 2...20.22Turtcmpae Ken 1 1 1f ffs2rwattbowia, trAnCso taw Links. i i I 6 4 anon loms•Cilaeolls• ft.. 00.4 • ' WI ITT< SiOSIUNC ••••••1a dads*, am • 4 A.••1 4 . 1 Ire Our •• x Tit CAMICATIIMOASTED ••••••••••••0 a SVEN. Iv tat ••••••••••••••• 4 •••:semen• Ca SOC•ne.an.›. Or Onkel g I a. •••••••• •OvollilistaiGt•nnt•Tz I> • AVOW let le••• •••• Seam • e =nasal IPA •iirECION I g‘t MANX ,.- li Oa LOCIER. j Wes I II!•AUI.Wousi I Fo.• us II tont I' 16 DEC 88 'WILT Oent• SAV-MISO-CE42 • " itAk, ../ .4 12 vi F. VAN DMIR ACE 1052 , JR.. . IAA 30.14•CTCSISKIMATIAL — SDNY GM_02754305 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241227 EFTA01326820 S NY GM 02754306 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241228 EFTA01326821 TM RY CAMERAAIRCRAFT SO. I REGIST DATE: 3-25_ 89 • enrcenutstarmapc. DEPARTMENT a 1RANSPORTATiON-41:01RAL AVV.TION A0IMNISTRATOI STANDARD AIRWORTHINESS CERTIFICATE re;ww.c z l••••••Crtoolli oaaril WI" • CATICOS %WM. N4496A I system% sty • Arror01•Tv "AO PSG FO• SSW= two onorron••••••••• on sue matron. 1•11mmIlesdpierscorrhislarermlakiroo. malltarlOraair• *PAW" re nor mod re ire. .- in Iowa to rar•••flo ar ••• ramie goo*. Y win cooloon • sob gores my rem .sr. bmn ore.. Coreormor ro •• Ina •4••loplea••• 100••••••••••• GNAW ii••••••• rioloro CROWS a.isorroarod Gonadial. nal Orl MIMI rest NONE a olir•o3 APO 0000, 06 We wove ••••••••1 0.1•••••• sari et a Wenn. am • Paso •••••••• My Pa hirramiralr. VS . km .•••••••c• r•••••••••••••••Ot orrorrord a Siam .1.1 sear Pell At OOPOOrawamarto••••••=marrotrlYat W I O. 6Suorol rum POMP ,16 DEC sa 1• • • a• ono inorotcooncoerha corilicso moo. roarrobriloo mei or Da ISIS CMS CatsMST ille••••••••••••• IMO Or ~en on ri•••••••VO mrool Pm riCcroLOOPOO SC MOW= lOr TM( ISOM" •IXOVJAMCI writ. •PRICaliLt =OW.. FM Fonn 8100-2 re 4 600 too .••• 4 - SDNY_GM_02754307 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241229 EFTA01326822 SDNY Gf...4_027 1308 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241230 EFTA01326823