• r' ""2"...S0a-57- .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 ad die 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

!I I 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. War Idanoticaaat ' 55 t --ff: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 AP 1864049 Foreign Certifie43 Meekank 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 of Ent 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 red leant . 4':c 7. Approval for Mora to Service . Parma (IS BY lode mita* Men persons specified bra, the adidentified in it= 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, FT w 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 . . (Airframe, Powerpiast, Propeffer, or Applinet) en %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 $1 SO0 for each such violation (Section 901 Federal Aviation Aa a 1931). I. Airmaft Nuke Gallant:am Aerospace Maki C.-W Serial No. 11025 144417aliaY red Regatta Mark NEC A, 2. One Nom (As town as registraext oroficeie) B A Leasing & Capital Corp. Addis (As town al roparsoco tati5cate) Two Embarcadena Center So Fr wart Ca 114111 3. For FAA Use Ovey t Unit Ittentifkatiaa 5. TM* Urtit Stake I Model I Serial No. Up= Abash Airframe (As clesaised io Mani Love) I PowpLant Propeller Appesoce Type Mau= ii. Conformity Swasett A. Amica-s's Name red Adam R Kid 0 f Araw C Cate No. LANCE A. MATTESON S.560 E. SAN FUME DRIVE SCOTTSDALE, AZ LAM X • U.S. Certifgemd Mechanic Ar *M441$ Foreign Certificated Mechanic 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 aircraft's 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

LAX AIRCRAPI EEC I STET ' CARERS N0. V. DATES 2-4 - 9 3 kin A•1." ... Oka Wo• 21.1.00) 'ID MAJOR REPAIR AND ALTERATION Far FAA Meat, es . .oasse Deree (Airframe., Powaplase, Propeller. or A Pr011occ) e ..........- ...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 of the 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 withaall 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 15,02 and 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@wner bdiv 4: 7 11.2,--Ca 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 operating limitatiov,:hangcs shall in the appropriate tart record. An alteration must be compstbk mit an previous 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) November 23, 1992, Gulfstream Aerospace Corporation (GAC) Model Sas( 1085, N88GA, FAA Type Catificate Data Sheet Al2EA. Refer to: AEROSPACE UGHTING CORPORATION {ALC) FAA Approved Information Bulletin No. 92-001, tided UPGRADING SERIES "66"FZ.UORESSITLIGH77NG SYS7ENS WITHAL -"I.2" SERIES LAMPS original release dated October 15,-1992. The impose of this change is to upgrade this aircraft's Cabin Fluorescent lighting System by =toting the existing ALC Series "66" fluorescent Lamps and Connectors and installing the ALC Series "12" Fluorescent Lamps and Connectors. The installation upgrade to the AL -12" Series Fluorescent Lamps on this aircraft eliminates the requirement of having to comply with Airworthiness Directive 90-14-06. Rammed the existing 14 each ALC P/N 6635.1220-25 cabin fluorescent lamps and 28 each ALC PIN 31.85.1A lamp end connectors and installed (in the existing motmittg clips) 14 each new ALC P/N AL- 1235-1220 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 installed parts are FAA/PMA approved and were purchased new from Aerospace Lighting Corporation; . 101-8 Cohn Drive-, Holbrook, N.Y. 11741; telephone 516-563-6400 and 516.563.8781 fax Berfonaxl System INS*CITON and CHECKOUT in accordance with paragraph 5.0 of the above referred to ALC Information Buie& and noted no abnormal operation of any of the cabin Fluorescent Lamps. ReturneA the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's mairlieTnce records. It has been determined that the intareli5orship between this change and any previously approved confvhcation wgl not hlreCitlett any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to, consideration that the FAA New York.Aircrall Certification Office has reviewed the information and procedures contained in the D3 92-001 and considers the AL "1r Series Lamps and AL-5113 Lamp Connectors to be acceptable; and Mavis= FAA approved Power Protected Unit 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 on a mgr. Amos WORD Z0; Med a CSAI.CLTS doc Paharl DctromnY. NO ADDMONAL wen 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- - Cwanallo. Dann 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. Meemb Nee 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 AP 1964•49 Fortran Certi6mtet1 Matta 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 1/2 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 on this 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 I Po. AFT V . j .E DCA]; Tr: F.I 17 1, 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 Pan 4) Me ti.S. Fettle* minim tha the intonation made m accordance with is rommeaems of of 4ultw ad 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. 4401POMYY • 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) "- se rata I a.sem i1/41•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 G-IV 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*BN4 Inetnlebone 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 rn fu ished he 4 trot and correct its the Deal of my nootedge. Date 3..4—/C4 —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 51/4 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. - 0 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 G-IV . 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. i1/2/01€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 .--..-. dintweedMO•nr) abort/ x awr.rwiwerre~wwwweat .• 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... 4 Hiosth=€(......... 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 neiartirlon certiticner 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 ales Dniotoitiesz.. Sep Authorized Ir, cO 4./._______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 installation . of ap auxiliary radio rack in this aircraft per Elsinore Aerospace Systems, Inc. Engineering Report #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 the configuration of that found in Elsinore Aerospace Systems, Inc. Engineering Report 1-52 dated 1/18/89, entitled "SUBSTANTIATiON - RH FWD AVIONICS RACK". This report has been FAA approved. 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 to be in conformity with the above mentioned approved data and continues to meet 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 umbid P NM, Cerielkuee Rini, Station • 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---"-t i ll FAA Fpm 937 Mier e. 0411: Iv*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 . dew bed in gent I shove) X wwwhiwmwwwrwwwwwrww.(As - 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 63 1 4✓'‘C.www.-47 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 Permaxticatisfy • 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 Genii-ate 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 ce Aerospa 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 espial lawn 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 AutitorlzedCa c laa..... 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 Suilowee Cmdcwaili r A. NSW* Name and Address Western Commandeer Int 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) . o BA Leasing and Capital Corp. ISan. Francisco, CACenter 94111 • . 3. Ied MA USE ONLY , t 7--- .--'''. CFA 1000. A O , .- / ... c S •Pj. 0 ebe, 4. WI I nuncio - scfril vv. ... ..... "Obit I Mat. NO. • Am MM. Amp. AIRFRAME *woof/ he; Mom) M. as I . 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 Immo ben been made la sccepdatme ith ,be requiemoonto of Pan 43 of the-US; Metal A t i tt ion Reeeladoet mid 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 flmostl omeeCtiemancouanor4 Ma 011.0141 x ItMili MOON .. alOtaui. NSW OP MieteCill BOOKTOt CO siOCull OM 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 0 ' • 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 on regIatinorminifleale) 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 uil/ • . 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 In026.3zz. al 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 M MIT aft's E 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 aryl xavicus~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 0 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 1 Mantdattwes - 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 pos Cangilca naltion e orNI. i 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 must be 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 21, 1991. Gulfstream Aerospace Corp. Model G-IV, s/n 1085, N88GA, Aircraft Type Certificate Data Sheet Al2EA. Refer to: FAA APPROVED Gulfstream Aerospace Corp. (OAC) RECOMMENDED Aircraft Service Change (ASC) No. 198 subject: AIR CONDITIONING (ATA 21) ACM (AIR CYCLE MACHINE) BYPASS SHUTOFF VALVE - ACTIVATION, dated November 19, 1990. This alteration modifies the air conditioning system to prevent the °COOLING TURBINE HOT' message on the °FICAS (Engine Instruments and Crew Alerting System) from annunciating when the aircraft is below 42,000 feet and wing or covl anti-ice is selected.- - Additional circuitry is added to ensure the air cycle machine bypass shutoff valve opens when the aircraft is below 42,000 feet and wing or cowl anti-ice is selected. Complied with installation instruction of ASC 198 referred to above. In addition, provided positive locking to the 8 screws that are required to attach the relay rail to the tail junction box (see figure 1). All parts that_xere installed as a result of.this change were new at the time of insta—lation and furnished with the ASC 198 kit that vas purchased frOm. Gulfstream Aerospace Corp. or comply with FAR 21.303' (b) (2)(4) . • • Successfully performed the ASC's installation checkout test. Returned the aircraft to flight status, recorded compliance with this FAA form 337 and ASC 198 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 wilt not introduce any adverse effect upon the.airvorthiness of the aircraft. This determination included, but vas 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. The effect of this change on tBeaireraft's basic weight and balance report was negligible. • • 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 to me 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 Ina Desiree' Ix lane, sums, Person raormai Tampon CANN I Aiiheifthitiel tie i 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 0 : • 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 • ' 1 Signature, 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 $" " lifea I luanitaton ' " / Inn ila01 I / _Y 1 I AA N yco" Ix ' Ammer sada, . -*low. The ;:n9Orleor*3 In item 1 wag bora' in ma "Wass cede a -APPROVED 0 ASJICTED I I inna-bon Autnodunion ICIon: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 II Product 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::.: • it tekk 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 Men I Wore) on 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 id K- • 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, 1 n 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 Reverser System (Sheet 2 of 2), page 3 dated August 31/87; and GAC G-IV Maintenance Manual 24-0-1 Page 5, dated August 8/86 para 10 Bolted Electrical Connections - Torque values. This ASC adds circuitry which ensures prompt thrust reverser deployment with 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 theme° for sennections sad &galantine d nib 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 • &weal (Ai 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 A3 Serilti,42f, & 3 0•10410401,0till 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 &teratd ies 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 . .... ame• 0 .,, tea 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: -- / 3/43- 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 ittie pr. 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 t NA ot-R060.i cfMtlete neentgrATON 1.,, _a ...n - MEW AvIATiON ADJAIKSTIATION .4.. r ‘‘' MAJOR REPAIR AND ALTERATION 0 -0 3 .a . TAPfroma, sowarplant, Propellor, or APP1h4F 5 FOR MA UM ONLY ONCE ofrancanoti . INSIRUCTIONS. Print al type ell ristlici. Stil FAR CS, PAR 43 ApPidna 8. sod AC 4351 les Abatement adios dash foe lostrealos sad dliposIdoo of 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 91406 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. I cotify that the npals end/or ahead°. somas to the waifs) identified is beta 4 above sod desalt.' es the tame ot east otats bent* be bees made Is ettoolsoce with the ageless' of Part 43 of the U.S. Metal Addeo R.gviedo. Nod 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 dada die ratted the odder prescribed by the Adataban of the Mad Analog. 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 .....4..c.o.c. 67 O.2%tes , ‘ Z 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 Weight and balance or oar ating limitation changes shall be entered in the appropriate aircraft •ecord. An alteration mint be compatibie with oft previous alterations to octane continued conformity with the applicable airworthiness requirements. 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),,,, ." 0 047 'FOR PAA USE ONLY • (Airframe, Powerplant, Propeller, or ApplioneaVaav 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 ( r‘ -j 0-Ill SERIAL NO. 1085 NADI:MAW( AND REGISTRATION A9/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 Le l. • 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 04 MA SanaTA , 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, 44‘ t - "N" q4aOfAtir 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/ . • 0 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 ci APR*•• • : 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 - . identified in tleM 4 twn inspeeted in the manna emcee by the Purloin, to the atahontY yetipens'absented belOw. IMt APPROVED - 0 REJECTED ACIII.MalratOf al the Federal Avow Administriban ono is 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 0 . MAJOR REPAIR AND ALTERATION al alarm. a kneroshof , (Airframe, Powerplant, Propeller, or Appliance) i . ildliSININSR 1 roan hltreved OW No.2120-0320 Por FAA Use Ordy 116117864ran INSTRUCTIONS: Print or type ell trees. See FAR43.9.FAR 43 Appendet El. endAC43.2-1(oesubeertuent . rerbionthereo0fOrInelructIons and dispowlien of nu 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 K 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 0 . 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 . liDestora,on 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 and tin *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 Irliellel TWO '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 3015 NORTH HAYDEN ROAD SCOTTSDALE, AZ. 85251. _ A VS.C.reseed44.41:Aarae • AP I664049 leareeGelikele04140IY A4 ANY Oirtecaleci Slaw 0. 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 or operating 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 she :Sniffy *Oh strati netionafity and agitelyttion rivek and date work completed.) June 27, 1990. Gulfstream Aerospace Corp. Model G-IV, s/n 1065, NEIAGA, Aircraft Type Certificate Data Sheet Al2EA. Refer to: FAA APPROVED Gulfstream. Aerospace Corp. (GAC) recommended Aircraft Service Change (ASC) No.. 170 sub: AIR-CONDITIONING (ATA-21), Cockpit/Cabin Temperature sensor power source-rebus, dated March 30, 1990;. GAC G-IV Wiring Diagram -Manual drawing 1159AV40103, DC POWER^ DISTRIBUTION, (sheet_1-ot-2) 2475-1, Page 3.,_dated annuary19/20k_ Military Standard MS35336; and MS51957: This ASC moves the power source ofcabin and cockpit temperature control system from the right main 28'Volt DC Bus to the essential 2U'Volt DC hue. • . . . Complied with all of the instructions contained in the ASC, except as noted herein: Wire P615AB14 was removed from the aircraft and discarded, a new vire was stamped and identified P602AF10 and connected between CH212 and 08292 and a MS51957-43 acre:, vas installed at CH292 connecting the vire, bus bar and circuit breaker together properly; Wire P603AD10 vas removed from the aircraft and discarded, a new wire vas stamped and identified P600AG10 and connected between CB214 and CH256 and a MS51967-43 screw vas installed at CB256 connecting the vire, bus bar.and circuit breaker together. properly; Wire P615AA12 and Wire P615214 were not removed from the aircraft. These deviations from the original ASC were done to conform to production changes that have been incorporated in aircraft s/n 1120 and subsequent and provide for•proper wire/circuit breaker matching; see:.FAA AC 43.13-1A para 429*, b., c. • . All installed parts were installed - new and comply with the appropriate parts of FAR 21.303 (b)(1)(2)(4). Succeisfullyperformed the ASC'a operational test, returned the aircraft to flight statue, recorded CoMpliance'vith this ASC in the 4ircraft's maintenance recordi, returned coMpleted compliance card to CAC. It has been. determined thatille Interrelationship between this change and any previousli, approvedTedefigOration vill.not introduce any adverse effect upon the aitiforibineei 'of thw:aircraft. This determination included, but was -dot limited to; (a) consideration that any deviations to the original ASC would not chinge.the intent, operation; or test procedures, (b) Aircraft quality vire vas-used that vas the correct size for the current reqUiremelitd,-operating temperatures, -and environmental conditions, and (c) the installed equipment will function in a manner that will not interfere'vitfi 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 • 0 • 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 Ra t 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 t1tC4106100110 HI win space As mewed inethetilettionet snails ;Sway with ancsala hation>lity end reptsfrab0n mark anctOent croft completed) DECEMBER 27, 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 K 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 Mai Oterecorine (Airframe, Powerplant, Propeller, or Appliance) Padteh•Sa Ateelebinette 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, • swam* A cennnety 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 I. Pete AVOrched bY hlettOtel 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 . _ 57 at 0, 41.10601 DEPART Len OF 11WISPOIRATION—FEDS:1/2 . AVIATION ACYJNISTRAIION • STANDARD AIRWORTHINESS CERTIFICATE INATOWITY 2 wayeACTIAWRA,OOODO. 4001AOT 1 4 ZAMICA. 11.04,114 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 • Tl cowman ras toe.. to Iwo inirtoorolitron...7.42144•1.‘toon•dorato.teOn•noS••• ••••••• Dr....ma ••• 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 1 1085 (TRANSPORT N4A86A 'CULFSTREA11 / G1V. !.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 t in h e nen of Part 43 of the U.S. Arians the information Waned heroin in and correct to bed ol mytugowledgo. DO, .- Z(V0-17 • 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 eapar. 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 X AIRFRAME N Am Apoied 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

I- IAA AIRCRAFT FEGISTRY LEAMEFA NO: i X DATE: ;6-23-90 ir se**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 • "" ;M I I. NICAMT SEW/ NO. iNATIONAUTV AND itectswAson ?AMC . 1085 1 NSSCA 2., "I" NAME fee Aeon on e•444.0144 coliAtoft) Ifr stess (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 1 OF 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.,.. i. yd:........„ 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-C 15, GS1-0-27 and 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. Fill Reopened 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 ;win. See FAR 43.9. TIRO Appcndix Sad AC43.9 I Ica tobantwat m um Smog) be 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) two Embarcadero Car, 10th Floor BA Leasing and Capital Corp. . /San Francisco, CA 94111 3. COI FAA USE. OKI 4. NIS IONTIFILAIION S IIII VIM .. mail m0Olt NOY MO. -AM 4 0. 1 a non mytuit •••— r - item I wen) (Al allesdnet n 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 Innis betebets made its stasedanoe sibthe tennimmenas of Pan 43 of the U.S. fedora Avinies RaSulation: sod 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 Eris to des AschoAry p•bb persons speasetbdo: the oak AcessiSed ' item 4 wee Uspaad I•the envier presaihed by do AdosiolaneSt 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 Weight and balance dr operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatib:e with all previous alterations to assure continued conformity with the applicable 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 I, STRUCTURES NM-494 . 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 FOR FAA USE ONLY AND 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 thereon lot kernsaions sad 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 • trim Embarcadero Ctr, 10th Floor BA Leasing and Capital Corp. ;San Francisco, CA 94111 I. BM FAA DIE ONLY - I. INITMOMOTION S nn wen -a Mott I lam no. ',SAM "".. Atio. AIRFRAME *tease neen I Aso) X Me wo 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. Len t* rho the repair aadior serration made to the lodes) identified in item I 444 and described on the re-Nme cm : actschisme-Memo Ism been made in accordance mid% he requitemeno of Pan 45 of bt US. Meal Al. iii I i0O Ritzy Laic,' . sad 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 ./1.24-rart-r3 7. ANIONµ 04 tElleaSEIVICI . hill Whet to the incleney pna peneas specifies' haler the sem Identified is imis-4 eu inp.naa is the mass.resc p ribed by WAdmisirauot of the Peden' Minim. AdsaMiseseers and 4 pi, AP PROVED la REJ itornACIven Partner ALMOMILITIOM ones isaew -adt• St IAA CIIMINIt x w mu, PSI Camemse Melfalta a W.01300.1 INIPICTeo I DAIE•Or Mesa Ot IH CeirOSCAre OA DESIGNATION NO . SKI se or sursOet,..72 0 0.0. 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-'30 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 WPPSD04: ANSTIWCylONS• 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'Cv Ar a uota:Grrr-ILI 8 Mint NO. mo ' IsmAerv, MAR[ 1085 I N88GA ?Oaf (Ai she...,. reeparolies cortidtaeol I ADCOKS$ (As Ana esrogithogion antAtele) LOWE, IBA Leasing and Capital Corp. ITwo Embarcadero Ctr, 10th Floor I San Francisco. CA 94111 I Wecli MEOW • 4. Uhf IDEFMAIIINI S ITN u.i r.Y1 shoot I mouno. tent. oval amp AJVIAA.1 . ' doeastird - • X -. (A. sons labors) • POWUPIAM isoreurA • AMINO IWO sieurVOACTUOUI I. ry AMBIT A. -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 furahibed herein is ton sad roam so the ben of any 1; 600 44 4. . OAR. 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. 04 OAT! OP APII.0XAL OR REACTION ,r 9- 7729 ' CERTACATE OR DIDONATION NO - :4221 OF ALITMOSIZIDIJAItte t„.... j . C.:-. ban C. rnham Chief Inspector . . M Paull A] v-0m • -- • . • 02754298 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF-EA_00241220 EFTA01326813

FAA .IRCRAA.,. 7Z01,511a CAMLEi NO. 3 p 'DATE: lr.- ) 3.-90 NOTICE Weight 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 CB 44 - AOA Stall Warn Computer P/N 96S-00,41-03.4. Alert CB 45 - Engine Fire Extinguisher Systems/Check. Alert CB 46 - N/L/G Forward Truss Brace Assy. A/N 1159I.M40802 -1 Custoter Bulletin 46 - Brake by Wire F.Bal P/N 6004903-2. Customer Bulletin 48A1 - FOB Terminal Lug Inspection. Customer Bulletin 410-- Inspect Outfitter Flourescent Lighting Incorporated the following Gulfstream Aerospace Aircraft Service - Changes: ASC 43 Windshield Heat - Temp Sensor Test Switch - Install ' 48A Aux Power - APO Fs.ry Test - Improvement 413 APU Starter Drop-tut Light #49 Cockpit Display & Nose Compartment Fans - Replace 497 Air Cond. - Cockpit Temp. Sensor Replace/Relocate 4110 Elect. Display Controller fl & 42 Wiring Modification €119 APU Shut-down Modification 4122 Take off Range Warning Ind. Switches - Adjust 4132 E Battery Wiring Modification rnsmalled Phase 2 Wiring per GAC Dwg. 41159SE42038 Rev. A dated 4-10-89. END C IAA AC /14•1114 K 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 taanoiatftt revision ihmon for inateaspano and diaptamoori of 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 r 16300 Daily Drive 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 PiANIIN4 to, dm motheariey meta persitto sPerift4d below the mit iprosifird is imm 4 was ins ad ia the manner prescribed by der Admialemot of 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? INDONJU d 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