I MAJOR REPAIR AND ALTERATION uS For — 6 Pgirtramd, Powerplant, Propeller, or Appliance) ,halt 'I • ' Onkel*, Form Approved OMB No. 2120-0020 FAA Use Only Office Identific2o22; _INSTRUCTIONS: Print or type all ntries. See FAR 43.9. FAR 43 Appendix B.and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of thirferTrii. port is required by law 09 U.S.C. 1421). Failure to report can result in a civil penalty net to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Al ft Make GULFSTREAM AEROSPACE model GIV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA, GA 30338 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity SlatomeM A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C AVIATION INC. 301 DISCOVERY DR. APPLET0N, WI 54915 U.S. Certificated Mechanic QK2R112L Foreign Certificawd mechanic X1 Cenificated Revak Station . manufacturer 0. I Certify that the repair andior alteration made tothe un fts) identified in item4 above and described on the reverse or attashmentshereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date DEC 16 1996 Signature of Authorized Individual 1.50-nitle,-te 4., 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is (1) APPROVED 0 REJECTED FAA Fit. Standards i Inspector Manufacturer I Other (Sandy) Inspection Authorization BY FAA Designee XX Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Remotion DEC 1 8 1996 Certificate or Designation No. OK2R112L Signature (loin. of Authorized Individual tlLZ2 FAA Form 337 .12 or SDNYGtvl02754102 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241024 EFTA01326617

NOTICE Weight and balance oroperating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished pl more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Installed a GTE/Magnavox C-2000 Digital Airborne Telephone System consisting of: 1 Ea. Air Radio Telecommunications Unit (ARTU), P/N 724855-801 1 Ea. ARTU Rack, P/N 724868-802 1 Ea. Duplexer, P/N 620317-1 3 Ea. Cabin Data Bus Repeater (CDBR-1), P/N 724864-801 '1 Ea. Cabin Data Bus Repeater (CDBR-2),'P/N 902205-803 1 Ea. CAS Unit, P/N 725256-801 1 Ea. Analog Interface Unit (AIU), P/N 724986-801 4 Ea. Phone Assembly, P/N 724866-801WH, -805PL, & -807PL 1 Ea. Antenna, P/N 902131-2 Two Global Wulfsberg Flitefone VI Radio Telephone Systems were removed to facilitate this installation. Removed components consist of: 2 Ea. GWS RT-18D Transceivers, P/N 400-0125-000 2 Ea. GWS WH-I0 Flitefone VI Handsets The newly installed antenna is located on the underside fuselage at FS 100 as per KCA Structural Drawing: Radio Telephone Antenna Installation, 1159-23-01-301, sht. 1, of which the structural aspects are DER approved by M. Lieblich, FAA DER SW-811. The C-2000 system wiring accomplished as per K-C Aviation Drawing: Radio Telephone, GIV-31085-23-98, of which the electrical/electronic aspects are DER approved by N. Kopesky, CHI-262. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conduc- tor shielded wire meets MIL 27500. All work done IAW AC43.13-2A Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END K Additional Sheets Are Attached GU.5. GOVERNMENT PRINTING OPPICC: It02-769-0I2/60I37 SDNY_GM_02754103 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241025 EFTA01326618

ir g 1/45-7 ! • • ' ' . ! I MA,JOR 1 6 I;TAiriniOi , • REPAIR AND ALTERATION , Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification. R ./.1 INSTRUCTIONS:Print or type :ties. Se•FAR 43.9. FAR 40 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions —enddisposition of thisiormitt rt is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty nol to exceed $1.000 tor each suc violation (Section 901 Federal Aviation Act of 1958). . 1 Aircraft Make GULFSTREAM AEROSPACE Model GIV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA, GA 30338 3. For FAA Use Only 4. Unit Identification 5. Tyr). Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERFLANT PROPELLER APPLIANCE Type Manufacturer & Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C AVIATION INC. 301 DISCOVERY DR. WI 54915 APPLETON, U.& Certificated Mechanic QK2R112L Foreign Certificated Mechanic XX Certificated Repair Station manufacturer D. I certify that the repair and/Or alteration made to the un Its) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information - furnished herein is true and correct to the best 01 my nowledge. Date DEC I 6 1966 Signature of Authorized Individual CFP6424, A t t , Z,e r 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the mariner prescribed by the Administrator of the Federal Aviation Administration and is 01 APPROVED 0 REJECTED I FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY I FAA Designee 111XX Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 181998 Certificate or Designation No. QK2R1I2L Signature of Authorized Individual C14,-. , ' *- ,_ FAA Form 337 .12 MP) SDNYGivl_02754104 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241026 EFTA01326619

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (II more space Is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Installed an Allied Signal Satellite Data Communications System (SDCS), interfaced to the existing Airborne Flight Information System (AFIS). The AFIS system is integrated with the GAC installed Honeywell Flight Management Systems providing complete flight plan and weather information through self-contained VHF COMM data link with the Global Data Center. The SDCS is interfaced to the AFIS and provides additional cabin/cockpit communication capabilities. Installed SDCS system components include: 1 Ea. Satellite Comm Unit (SCU), P/N 153-017311-01 1 Ea. SCU Antenna, P/N 121-017537-01 (Sensor P/N S65-8282-101) 1 Ea. HPA/LNA, P/N 153-017310-01 The SCU Antenna is installed as FS 265 in accordance with KCA Dallas structural drawings; 447-5338, of which the structural are DER approved by M. Lieblich, SW-811. The SCU is located in the R/H radio rack extension and the HPA/LNA is located in the R/H cabin sidewall at FS 250 on existing structure. Refer to KCA Drawing: AFIS/SDCS, GIV-31085-34-63, of which the electrical/electronic aspects are DER approved by N. Kopesky, CHI-262. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conduc- tor shielded wire meets MIL 27500. All work done IAW AC43.13-2A Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END 0 Additional Sheets Aro Attached *U.S. 00VCIIHMENT PRINTINCt OIPICI 1192-70-012/10157 SDNY_GM_02754105 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241027 EFTA01326620

rirc.-7,77 . i O., . 3M - 6 1.997M or won (Akira onmsan • , REPAIR AND ALTERATION of owerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identificaip2 i i INSTRUCTIONS:Print or ty en les. See FAR 43.9. FAR 43 Appendix B. and AC43.9-1 (or subsequ nt revision thereof) for instructions type a and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only ',The dna Ident if fed herein compiles with the applicable airworthiness requirements oral I. approved for the above described aircraft subject to conformity inspect in by a parsers authorized in FAR 43, Section 43.7". Date DEC 1 0 ME IAA Inspecte 61.13 4. Unit Identification 8. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described In horn 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive A ppleton, WI 54915 US. ceni Heated Mechanic QK2R112L Foreign Cenificated mechanic X Cenificated Repair Station Manufacturer D. !certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on t e reverse orattachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date DEC 1 0 1996 Signature of Authorized Individual 47-ser/V er,IZZ---• 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XX APPROVED CI REJECTED FAA Fit Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 8 1996 Certificate or Designation No. QK2R112L Signature of Authorized Incrvidual cap.,- • FAA Form 337 ono SDNYGlvl_02754106 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241028 EFTA01326621

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be conipatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Modified the previously installed Galley and Cabin electrical system by removing previously installed equipment and wiring and installing new equipment and associated wiring. Installed the following equipment: lea Nordskog HI Temp Oven P/N: 50231L. lea Microswitch Leaf Actuator P/N: JV-26. lea Rotron Fan P/N: FS24H3. lea Tappan Microwave Oven P/N: TMS083E1S0. lea Krups Coffee Maker P/N: Pro-Cafe. 2ea Grimes Light Assembly P/N: 34170-1. lea Audio Int. High Current Control P/N: MSM285. lea Audio Int. Aft Lav Switch Panel P/N: SPS-4-1-1759. lea Audio Int. Aft VIP Switch Panel P/N: SPS-5-3-1761. lea Audio Int. FWD VIP Switch Panel P/N: SPS-5-3-1753. lea Audio Int. Divan Switch Panel P/N: SPS-4-1-1762. lea Audio Int. Divan Switch Panel (Master) P/N: SPS-4-1-1758. lea Audio Int. R/H Galley Switch Panel P/N: SPS-6-2-1754. 2ea Audio Int. Credenza PSU Switch Panel P/N: SPS-3-1-1757. 4ea Audio Int. Passenger Service Unit Switch Panel (PSU) P/N: SPS-4-1-1756. 4ea Audio Int. PSU Switch Panel (Master) P/N: SPS-4-1-1755. lea Audio Int. Vestibule Switch Panel P/N: SPS-6-1-1760. Wiring for the newly modified / installed Galley and Cabin electrical systems is per K-C Aviation,Inc electrical drawings: Electrical Power Distribution (Galley Power), GIV-24-1085-100 (Sheets 1 & 2); Galley and Cabin Electrical Interface, GIV-24-1085- 110 (Sheets 1 thru 3); Water Drain System, Water/Drain Heaters (Digital Switching), GIV-38-1085-112 (Sheets 1 & 2) and Electrical Switching and Control GIV39-1085-126 (Sheets 1 thru 9). Structural aspects of the newly installed/modified Galley and Cabin electrical systems are approved separately. Existing aircraft wiring diagrams affected by the above installation/modification are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapters 1 & 2 and manufacturers installation data. Aircraft equipment list and Electrical Load Analysis revised. Aircraft reweighed. END K Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1112-761-012/G0IST SDNY_GM_02754107 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241029 EFTA01326622

li r , t& ment 6 ) f t , Oewo MAJOR . i ' twai.1 — 6 (Airframe); ' REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office identigption ttl~ OF I matklispositionof.thisloanahimapart for ..• 4STRUCTIONS: Print or type all envies. each such violation (Section 901 See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequ nt reviSiOn then:eel) for instructions is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not toexceed51.000 Federal Aviation Act of 1958). 1. Aircraft make GULFSTRENI AEROSPACE Model G-IY Serial No. 1085 Nationality and Registration Mark Ni38GA 2. owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only oThe dateallIIIIIIIIIIIrldentif led herein =plies with the applicable •Irworthinesa requirements and Is approved for the tows disarmed aircraft subject to cceiformi ty inspection by a person authorized in FAR 43, antigen 43.70. Date DEC 1 0 1996 FM Inspector CUM 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agencys Name and Addres B. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive U.S. Certificated Mechanic Foreign Cenificsted Meenanie I Cen Manufacturer D. I certify that therepair and/or alteration made to theun t(s) identified in item 4aboveand described on the reverse or attachments hereto have been made in accordance with the requirements of P rt 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my nowledge. Date DEC 10 1996 Signature of Authorized Individual e fewa4/A°' / 0-7..:, 7. Approval for Return To SeMce Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XX APPROVED 0 REJECTED FAA Eli Standards inspector Manufacturer inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 8 1996 Certificate or Designation No. 0K2R1121. Signature of Authorized Indivdual Catfrp.., c FAA Form 337 meat SDNY_Giv1_02754108 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241030 EFTA01326623

NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be corripatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Removed the previously installed cabin and lavatory lighting system and installed a new cabin and lavatory lighting system with Ordinance Signs consisting of the following equipment: 3ea Aerospace Lighting Corp, Lighting Inverter P/N: AL-0581. , 18ea ALC Lighting Power Supply P/N: AL-5112. 2ea ALC Lighting Power Supply P/N: AL-2000. lea Grimes Light Assembly P/N: B3550. 2ea Grimes Light Assembly P/N: 34170-1. lea Luminator Light Assembly P/N: L16256-1. 21ea Wemac Light Assembly P/N: 2520-3. lea Bruce Industries Ordinance Sign P/N: BR9206-907. 4ea Wemac Ordinance Sign P/N: 3585. Wiring for the newly installed cabin and lavatory lighting systems are per K-C Aviation,Inc electrical drawings: Feature Panel Lighting (Digital Switching), GIV- 33-1085-111; Overhead Cabin Lighting (Digital Switching), GIV-33-1085-122; Vestibule Dome & Boarding Light, GIV-33-1085-114; Reading and Table Lights (Digital Switching), GIV-33-1085-115; Ordinance Lights, GIV-33-1085-125; Lav Lighting, GIV- 33-1085-106; Cabin Aisle Lights, GIV-33-1085-102 and Cabin Terminal Junctions, GIV- 39-1085-128. Structural aspects of the newly installed cabin and lav lighting systems are approved separately. Existing aircraft wiring diagrams affected by the above installations are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets NIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAN AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list revised. Aircraft reweighed. END 0 Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: Illt2-769-012/60157 SDNY_GM_02754109 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241031 EFTA01326624

11.5 (q;1 ,• I.: V; i *; I. • US NII9OR - 6 gmrtnint • • REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Only Office Identillcati7Use ICISTRUCTIONS.Print .loadisposition for 1.." nes. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instructions is required by law (4(1U.S.C.1421). Failure to report can result Inacivil penalty not to exceed $1.000 federal Aviation Act of 1968). or type all e attlaisforro,Thittegort each such violation (Section 901 1. Aircraft Make GULFSTREAN AEROSPACE Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only *The data /a identified herein is approved for the above sneer ibad aircraft in FAR 43, Section 43.74. Date DEC 1 0 100$ FM Inspectorr ie r carpi fee with stasJect the applicable to conformity airworthiness requirements inspection by a person authorized 0u3 4. and Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. ngeneys Name and Address B. Kind of Agency C. Certificate No. K-C Aviation, Inc. . 301 Discovery Drive Appleton, WI 54915 U.S. Certificated MeChenie QK2R112L Foreign Coniticaled Mechanic X Certificated Repair Malian manufacturer D. Icertify that the repair and/or alteration madeto the un t(s) identified in item 4 above and described on the reverseor attachmentshereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date DEC 10 1996 Signature of Authorized Individual 101.04 /1,r,..11*.Z.:4 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below, the unit Identified In item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is =APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 1 8 1996 Certificate or Designation No. QK2R112L Signature of Authoriz Individual (14..40 s, - FAA Form 337 (12461 SDNY_GM_02754110 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241032 EFTA01326625

NOTICE Wert and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description ofWorkAccomplIshod Olmom spacers required. attach additional sheets. with aircraft nationalityandlegistralionmade and date work completed.) Removed the previously installed cabin audio and entertainment systems in their entirety and installed a new cabin audio and entertainment system consisting of the following equipment: 10ea 10ea 2ea 4ea lea lea lea lea lea lea lea 4ea 2ea lea 2ea 2ea lea lea lea lea lea lea lea lea Audio International Headphone Control Baker Speakers P/N: HF93. Quam Speakers P/N: 4C5Z8. Baker Subwoofer Speakers P/N: LF91. BBE Sonic Maximizer P/N: SM-4012. Collins ATR Rack P/N: 622-1196-001. Stereo/PA Amplifier P/N: M3070M. Archer Amplified Coupler P/N: 151116. Audio Int. Video Switcher P/N: VSSO4. Audio Int. Video Switcher P/N: VSS04T. Audio Int. Audio Switching Controller P/N: MSM2804. Baker Audio PreAmp/Power Supply P/N: M1084PS. Audio Int. Infrared Receiver/Transmitter P/N: Alpine FM/AM Cassette P/N: TDA7552. Baker 14" LCD Monitor P/N: 990-4110-002. Panasonic VHS Hi-Fi VCR P/N: PV-4662. Sony CD Changer P/N: CDX91. Sony CO Controller P/N: RMX59RF. Airshow Genesys DCU P/N: 920060. Airshow Short Mount P/N: 914026. Asinc TTD Controller P/N: 911010-2. Audio Int. Mouse Switch Panel P/N: SP-450-1. Rosen 6.4" LCD Monitor P/N: RLCD64-1-1ACB. Rosen Power Converter P/N: RISR-28-12-6. Panel P/N: HSP-037-1. IFR9A-A-38. Wiring for the new cabin audio and entertainment systems is per K-C Aviation,Inc electrical drawings: Cabin Audio, GIV-31085-23-61 (Sheets 1 thru 4); Cabin Entertainment, GIV-31085-23-62 (Sheets 1 thru 9) and Airshow, GIV-31085-31-52 (Sheets 1 & 2). Structural aspects of the newly installed cabin audio and entertainment systems are approved separately. Existing aircraft wiring diagrams affected by the above modification/installation are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAN AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list revised. Aircraft reweighed. END K Additional Sheets Are Attached *us GOVERNMENT PRINTING OFFICE: I992-769-011/60137 SDNY_GNL02754111 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241033 EFTA01326626

. -=--.- 1' vs mere f• Ilmn s II a 6 I-Cir:,(A . fri t I • AJOR REPAIR AND ALTERATION es Powerplant, Propeller, or Appliance) I Form Approved OMB No. 2120-0020 For FAA Use Only Office Identilicfroni3 INSTRUCTIONS. Print or ry --anddispositionPi form. This for each such violation ( 110n entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions al El I eport is required by taw (49 U.S.C. 1421). F Ilure to report can result in a civil penalty not to exceed S1,000 01 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAN AEROSPACE Model G -IV Serial No. 1085 . Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. AddreSS (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Us* Only •The identified herein the and data/FS complies with applicable airworthiness requirements is approved for the above discribed aircraft abject to conformity inspection by a person authorized in FAR 43, Section 43.70. Date DEC 1 0 1996 FAA Inspect . GL13 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As deserted in item I above) X POWERPLANT • PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated mechanic 0K2R112L K-C Aviation, Inc. Foreign Certificated Methanic 301 Discovery Drive y certificated Revak Station Appleton, WI 54915 amubOwer D. I certify that therepairand/oralteration made to the un have been made in accordance with the requirements furnished herein is true and correct to the best of my knowledge. t(f) identified in item 4 above and described on the reverse orattachments hereto of Part 43 of the U.S. Federal Aviation Regulations and that the information Date DEC 1 0 1896 Signature of Authorized Individual odoe. 4Y/ent-- T. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is )(It APPROVED 0 REJECTED FAA Fit. $IBMard9 Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Dateof Approval or Rejection DEC 18 1886 Certificate or Designation No. RK,R119L Signature of Authorized Individual C20w-wr c 16.-: FAA Form 337 0240 SDNYGIvl02754112 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241034 EFTA01326627

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircral t record. An alteration must be coMpatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. identify with aircraft nationality and registration mark and date work completed.) Modified the previously installed 115 VAC 60Hz Conveiter system by installing new outpu wiring to the existing galley circuit breaker panel and adding (6ea) new 115VAC outlets per K-C Aviation, Inc. electrical drawing: 115VAC 60Hz Converter, GIV-24-1085-147 and Utility Outlets, GIV-24-1085-146. Structural aspects of the newly modified 115VAC converter system are considered minor. Existing aircraft wiring diagrams are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapters 1 & 2 and manufacturers installation data. Aircraft equipment list and weight & balance revised. END K Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-M/60157 SDNY_GM_02754113 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I035 EFTA01326628

i)N(e-'71 • -,- i PI J.:40 — 6 l'.;:: ,t MA OR REPAIR AND ALTERATION o (Airfr# , Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification A. -4//_.; tidnumtromm - —4 • INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for instructions and disposition el this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only •The data, identified herein complies vi h the applicable airworthiness readrements rd is reproved for the above discribed aircraft subject to conformity irapection by a person authorized in FAR 43, Section 43.7a. Date DEC 1 0 1996 FM Inspector • C- - - 61.13 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X . . POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. K-C Aviation, Inc. Drive 301 Discovery Appleton, WI 54915 U.S. Certificated mechanic QK2R1I2L Foreign Caelificated mechanic x oolitic's«, rt.pattsumto,, Manufacturer O. I Certify that the repair andlor alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date DEC 1 0 1996 Signature of Authorized Individual c 6,..3„.47,e,"Z:e-.... 7. Approval for Return To Service Pu suant to the authority given persons specified below, the unit identified in Item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XXAPPROVED Cl REJECTED FAA Fit. Standards Inspector Manufacturer Inspection AuthOdzation Other (Specify) BY FAA Designee A Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection DEC 18 1996 Certificate or Designation No. OK2R112L Signature of Authorized Individual 570,--- t d —IL FAA Form 337 112481 SDNYGIvl02754114 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241036 EFTA01326629

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (It more space is required. attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Modified the existing electric toilet system by installing a new Lav Switch Panel P/N: SPS-4-1-1759 per K-C Aviation,Inc electrical drawing: Electric Toilet, GIV-38- 1085-101. Structural aspects of the modified electric toilet are considered minor. Modified the previously installed electric window shade system by installing new wiring and new passenger Service Unit Switch Panels per K-C Aviation,Inc electrical drawing: Electric Window Shades, GIV-25-1085-127. Structural aspects of the newly modified electric window shades are considered minor. Installed wiring for (2ea) new electrical adjusting passenger seats per K-C Aviation, Inc electrical drawing: Electric Chairs, GIV-24-1085-129. Structural aspects of the new electrical adjusting seats are approved separately. Existing aircraft wiring diagrams affected by the above modifications or installations are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list and weight & balance revised. END K Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 166x-766-01L6016T SDNY_GNL02754115 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241037 EFTA01326630

I ; i \ .. f C l uS4in:crimen :. . illiVOR • - REPAIR AND ALTERATION Powerplant, Propeller, Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only ? 6 r,cyxAi rt Airnirisnotion e, or Office IdentifiesIon in 6".Z.1-, J I) INSTRUCTIONS: Print or type a - anddisposition of thiSform...112dreport for each such violation (Section I entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for Instructions is required by law (49 U.S.C. 1421). Failure to report can result in &civil penaitynot to exceed 51.000 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE Model G -IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) COCA-COLA ENTERPRISES INC. Address (As shown on registration certificate) 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only "The data. (dent if fed herein cowl les with the applicable airworthiness requirements ard is approved for the above described aircraft subject to conformity inspection by a person authorized in FAR 43, Section 43.7s. Date nFe 1 n 1005 FM I i nspectr,, - SI.13 4. Unit Identification 5- Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer S. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. K-C Aviation, Inc. . 301 Discovery Drive A ppleton, WI 54915 US. Certificated Medtanic QK2R112L Foreign Certificated Mechanic X Certilkated Midair Station Manufacturer 0. I certify that the repair and/or alteration made to the un t(s) identified In item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is trUltand correct to the best of my knowledge. Date . DEC 1 0 1996 Signature of Authorized Individual d.sesmi.A°7 7“. 7. Approval for Return To Service Pursuant to the authority given persons specified haw, the unit identified in item 4 was Inspected in the manner prescribed by the • Administrator of the Federal Aviation Administration and is X APPROVED 0 REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Dale of Approval or Rejection DEC 1 8 1996 Certificate or Designation No. QK2R112L Signature of Authorized Individual 'gen,. FAA Form 337 id.ed SDNYGIv1_02754116 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I038 EFTA01326631

NOTICE Weight and balance oroperating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is ICQUired, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Modified the previously installed Cabin Call System per K-C Aviation,Inc. electrical drawing: Call System, GIV-33-1085-124. Structural aspects of the modified Cabin Call System are considered minor. All work done TAW AC43.13-2A chapter 1 & 2. Aircraft equipment list, Electrical Wiring Manual revised. Aircraft reweighed. END O Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: t992-769-012/60157 SDNY_GM_02754117 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241039 EFTA01326632

L. . \--. . MAJOR REPAIR AND ALTERATION nw 3 0 'Airframe, Powerplant, Propeller, or Appliance) msm .I..:> • fowMm j n Form Approved OMB No. 2120.0020 For FM Usa Only Office IdentifiZ 1.. fri INSTRUCTIO • ' tries. See FAR 43.9. FAR 43 Appendix B, arr AC43.9-1 (or subsequent revision thereof) for instructions t of this form. This report is required by law (49 U.s . .1421). Failure to report can result in a civil penalty not to exceed$1,000 for each such violation (Section 901 Federal Aviation Act of 1858). 1. Aircraft Wdr AEROSPACE Model FSTREAM G-IV Serial No. 1085 Nationality and Registration mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. K-C Aviation, Inc. 301 Discovery Drive Appleton. WI 54915 U.S. Certificated mechanic QK2R112L Foreign Canificated mechanic X Certificated Repair Station Manulacturer D. I certify that the repair and/or alteration made to the un t(s) dentif led In item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Data SEP 2 4 1996 Signature of Autho zed WU 'dual 7. Approval for Return To Service Pu suant to the authority given persons specified belOve, the unit identified in item 4 w peeled In the manner prescribed by the Administrator of the Federal Aviation Administration and s ,R. APPROVED 0 REJECTED FM Flt. Standards Inspect or Manufacturer Inspection Authorization Other (Specify) Inspeet. BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approvalor Rejection SEP 2 4 1996 Certificate or Designation No. QK2R112L Signature of Au th ed Individual (C421 C 1-- FAA Form 337 oar SDNY_GM_0275aile SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00241040 EFTA01326633

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record4seh.prati compatible with all previous alterations fo assure continued conformity with the applicable ainvorfh I-- ust be tits. 8. Description of Work Accomplished Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Repaired left (02 from outboard) and right outboard flap drive rods and ground existing structure that rod goes through in accordance with Gulfstream Aerospace Standard Repair Drawing 5E05807901. Removed left and right main gear forward trunnion bearings, removed corrosion in trunnion support and plated in accordance with Gulfstream Aerospace Standard Repair - Spherical Bearing - Main Landing Gear - Sponson Rib - Trunnion repair drawing 5E45732901. No weight and balance change. END 0 •Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60IST SDNY_GM_02754119 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241041 EFTA01326634

017M41143•1 co wg?Inosircei..."'"".“nosmasherroArse " " • STANDARD AIRWORSHNSSS CERTIFICATE att., NORGA istfacM10•••••••00124 cocrarReam / vxv - - I s - k R A - - . - . 0 LOSS ASSORT . 1 s - - Yw 12/14/88 CL atis— TAY (WO °"`ARYCOSNEN% VMS CII•t0Call M CMPAII) •• 114 WIWI' w ACCOOISCII WPM AMON. Raft FAA Fain 11103-2 ww SONY GM 02754120 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15 EFTA 0024I042 EFTA01326635

SDNY_GM_02754121 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241043 EFTA01326636

0 MAJOR REPAIR AND ALTERATION US Deponent (Airframe, Powerplant, Propeller, or Appliance) of toreceubo• Fekel Medea elsothenneee Fee Armed 020 Na 21200720 For FAA Use Only office identification ii 9—O7 INSTRUCTIONS- Print or typo all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9.1 (or subsequent evision thereof) for instructions and eitsposillon of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G - I V Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above X Powerplant Propeller - Appliance Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X U.S. Certificated Mechanic AP 1864049 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unfits) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation R lations and that the information furnished herein is true and correct to the best of my knowledge. Date 7....70 -ft S • • • r 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit id ntified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 121 APPROVED O REJECTED BY FAA Rt. Standards Inspector Manufacturer X Inspection Authorization Other (Specily) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 7 -A9 -fAr Certificate or Designation No. 526705494 IA Signature of Auth • In dual GL Ls Michael Donnelly FAA Form 337 (07-96) This is a computer ed form created by Michael Donnelly. SDNY_GM_02754122 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_OO241O44 EFTA01326637

NOTICE Weighrand balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) In order to provide continuity during fitture inspections, maintenance or alterations a true dopy of this FAA form 337 and all listed Wiring Diagrams must be kept with the aircraft's records as long as the alteration remains in effect. July 10,1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet A I2EA. Aircraft in-service data: 2241.9 hours & 932 landings. Refer to the following FAA Approved Data: GAC Aircraft Service Change {ASC} 143 (ATA 24) Alternator Field Current Overcurrent Monitor, dated: October 7, 1994; and FAA Form 81 I 0-3, dated: 7-10-96, Identifying: Drawing No. ASC 143-062096, Titled: TOP DRAWING ASC 143 (ATA 241 Alternator Field Overcurrent Monitor Original Issue (no revisions), dated: 7-9-96, — the following Wiring Diagrams are listed on the TOP DRAWING: • Wiring Diagram No. 06209601, Titled: }.EFT SIDE DEVIATIONS dated: JUL 09/96 and • Wiring Diagram No. 06209602, Titled: RIGHT SIDE DEVIATIONS, dated: JUL 09/96, as approved data, signed by: John R. Chambless, NM-567, Systems and Equipment (Electrical). The purpose of this alteration is provide an indication that maintenance personnel can use to determine that an overload condition has occurred in a main engine alternator field circuit. This alteration adds a current sensor assembly and fault latch indicator to the left and right converter shelves and modifies the aft equipment compartment wiring. The above referred to Wiring Diagrams show deviations that were made to ASC 143 in order to provide a way to disconnect a DC Current Sensor or Alternator Overcurrent indicator display without cutting wires. These deviations also add a shield braid for each existing alternator (+) field wire and bond both DC Current Sensors, eliminating the need to run new wires to the left and right engine disconnect plugs. Performed all of the modification instructions of ASC 143, except as provided for on the above listed Wiring Diagrams. All parts were purchased from Gulfstream Aerospace Corporation — Savannah, GA and were new at the time of installation. Successfully performed — ASC 143 Operational Test in accordance with Paragraph E. of the ASC's instructions and noted no abnormal conditions or unusual operation. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. Incorporation of this alteration adds 0.2 amps to the Essential 28 VDC bus. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. This is • computer generated fan created by: Michael Donnelly ASC14388.DOC WORD 7.0 07/10961239 PM NO ADDMONAL SHEETS ARE ATTACHED. •END' K Additional Sheets Are Attached SDNYGIvl_02754123 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241045 EFTA01326638

-Pi JR . U.S. DEPARTMENT OF TRANSPORTATION , • FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7-10-96 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE ei il ,„ GULESTFEAM AEROSPACE MODEL NO. G-IV TYPE (Airplane, Radio, Koko: Net, etc.) AIRPLANE NAME OF APPLICANT THE DIAL CORPORATION / UST OF DATA IDENTIFICATION TITLE ' DRAWING NO. REV DATE #SHTS ASC ALIEFtNATOR CURRENT BY DRAWING TITLE ASC-143-062096 N/C 7-9-96 1 °THE ABOVE DATA N REVI WED NAME: ..a .7 TOP 143 DER DATE DRAWING (ATA-24) FIELD OVER MONITOR CANDIDATE 7-9-96 Michael natty PURPOSE OF DATA TO SHCE4 OCMPLIAI4CE WITH FEDERAL AIRWORTHINESS REGULATIONS, ON AIRCRAFT MODIFICATION WIRING DIAGRAM CN ANY GULFSTREAM G-IV HAVING ASC-143 APPUCABLE REQUIREMENTS (List spades sections) 25.1301(a,b,c,d); 25.1309(bl); 25.1353(a,b); 25.1357(a,c); 25.1431(c) CERTIFICATION — Under authority vested by direction of appointment under Part 183 of the Federal Aviation - NONE - have been examined of the Administrator and in accordance with Regulations, data listed above and on attached in accordance with established procedures conditions and limitations sheets numbered and found to comply with applicable requirements of the Federal Aviation Regulations. I (We) Therefore 0 Recommend approval of these data these data F3 Approve SIGNATUREtS) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) I DESIGNATION NUMBER(B) CLASSIFICATONIE) dr ...4 or ..7 6/.2ser....a.,,,..4 John R. Chambless NM-567 Systems &Equipment (EleCtrical) FAA Form 6110-3 (11-70) SUPERSEDES PREVIOUS EDITION 7.00 Qj 011 YNN0P This a a cernpuhr geneated lam anted (0995) by: hada& Dannelly 9t92 6St Z0L 0C:60 96/0T/L0 SDNYGM_02754124 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241046 EFTA01326639

SDNY_GM_027.125 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I047 EFTA01326640

ASC 143 (ATA 24) Alternator Field Overcurrent Monitor LEFT SIDE DEVIATION The Dial Corp Aviation Department WIRING DIAGRAM No. 06209601 Original Issue JUL 09/96 , ASC 143 (ATA 24) Alternator Field Overcurrent Monitor RIGHT SIDE DEVIATION The Dial Corp Aviation Department WIRING DIAGRAM No. 06209602 Original Issue JUL 09/96 The Dial Corp Aviation Department 2505 E. Airlane Blvd. Phoenix, AZ 85034 602-207-5363 voice 602-207-5353 fax Gulfstream Aerospace Model G-IV effective all S/N aircraft having ASC 143 (ATA 24) Alternator Field Overcurrent Monitor TOP DRAWING No. ASC143-062096 Original Issue JUL 09/96 SDNY_GNI_02754126 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241048 EFTA01326641

SDNYGM02754127 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241049 EFTA01326642

V1013A20— › bød • ~0 TO IJCItt *PI Cain tut Otleantl4.1 Namur mar ~ma we Nunn.. ~et The Dial Corp Mtalniittitlemeta 23,3 Z. AMY* OW& non» At 11414 60201141 ere 00000 In 02.1•1 Mgt Cata V.013020 Ma ACC NC DIAL CORP »ANC NACAMA 000141A1C Iq MGM SIDE DEVIATION' VINIX20 edd VIMILANUI TV10,114 W CONN WI PC" AHCO II •Ltat lEIAPRO 1~ .1~1~ MU) WO ~ILO Y •••41.11.8 tat 1•110.0.8S1 . 1År ~Ns Mtn ~Ka lababre• LEFT µNA arg OVORGURROKT m» NOCAT011 1•01.7.021 nit tic saw Mr» Male » amommmer Ma— »re« • paltatitneett. — ~It att ...es .25 MPG Imo» Rob» On M lamed 18 DOG metro Gødø 1 (NO ALT» MUD CtMAINT 2040.1 Ms CT.» WA til~Milit tattilitt Pmet•Imetw HI GA@ 44.43 .0~ • • ••• • a ~S. —• •••• • • •••••• LEFT CONVERTER SHELF no roam» ~moon --a otthanam• =it% oq LEFT »WM OttCON/ICCT S010 ret Aka tft do rae• GI.0 11• td.143. »We» «Met» el Pent NTA 341 AM. natas field Ovensmem10MMA Tids Waco Nap ~a» an Adana lb Immeonel »A en »acme« monn« b. occombø De ~mar ~en» Ton ..Mn aeon 5.1.• won •••••••••••.» to i» W I.M,011 vermorme WM. imbo »OD« irgapommicammelmaimids• TMtl rianae. ono» ~WM» NM MAID 143 InM.rb Moan • Way W distant • OG GoribM Sal« M AgrnnM Ostonat ~My dibia.1~ maim •••• TIN ~Sea MO ~Me •OCA ~lie ~mar 1./.4.11 • bonds M. DC Gam» tam" emnaads. No MIN bisatt ~el let ~NA »4 MN taiatit‘i40~1...• d+å »Am» ea Mad wools 1141.0210/18me »see et» Mom Nina am.b• »mum» M/ »men ammo GAG Wig» tam SI dap» nova IN» at At Ow» 10•41—.~...1~ »a • mapieSTR. oie es Der. Hy outmost St ~Myth" Ailen.mbie lanai 13-1V effliam ø• AM »emit 55.1.» Alt 10 1ATA LI Anortelor PAM Oremmn». »MI« LOOT SIM pre101014 WIRMO DIMULUI No DHOW» Orameed Ina AA 0.At • SDNY_GM1,1_02754128 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241050 EFTA01326643

- SDNY_GM_02754129 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024105 I EFTA01326644

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SDNY_GM_02754131 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I053 EFTA01326646

.- rb MAJOR REPAIR AND ALTERATION isio a .r (Airframe, Powerplant, Propeller, or Appliance) Mr ha° AIW0nd MIX*. 21204020 For FAA Use Only Office Identification ItISTRUCTIONS' Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of (hi /can. This report is required by ism (49 U.S,C. 1421). Failure to report can result In a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G - I V Serial No. 1 0 8 5 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above) X Powerplant Propeller Appliance Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X U.S. Certificated Mechanic A P 1 8 6 4 0 4 9 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made o the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my Imowledge. Date Si o o ed Individual ""717` - p( t e 7. Approval for Return to Service Pursuant to the authority given persons pccified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is al APPROVED 0 REJECTED BY FAA Flt Standards Inspector Manufacturer X InspectionAuthorization Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 4-- /8 -94 , Cenifieste or Designation No. 526705494 IA Signature of Au d e 71 Michael Donnelly FAA Form 337(114s) This is a cater generated form created by Michael Donnelly. SDNY_GM_02754132 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_0024 (054 EFTA01326647

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 06/17/96 Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al 2EA. Aircraft time in service: 2234.1 hours and 929 landings. FAA Approved Data: FAA Form 8110-3 Statement of Compliance with the Federal Aviation Regulations dated 11/01/94 for Gulfstream Model GIVAirplane, listing GAC Drawing No. SE45807901 - REV. A - 10/31/94, effective for S/N 1000-1195, title: STD REPAIR — BREATHER WING T.E. BOX - F.S.498.00 (MAJOR), signed by Structures DER John G. Wilder, Designation Number SO-483. The purpose of this repair is to remove the existing GAC P/N 1159W40226-17/-18 (aluminum) breathers that are cracked beyond limits from the aft side of the trailing edge (T.E.) box beam and replace them with new P/N SE45807902-11/-12 (stainless steel) breather on the forward side of the beam as shown on the above referred to drawing. Removed the existing breathers from the aft side of the left and right wing trailing edge boxes by drilling out the attaching fasteners. Trinuned the perimeter of the new SE45807902-11/-12 breathers to fit the installation and match drilled 0.164-0.167 inch diameter holes in the breathers to existing aircraft rivet hole locations. Finished fay surface of SE45807902-11/-12 breathers with two (2) coats of #2012 Epoxy Primer and one (1) coat of 2013 epoxy top coat paint. Attached the prepared left and right breathers to the forward side of their respective beams using new Hilok fasteners P/N HL 10V5-2 Hi-Lok and P/N HL, 70-5 collar at each of the 10 inboard attach points; and new P/N HE., 30-5-3 (-4 at the top position only) Hi-Lok and Bl, 70-5 collar at each of the 6 outboard attach points. Note: All fasteners were installed wet with pro-seal 870 (or equivalent product per MIL-S-81733). Changes to the aircraft's weight and balance were negligible. This computer generated form was prepared by: Michael Donnelly. NO ADDMONAL SHEETS ARE ATI-ACHED. oalD• O Additional Sheets Arc Attached SDNYGIvl_02754133 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241055 EFTA01326648

CIS MI 0 c';_,:y‘F.IVED FAA 4 .1)' (../ MAJOR REPAIR AND ALTERATIOW B 121°96 us oeconnwar cliemponmen (Airframe, Powerplant, Propeller, or A PPIIMYSSDO Weed Aviatio Administrationn Form Approved OMB No. 2120-0020 For FAA Use Only office Identification VW ite—6PD INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43Appendix B. and AC 43.9-1 (or subsequent revision thereof) tor instructions and disposition of this form. This report is required bylaw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Gulfstream Aerospace Corporation Model G-IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Nam.kiels shown on registration certificate) Mellon Financial Corp. Ni Address (As shown on registration certificate) 4444 One Mellon Bank Center Pittsburgh, PA 15258 3. For FAA Use Only • .0. Unit Identification S. Type Unit Make Model Serial No. Repair Anatol,: AIRFRAME (As described in Item 1 above) X .. POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CFC Aviation Company,LI-C dibta The Jet Center 16300 Daily Drive Van Nuys, CA 914064283 u.s. Cenificateo Mechanic C9FI1844.1 Airframe 3,4 Ptilid10 112 & 3 Limited Powerplant, instrument & Accessory Foreign Co:Ideated Mechanic X eormieatee Repair Station manuractwer D. I certify that the repair and/or alteration mode l° the un't(s) identified In item 0 above and described on the reverse or attachments hereto . have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date FEB. 9 1,38 Signature of AuthOr Individual • '. 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below, the unit identified In item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is 0 - APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada AirworthineSS Group Date of Approval Or Rejection FEB' 9 1996 Ceniticale or Designation No. C9FR844J Signature of Authorized lndi • al ..a.-4.-c-t 2 ...--4,...t...4" FAA Form 337 SDNY_GM_02754134 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024I056 EFTA01326649

NOTICE Weight and balance or operating limitation changesshall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations fO assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished- (If more space Is required, attach additional sheets. identity with aircraft nationality and registration mark and date work completed.) 02/09/96 GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA This is to amend FAA Form 337 dated 01/26/96 regarding the provisional installation of a Honeywell NZ-2000 FMS Computer modified to software version 4.1 which functions as an independent third navigation system and as a warm spare to replace either FMS-1 or FMS-2 including its aircraft systems interface. An upgrade to previously installed dual Honeywell GPS sensors from PN: HG-2021-AB02 to HG-2021-GD-02 was also incorporated in conjunction with the third FMS. These modifications were incorporated in accordance with the applicable technical data contained in configurations 13, 15,16 and 17 of The Jet Center Configuration Control Document 08006005 Rev. D dated 01/20/96, FAA approved 02/02/ as a later revision to plemental Type Certificate No. SA3774NM. Airplane Flight Manual Suplement Document Nos. 08015090 Rev. N/C, 08015091 Rev. N/C, 08015009 Rev. A, and 08015011 Rev. B, all of which were FAA approved on 02/02/96, have been provided to the operator. Minor deviations to the STC with regard to the electrical installation were accomplished in accordance the following Jet Center wiring diagrams which are FAA approved by Sarkis A Karaguzian, FAA Systems and Equipment DER NM-2128 on FAA Form 8110-3 dated 02/09/96: 08069100 Rev. A dated 01/20/96 - No. 3 FMS 08069324 Rev. A dated 01/20/96 - No. 1 & No. 2 Global Position The 3rd FMS computer may be installed in the mount provided. The circuit breakers controlling power to the two GPS sensors can be closed. The placard stating "FMS-3 AND GPS INOP PENDING FAA APPROVAL" placed on the instrument panel can be removed. The effect of these modifications upon the aircraft empty weight was reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagrams listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END O Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: I992-769-012/60157 SDNY_GM_02754135 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241057 EFTA01326650

'at—!o ff 0 • . MAJOR REPAIR AND ALTERATION USCepeetrrent or soNsoonsson (Airframe, Powerplant, Propeller, or Appliance) hwassiatioilai Adrewstration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identlficatlpp Illig -P 512O INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix Et and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1400 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make GWfstream Aerospace Corporation Model G-IV Serial No. 1085 Nationality and Registration Mark N811GA 2. owner Name (As shown on registration certificate) Mellen Financial Services Corp. ft3 Address (As shown on registration certificate) 4444 One Mellon Bank Center Fittsburgh,PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certi Nate No. CFC Aviation Company, L.LC. d/b/a The Jet Center 16300 Daily Drive Van Nuys, CA 91406-1283 U.S. Certificated Mechanic C9FR844.1I Airframe 3,4 Radio 1,2 & 3 ..irnited Powerplant, .ost rument & Accessory Foreign Certificated Mechanic X Cenificaled Repair Station Manufacturer D. I certify that therepair and/or alteration made to the un t(s)Identif led in item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my nowledge. Date JAN 2 6 1996 Signature of Authorf Individual 7. Approval Approval or Return To Service Pursuant Administrator BY to the authority given persons specified below, the unitidentified In Item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is er -APPROVED 0 REJECTED FAA FP Standards Inspector Manufacturer Inspection Authorization other(Specify) (Specify) FAA Designee X Repair Station j Person Approved by TrariSPOrt Canada AinvonhIness Group Date of Approval or Rejection ;JAN 2 6 1996 Certificate or Designation No. C98148443 Signatur Authorized Individual -4-4-6-4- - C FAA Form 337 meal SDNYGl.l02754136 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241058 EFTA01326651

NOTICE Weight and balance oroperating limitation changes shall be entered in the appropriate sacra I t record. An alteration most be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished' (It more space Is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS . Removed an existing Honeywell NZ-920 acting as the third Flight Management System Computer with its mount, and the dual Honeywell HG-2021-AB-02 Global Navigation Satellite Sensor Units previously installed per STC #SA3774NM. Flight Manual Supplement Numbers 08015014 and 08015015 "Original" Revisions dated 07/18/91 for FMS-3 and Dual Honeywell Global Positioning Sensor System were removed from the Airplane Flight Manual. Installed provisions for a third Honeywell NZ-2000 Flight Management System (FMS) computer modified to software version 4.1C a ong with mounting provision and a configuration module to function as an independent third navigation system and as a warm spare to replace either FMS- 1 or FMS-2 including its aircraft systems interface. Electrical provision were also made for dual Honeywell HG-2021-GD-02 Global Navigation Satellite Sensor Units that are installed in conjunction with the third FMS. Parts 1 and 2 of the Type Inspection Authorization for FAA Project No. SA4222LA-T have been satisfactorily completed and issuance of the revision to STC SA3774NM is pending FAA approval. Electrical provisions were installed in accordance with the following Jet Center Wiring Diagrams which are FAA approved by Sarkis A. Karaguzian, FAA Systems and Equipment DER NM-2128 on FAA Form 8110-3 dated 01/26/96: 08069100 Rev. A dated 01/20/96 - No. 3 FMS 08069324 Rev. A dated 01/20/96 - No. 1 & No. 2 Global Position The #3 Navigation Computer was installed on an existing avionics shelf located in the right hand avionics bay at Fuselage Station 162.0 (Horizontal Arm 102.0). Both GPS Sensor Units are installed in the existing mount structure used for the removed sensor units beneath floor 15. These installation meet the static load requirements of AC 43.13-2A Chapter 1. The 3rd FMS computer is not installed in the mount provided. The circuit breakers controlling power to the two GPS sensors are locked open pending FM approval. A placard stating "FMS- 3 AND GPS INOP PENDING FAA APPROVAL" is placed on the instrument panel. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagrams listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END El'Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-0I2/601S7 SDNY_GM_02754137 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241059 EFTA01326652

t1/44,4,0 Tx"- ? /, OP MAJOR REPAIR AND ALTERATION uSeaslOttfred creonspcneton (Airframe, Powerplant, Propeller, or Appliance) Wirer *Melon Aaminumnion Form Aeon:wed OMB No. 2120-0020 For FAA Use Only Office Identification I/WV—FWO INSTRUCTIONS: Print or type all entries. See FAR 43-9. FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C.1421). Failure to report can result in a civil penalty not to exceed $1000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Gulfstream Aerospace Corporation Model G-IV Serial No. 1085 Nationality and Registration Mark NSSGA 2. Owner Name (As shown on registration certificate) Mellon Financial Services Corp. 83 Address (As shown on registration certificate) 4444 One Mellon Bank Center Pittsburgh, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X _ POWERMANT PROPELLER .SCEIVED FAA APPLIANCE Type JAN 2 9 1996 ' NV FSDC% Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CFC Aviation Company, LLC. dlb/a The Jet Center 16300 Daily Drive Van Nuys, CA 914041283 us gene:cats Mechanic FR844J Airframe 3,4 dlo 1,2 & 3 ted Powerplant, strument & Accessory Foreign Certificated Mechanic X Certificated Repair Station Manulacturer 0. I certify that the repair and/or alteration made to the un t(s) Identified In item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my nowledge. Date .IAN 2 6 19 9 6 Signature of Aut I ed Individual . . - e SA 0 017 . --ne---4-1----- - 7. Approval for Return To Service Pu Administrator BY suanl to the authority given persons Seedbed below, the unit identified In item 4 was inspected in the manner prescribed by the of the Federal AviatiOll Administration and is rr APPROVED ID REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rekection JAN 2 61996 Certificate or Designation No. C9F118441 Sig natur of Authorized Inclivpcit! ) ..A....e...a.. a. FAA Form 337 rizen SDNY_Glvl_02754138 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241060 EFTA01326653

NOTICE e • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS The following major Gulfstream Aerospace Aircraft Service Change is incorporated into this aircraft: ASC No. 349 with Amendment 1 - Navigation (ATA 34) Nav System Upgrade to NZ-2000 The amendment upgrades navigational computers 1 & 2 to software version 4.1. Gulfstream Aerospace Airplane Flight Manual Supplement No. GIV-95-04, FM approved on Nov. 3, 1995, required with this change, has been inserted into the Airplane Flight Manual. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list has been added to the aircraft records. The work described has been found to be in conformity with the above mentioned FM approved ASCs. The aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work order 9042, on file with this agency, covers the above described work. END K Additional Sheets Are Attached OU.S. GOVERNMENT PRINTING OFFICE: 1092-769-012/60167 SDNY_GM_02754139 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241061 EFTA01326654

0 i MAJOR REPAIR AND ALTERATION USOmerunere eflecepCeleaa. (Airframe, Powerplant, Propeller, or Appliance) Feelefol fretleflon Adminhaemen Form Approved OMB NO. 2120-0020 For FAA Use Only Office Identification nt" -590 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43Appendix Mend AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of thisformThis report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1 Aircraft . Make Gulfstream Aerospace Corporation model G-W Serial No. 1085 Nationality and Registration Mark NSSGA 2. Owner Name (As shown on registration certificate) Mellon Financial Services Corp. #3 Address (As shown on registration certificate) 4444 One Mellon Bank Center Pittsburgh, PA 15258 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 abo 0) X POWERPLANT PROPELLER APPLIANCE Type Manulacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CFC Aviation Company, LLC. dibla The Jet Center 16300 Daily Drive Van Nuys, CA 91406-1283 us. certificated Mechanic C9F11844J Airframe 3,4 Radio 1, 2 & 3 Limited Powerplant, Instrument & Accessory Foreign Cenificated Mechanic X 0min:sled Repair Station Manufacturer 0. I certify that the repair and/or alteration made to the un t(s) Wenn! ied in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date JAN 2 6 1696 Signature of Authorized Individual 7. Approval for Return To Service Pu Administrator BY suant to the authority given persons specified below, the unit-identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is 2 -APPROVED 0 REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada AinvorthineSs OreeP Date of Approval Or Rejection JAN 2 6 1996 Certificate or Des na C9 tionNo Signature of Authorized Individual a4/-4 C. Ccja-e-tra.-4 1 FAA Form 337 na-ae/ SDNY_GIvl_02754140 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241062 EFTA01326655

NOTICE • 41" Weight and balance oroperating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished' (II more space is required, attach additional sheers. Identity with aircraft nationality and registration mark and date work completed.) 01/26/96 GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS Removed existing Sundstrand Mk. V Ground Proximity Warning Computer PN: 965-0676-006 from this aircraft. Flight Manual Supplement Number 41 349607-04 dated 10/14/87 for Sundstrand Digital Ground Proximity Warning System was removed from the Airplane Flight Manual. This unit was replaced with Allied Signal Mk. V Ground Proximity Warning Computer PN: 965- 0676-010. The new computer was installed in accordance with data contained in Gulfstream Aerospace Index List No. SC41-349836 Rev. C dated Feb. 20, 1095 reference on Supplemental Type Certificate No. ST00714AT issued on March 15, 1995. FM approved Airplane Flight Manual Supplement SC41 349M36, Rev. "Original" dated March 15, 1995, which is a required part of this STC, has been placed in the Airplane Flight Manual. Minor deviations regarding the electrical installation of this modification where accomplished using data contained in The Jet Center Wiring Diagram No. 08069434 Rev. N/C dated 10/09/95, "Ground Proximity & VVindshear" which is FAA approved by John R. Chambless, FM Systems and Equipment DER NM-567 on FAA Form 8110-3 dated 01/26/96. A forward pressure bulkhead feed through at Fuselage Station 85.5 was added to provide wiring &togs for stall warning computers. This was accomplished using data contained in Engineering Change Order EO043 applied to The Jet Center Drawing No. 08088188 Rev. N/C dated 01/17/96. This drawing is FAA approved by Joseph R. Holton, Jr., Structures DER SW-862 - on FM Form 8110-3 dated 01/26/96. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagram listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END O Additional Sheets Are Attached CU.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/601 67 SDNY_GM_02754141 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241063 EFTA01326656

fer Ftelb ArtC0•44 OMID Na 31204030 • C O MAJOR REPAIR AND ALTERATION For FAA Use Only net (Airframe, Powerplant, Propeller, or Appliance) ar rouenntim • Dews me Ader**Lesil mo ei Office Identification aef7 INSTRUCTION& Print or type as envies. See FAR 43.9. FAR 43 Appendix B, and AC 43.9-1 (or subsequent r Ion thereof) for instructions and disposition of INS lent. This report Is required by law (49 U.S.C. 1421). Failure to report can taunt In a OA penalty not to exceed $1,000 for each such violation (Sedan 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G-IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item 1 above X Powerplant Propeller Appliance Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X U.S. Certificated Mechanic AP 1864049 Foreign Certificated Mechanic _ Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unk(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirem nts of Part 43 of the U.S. Federal Aviation Regu ations and that the information furnished herein Is true and correct to the best of my knowledge. Date /ci t " re Signature of Audio ' ivi — Ce 7. Approval for Return to Service Pursuant to he authority given persons pecified below, the u it identified in item 4 was inspected in the manner prescribed by the Admin'strator of the Federal Aviation Administration and is C33 APPROVED Cl REJECTED BY FAA Flt. Standards Inspector Manufacturer X Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection / - 9 - - 94 Certificate or Designation No. 526705494 IA Signature of Authorized In ual Michael Donnelly FAA Form 337(l1.95) This is a computer gyyriyedfonn created by Michael Donnelly. SDNYGM02754142 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241064 EFTA01326657

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) In order to provide continuity during future inspections, maintenance, or alterations a true copy of this FAA form 337 must be kept with the aircraft's records as long as the alteration remains in effect. January 05, 1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2090.8 hours & 877 landings. Refer to the following FAA Approved Data: FAA Form 8110-3 dated November 17, 1995 identifying Aircraft Alteration Report No. 23-100895 AFIS PRINTER Original Issue no revisions dated October 8, 1995 Pages 1 through 15 as approved data, signed by John R. Chambless NM-567 Systems and Equipment (Electrical). Refer to the following FAA Acceptable Data: ACCULEX DPP-210/410 THERMAL PRINTERS User's Manual for operator instructions, maintenance, and other information. The purpose of this alteration is to install a miniature thermal printer that will print Airborne Flight Information System (AFIS) received messages. This alteration installs a modified ACCULEX model DPP-410 thermal printer in the co-pilot's side console, associated wiring to the existing AFIS Data Management Unit (DMU), and a I amp circuit breaker on the co-pilot's circuit breaker panel. The installation requires approximately 24 man-hours to incorporate. Performed all of modification instructions listed in the above referenced Aircraft Alteration Report. Printer was modified to -503 status by and purchased from Gulfstream Aerospace Corp. Long Beach, CA. Successfully performed an AFIS message — Operational Test in accordance with the instructions contained in the above referenced Aircraft Alteration Report. The aircraft may be dispatched with the AFIS PRINTER in-operative provided the AFIS PRINTER circuit breaker is pulled and an IN-OP placard is placed on the printer. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. Operation is automatic and straight forward and no Airplane Flight Manual revisions were required or installed as a rcsult of this alteration. The effect of this alteration on the aircraft's electrical load analysis was negligible and no changes were made to the aircraft's electrical load analysis report. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. this is a computer generaced loon created by: Michael Donnelly PRINTER.DOC WORD 6.0a: 01!05#96 7:43 PM NO ADDMONAL SHEETS ARE ATTACHED. •END' O Additional Sheets Are Attached SDNY_GM_02754143 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241065 EFTA01326658

yt` 0 MAJOR REPAIR AND ALTERATION US. Dtparimett (Airframe, Powerplant, Propeller, or Appliance) N Tenticanitica ntral A•loan A 4thilsinttlan RIM APMW. am NO 21200020 For FAA Use Only Office Identification a t -/C54 6 INSTRUCTIONS: disposition of this each such viotati Print Cf typo as entries. See FAR 43.9. FAR 43 Append% B. and AC 43.9-1 (or subsequent revision thereof) for instructions and form. This report Is required by law (49 U.S.C. 1421). Failure to report can result In a civil penalty not to exceed $1,000 for n (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G-IV Serial No. 1085 Nationality and Registration Mark N88GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification • 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above ***** ************** X Powcrplant Propeller Appliance TYPc Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X U.S. Certificated Mechanic AI' 1864049 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regu ations and that the information furnished herein is true and correct to the best of my knowledge. Date /— g - n Signature of zed Ingidu ./.:ct 7. Approval for Return to Service Pursuant to the authority given persons pecified below, the unit identified in Item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Ell APPROVED O REJECTED BY FAA Flt. Standards Inspector Manufacturer X Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date o Approval or Rejection /Ale‘ Certificate or Designation o. 526705494 IA Signature of Authorize Indivi I reAe r Michael Donnelly FAA Form 337 (11-95) This se a ter generated form creased by Michael Donnelly. SONY_GM_02754144 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241066 EFTA01326659

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) January 08, 1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2090.8 hours & 877 landings. Refer to the following FAA Approved Data: Gulfstream Aerospace Corporation Aircraft Service Change 364. subject: DOORS (ATA 52) 12th STAGE AIR SOURCE - DOOR SEAL SYSTEM PRESSURE, dated September 26, 1995. The purpose of this alteration is to reduce the potential for door seal deflation by ensuring a constant high pressure and maximum flow output from the door seal regulator. This Service Change installs additional pressure supply lines, one from each engine, routed from a port located in the pylon upstream of the 12th stage H.P. valve to the existing door seal regulator pressure supply lines located in the tail compartment. The existing pressure supply lines are re-routed to separate the water system pressure tap and the total air temperature probe pressure supply form the door seal pressure supply lines. A separate air supply manifold now supplies this circuit. This Service Change modifies door seal plumbing in the tail compartment and in both nacelles. The installation requires approximately 90 man-hours to incorporate. Performed all of modification instructions listed in the above referenced Aircraft Service Change. All parts installed were provided in kit form by Gulfstream Aerospace Corp. Savannah, GA. Successfully performed a Bleed Air System — Operational Test in accordance with the instructions contained in the above referenced Aircraft Service Change. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. Entered a change of + 8.0 pounds at horizontal arm 627.7 (ES. 609.7) to the aircraft's basic weight and balance report. this is a computer generated form created by: Michael Donnelly ASC364.0OC WORD 6.0a: 0U08/967:13 PM • NO ADDITIONAL SHEETS ARE ATTACHED. •END• 0 Additional Sheets Are Attached SDNY_GM_02754145 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241067 EFTA01326660

. , 0 MAJOR REPAIR AND ALTERATION u.S. Drys:moil (Airframe, Powerplant, Propeller, or Appliance) "r"°""°` TochnlAvIstlea Mallalstra4.• Rs Aro.41 OMB Na 21204020 For FAA Use Only Offee Identification 554 -- Flea INSTRUCTIONS Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instruellons and dIsposIdon of thl form. This repents required bylaw (49 U.S.C. 1421). Failure to report can result Ina civil snaky not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Gulfstream Aerospace Model G-IV Serial No. 1085 Nationality and Registration Mark NS8GA 2. Owner Name (As shown on registration certificate) MELLON FINANCIAL SERVICES CORP #3 Address (As shown on registration certificate) 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item 1 above 71 Powerplant Propeller Appliance Type Manufacturer 6. Conformity Stat went A. Agency's N me and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON 13560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 8S258 X U.S. Certificated Mechanic AP 1864049 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date liC 6-fr- Signature of on Indiv au. I 7. Approval for Return to Service Pursuant to the authority given persons pecified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED CI REJECTED BY FAA Flt. Standards Inspector Manufacturer x Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Ithaspon Canada Airworthiness Group Date of Approval or Rejection ide /e5 r- certificate or Designation No. 526705494 IA gnatu of Autho' d Michael Donnelly FAA Form 37 (I I-95) This is a co efgenerated form totaled by Michael Donnelly. SDNY_GM_02754146 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241068 EFTA01326661

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identify with airman nationality and registration mark and date work completed.) In order to provide continuity during future inspections, maintenance, or alterations a true copy of this FAA form 337 must be kept with the aircraft's records as long as the alteration remains in effect. November 05, 1995. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2073.2 hours & 869 landings. Refer to the following FAA Approved Data: FAA form 8110-3, dated September 14, 1995 for Gulfstream Aerospace Model O-111 airplane, Identifying: The Dial Corp Aircraft Alteration Report No. ST4502LA-T; Titled: APU HOUR METER MONITOR Original Issue, dated September 08, 1995 — No Revisions — Pages: 1 through 14. The purpose of this alteration is to provide current limiting protection for the Auxiliary Power Unit's {APU} Electronic Control Unit {ECU} that will prevent a short circuit in the hour meter or associated wiring from affecting the normal operation of the APU. This alteration also provides a visual cue that maintenance personnel can use to monitor the operation of the APU Hour Meter. Past experience has shown that if the APU Hour Meter or associated wiring short circuits while the APU is running an unwanted APU shut down will occur and normal starting will not be possible. It has also been demonstrated that the ECU can be damaged if repeated start attempts are made with a shorted APU Hour Meter or associated circuitry. Performed all of instructions listed in the above referenced Aircraft Alteration Report. Successfully performed an APU operational test using the FAA Approved G-IV Airplane Flight Manual and while the APU was running above 95% APU RPM (+ 4 seconds time delay) verified that the APU HOUR METER MONITOR indicator was ON (dim) and pulsed (bright) approximately once every 3 seconds. Shut down the APU and verified that the APU HOUR METER MONITOR indicator was OFF. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. The effect of this alteration on the aircraft's electrical load analysis was negligible and no changes were made to the aircraft's electrical load analysis report. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. HR_MTR.DOC WORD 6.0x IIMPIS II:26 AM NO ADDMONAL SHEETS ARE ATTACHED. *MD* Cl Additional Sheets Me Attached SDNY_GM_02754 147 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241069 EFTA01326662

• U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE September 14, 1995 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream Aerospace MODEL NO. G-IV TYPE MIS RS Holkoptor. so) Airplane NAME OF APPLICANT The Dial Corp LIST OF DATA IDENTIFICATION TITLE AIRCRAFT ALTERATION REPORT Report No. ST4592LA-T APU HOUR METER ORIGINAL ISSUE No Revisions Pages: 1 through THE ABOVE DATA NAME: — 14 MONITOR dated: September B EVI D 08, 1995 ‘& BY DER DATE: ( 8, 5 .c.)., I _ e i r tA° CANDIDATE September 19. 1995 Michael Donne PURPOSE OF DATA In support of Supplement Type Certificate (STC) for the Installation of Current Limiting Protection and Monitoring of the Auxiliary Power Unit's Hour Meter in the Gulfstream Aerospace G-IV Aircraft. APPLICABLE REQUIREMENTS (List specific sections) 25.1301 (a) (b) (c) (d); 25.1309 (b) 1; 25.1353 (a) (b); 25.1357 (a); and 25.1431 (c) CERTIFICATION — Under authority of appointment under Part 183 of the NONE have been vested by direction of the Administrator and In accordance Federal Aviation Regulations, data listed above and on attached examined In accordance with established procedures and Aviation Regulations. with conditions and limitations sheets numbered found to comply with applicable requirements of the Federal approval of these data these data N Recommend I (tse)Therefore M Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMBERM CLASSIFICATION(S) / 44 7 efi7 6 Z-apf John R. Chamblass NM-567 Syistems. aitquipment (E =trio FAA Form 8110-3 (11.70) SUPERSEDES PREVIOUS EDITION T006j GET VNN0D nes Ise =craft genecated form anled OM by: (.9:oot Donnelly 9695 696 Z0L 3Y3 LS:ST 28/SO/TT SDNY_GM_02754148 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241070 EFTA01326663

SDNY_GM_02754149 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00241071 EFTA01326664

SDNY_GM_02754150 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241072 EFTA01326665

a IAA AIRCRAFT REGISTRY CATIERA NO. a DATE: 5 - . - • ' MAJOR REPAIR-AND ALTERATION ligiel. — -' • - ' (Airframe, .. Powerplant, Proper, Or AppRinee) • lem Apo.. means@ For FAA We Oa Offse leant-two .57:x - t e) a iNTIRUCKINS: ingthotions and penalty not to Print or roe all aunts. See FM 43.9, FM II Appendix B. and AC 43.9-1 (or subsequent ration thereat) for disposidon of dos form. This Noon Is moat by law (49 U.S.0 1421). snore to report can !teak In a ad acted $1,000 for each such *anon (Section 901 Federal Avladon Acid 199). I. Aircraft Make Gulfstream Aerospace Model G-P/ Serial No. . 1085 Nationality and Registration Mark • N8RGA" 2. COM16F . , Name (As shown on registration certificate) ; ; Mellon Financial Services Corp /13 .. . . : Address (As shown on registration as ficate) 4444 On Mellon Bank Center Pittsburgh, PA 15258 • 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make j Model Serial No. Repair Murton Airframe (As described in Item I above) X Powerplant • Propeller - • Appliance -1,Tc Mandan 6. Caforathey &maw • - . A. Agency, Name and Address B. Kind of Agency C Certificate Ne. LANCE A. MATTESON 6560 E. SAN FE LTPE DRIVE SCOTTSDALE, AZ 0.5250." X U.S. Certificated Mechanic AP 10.64049 Foreign Certificated Mechanic Certificated Repair Sudan Manta: am D. (certify the the 'w aneVor amen= made to the wills) identified in item 4 above and demnbcd on the '<verse a seachments berm have then ma to scostace with the requirements (Part 43 of the U.S. Federal Aviation Reganon, IS th.c the infosintion finished Inns is eye and area co the beatof my knowthige. • Date 2.5-0i4 +-cal. itter....- &pane of • ind z.. • d 'l • 7. Approval for Raton to Sawn Puma= to thc =betty give paces specified below, the unit tanned en etam 4 was inapsted in a manna *thothed by the Administrator of the Fulani Aviation Administration and is la APPROVED El REJECTED - BY FAA Rt. Scents Seems Manufacturer x Ramon Authorise* .i Otha (fiPendY) FAA Deep= aeprir Sluice :- ?CM= Approved by Transport - Canada Aiswordaess Orem Caen ApprOVal or /Sc --/P- Cavan or DetisoadonNo. 526705494 IA Signsten of Authorized r Michael Donnelly FAA Fero ) • • - 4 — SDNY GM 02754151 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00241073 EFTA01326666

IAA AIRCRAFT REDGAI TSTER? .7_ 7... Fs CAnES RD* • Weight and baler or operating limitation airy, shall be entered in the appropriate aircraft record. An alteration must he tympani* with all previous alterations to conatinued conformity with the applicable Unworthiness requiranents. t Description of Work Accomplished - (If more space is required mach idelinond them. Identify with secret =keenly sod rcipstrenon mart =4 Eats work oxonktedi In order to provide continuity during future inspections, maintenance and alterations a true copy of this FAA Form 337 is required to be kept on board the aircraft as long as the alteration remains in effect. March 24, 1995. GulfstreaniAerospace Corporation (GAC} Model G-IV, Serial Number 1085, N8801‘ FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 1896.4 hours ft 784 landings, Refer to the following FAA Approved Data: Gulfstream Aerospace Corp. Model G-IV (GAC) Aircraft Service Change (ASC) 234 SUBJECT: ELECTRICAL POWER (ATA 24) ESSENTIAL BUS FEEDERS — REROUTE dated December 16, 1993. . _ Refer to the following FAA Ac: ptable Data: Gullet:ream IV Computerized Maintenance Program (CMP) Revision 26, dated September 30, 1994; <IIIIIIONN> denotes applicable wok code. The purpose of this alteration is to separate electrical feeder cables and remove unnecessary wire connections. bliagfiaci the Left Cockoitlunction NW (30 SAD as fol km; (see figwe 2 of the above listed ASC) Removed and discarded the following woes from comectors 305A112 and 30:MI112: 1X560016A, I X5611216B. and 1X562D16C. Removed the following wires from connector 305A1P2:1X560E16A. DC561E168. and 1X562E IOC. Removed the following wires from connector 305A1P12: I X560A16A: IX561A168, and I X562A16C. Using a GAC P/N GASSOSM blue splice committed the following piths together rim the 305A I bosom plug connectors: 1X560516A & 1X560Al6A; 1 X.561E16B & I X561;416B; and DC562E16C & I X562A16C. Modified the Right Cockpit Junction Panel (10AA1 we follows. (see fig= I of the above listed ASC) Removed and discarded the following wires from aninecton 306AIM and 305A1113: 2X56013I 6A. 2X5611316B, and 2X5621:06C. - .. . . Removed the following wires from connector 306A IN: 2X5MEMA,230611I68, and 2X562E16C. Removed the following wires from connector 305A1P13: 2X560A16A, 2X561A16B, and 2X562A16C. Using a GAC P/N GASSO5A4 blue splice connected the following pairs tOgether near the 306A 1— hottattplagesearactx 2X560E16A & 2X560A16A; 2X561E168 & 2X561A16B; and 2X562EI6C & 2X562A16C. )lgglifiggign aircraft wiring as follow, (refer to the above listed acceptable data) Removed and installed Power Distniation Box in accordance with C4505@. Removed and installed lbansformer Ftectifler Unit ill accordance with C43025>. Separated (from each other) the craning pilot's electrical feeder cables Item the exist ing copilot's electrical feeder cables that nth from the Pow= Distribution Box (05A2) to the pilot's (315A1) and to the copilot's (314A1) chair break= panels. After reviewing the existing approved configurations it was determined the: dorm limited wirt-ron space and possible interference with =rating avionics and electrical installations it wu act practical to comply with the ASC's purpoae of separating the left, right, and essential bets feeders (from each other). Performed AC Power (26 Voh) System - Operational Ter; 4244045> and AC / DC Power Distribution - Function Tat 045051>. Recorded compliance with this FAA form 337 in the Masts maintenance records and =reed the stash to Mat Same. . . No changes to the south's tier:M=1.10nd analysis Suited hem this Cation The effect of this change on the airendrs Weight and liaise= Ins OtieigthIC and no tinges were made to the Maras sash weight and balance report Buseaccepra generstai farm card by: eras Desalt WORDia 01249511M MI NO ADDRIONAL SI TS ARE ATTACHED. *END' O Additiceal Sheets Are Attached • C C al'aga SDNY_GM_02754 1 52 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241074 EFTA01326667

0 MAJOR REPAIR AND ALTERATION VI Otswena . (Alrlesine, Powerpl an I, Propeller, or Appliahce) . sibuqns• Faiat...os ar ria Rt.Ma-a Oa as :tamp For FAA Um Ord1 Offtee Marairmatiaa a C • hOP INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-I (or subsequent :canon thereof) for Instructions and disposition of this form. This report is required by law (49 U.S C 1421). Failure to report can result In a chit penalty not to teed 51,000 for each such violation (Section 901 Federal Aviation Act-of 1958). 1. Aircraft Make - . ' Ca/Usti-mum Aerospace. Model G-IV Serial No. 1085 Nationality and Registration Mark N118GA Name (As shown on regrowth.* certigrtee) - T. Owe Mellon Financial Services Corp 03 Address (As shoat on registration certificate) 4444 One Mellon Earth Center Pittsburgh,. PA 15258 3. For FAA Use Oaly . 4. Dalt identification 5. Ten Uoit I • Model I Serial No. Repair Akeradon Airframe . , ••••••••••"••••••• (As descratird in Item. I ton) X . Powerplant Propeller SPOSts-t. .1)F " i Mahan ' • 6. CoMormith Statement ' A. Agra Name and Address ' B.- KIS of AiOnc, C. Cerlifmata N. • . LANCE A. MATTESON •• , 8560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 X US. Certificated Mechanic ' AP 1864649 • Foreign Certificthed Mechanic Certificated Repair Slalom Manufacturer D. 1 earn the the repair ardoraltaalloa nude to the math) identified in item 4 above sad described co the reverse or atiactimerth hereto have tom mak in eat with the requirements of Pan 43 of the US. Federal Anson Regalia= end thee the information tieraithed herein 4 Se ad CPTIX310 the ben of my knowledge. Daft ... . Ai-aid/acne /per •• - . . . _ Signature dua 7 Zt . .7. Appeoral f or Return to Sank, Pornisa Adrokasterne BY to the aaboriry given persons podded below, the St identified in item 4 was Imparted leathern/met preserazd by the of the Federal Aviation Adatthistration and a OE APPROVED CI REJECTED . FAA Ft Sande* awn Mande:pm _x rasp:arm Authonzadoe . . Other (Speedy) PAA Doha" Repair Radon • Person A4Vorned by Toreson Canada Mniortainesa Grow Dale of Appomere Rejection ' 3/2.5115 - - Sarsthma or thaintien No. 526705494 u t Signature a( A r Michael Donnelly - 1 cailaPerec - „ cajole? SCINT GM_02754 153 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241075 EFTA01326668

FAA AIRCRAFT REGISTRY ^ CAKERA ro Diaz t NOTICE Weight and balance or operating limitation changes shall be enured in the appropriate aircraft record. An alteration must be compatible with all previous alterations so assure continued conformity with the applicable airwonhiness requirements. 8. Description of Work Accomplished elf rote spec is required. 11111.6 OddlUalla steers. Iskatify with aircraft =noway a a:Otani:in matt and date work completed) March 24, 1993. Gulfsircani Aetolpace Corporation (GAC) Model G-1V, Serial Number 1085, NS8GA, FAA Aircraft Type Catifintitopsta Sheet A PEA. Aircraft in-service data • 1896.4 hours & 784 landings. . . Refer to the following FAA Approved Data: FAA Form 8110-3 dated 11.22.93 for Gulfstream Model (3-IV identifying GAC drawing oust I1590D1.40140 REV C (dated 11-17.93), AXLE FI777NG ASSY MAIN LANDING GEAR • (five sheets), as FAA Approval data signed by John G. Wilder Structures DER 50-483. Refer to the following FAA Acceptable Data: Gulfstream IV Computerized Maintenance Program (CMP) Revision 26. dated September 30..1994; d 0 0 018> denotes applicable work code. The purpose of this alteration is to install bushings into the boles for both main landing gear (MLG) axle fitting locking pins. In accordance with the above lined acceptable data: lacked the aircraft: <323001>. Removed four MEG wheel assemblies: <324011> 024012> <324013> <324014>. Removed four MIA brake assemblies: <324104> <724105> <324106> <324107>. Removed (car MIA wheel speed season: <324187> <324188> <324189> <324)541>. Removed the left and right GAC P/N i 159U:440140-II MEG axle fining assemblies. In accordance with the above listed approved data: Modified both MLG axle fitting locking pin holes. Cadmium plating was done by: Able Metallic Services - FAA repair station UMBR 624K - lob* 13253. Fabricated 2 each -II and -13 bushings (see Table I) and installed a -11 and a -13 bushing into each MLG axle fitting assembly. Prepared, painted, and installed both MLG axle fitting assemblies; Left S/N CPT 5102 HSM and Right S/N CPT 5221 HSM. Changed identification of both MLG axle fittings by lining an existing GAC P/N 11591-M40140-II and adding identifying mark I I590DLK114434. Note: Installed a new GAC P/N 1159L1420151-I I Ma gear axle fining locking pi (no S/N) and a new GAC PIN I15912440148-13 main gear axle fining attach pin: Left SIN CPT 6121110M and Righi S/N CPT 6152 10M, into each MLG assembly. . . Restored the following equipment to original configuration is meordanee with the above lined acceptable din;,Installed four MLG wheel speed so:mom <324187> <324188> <324189> <124490>. lassalled four MLG brake assanblits; <324104> <324105> 024106> 024107>. Inspected and packed all MU) wheel beesiaga <324051> <32.4.032>024053P <324054;. Installed four MW wheel assemblies; <324011> <324012>-.02A0I3><324014>. Performed Left. Right. and Emergency Brake Bleed mid Sakti; 424185≥012.4124n <3241i7>. PerforrnedkVbeel Brake and Anti-Skid System Funnion Tests <324I0I> <324I03>.• Norm' AmF-SkJ4 System Pmelion Test Stodes landing gear retraction and extension. Checked Left and Right NuteraCioi Saila AdfMameanti26021> <326/32$: Removed auvah fromjacks: <333001>. . An aprimpriately need pilot performed in aircraft Si %animal test and determined that ground handling and braking operations were satisfactory.. Recorded compliance with this FAA form 337 in the aircraft's maintenance. records and returned the aircraft to flight item. , , . • The effect of this change on the iireraft's weight and balance watt neglignsfie and no changes west made logic aircraft's basic weight and babnit import. - • • : - No AIMMONaMall, ATTAMIM IND° - ' 0. Additional Slats AreMated • SIDNY_GM_02754154 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFFA_00241076 EFTA01326669

• TAA AIRCRAFT REGISTRY CAKERA NO •OZ DATE: - Caa Piety. /US Ctstetat 04~ Ø1O-19% 14:ff2 FI1 GLLFSTREFTI IECH4ICAL CPS TO 916122075353 P.01 I .t, Rie.C.10 OAT{:. • estnnescs.• et rotate ,,,,, ,.. stintiAk AinAlsOm AOMINI ION STATEMENT OF COMPL/ANCE ?NTH THE FEDERAL AVIATION REGULATIONS I / fj: 1. F-- qi AIRCRAFT OR AIRCRAFT COMPONENT onNintIcAnom *ARC 1 • GULFS7RE.A.M 100 V. 11k, • I TY I e (szr. Reel, It...fit...re" AIRPLANE . m as< O • AP"tc no. • GULFSTREAM AEROSPACE CORP. LIST Oit DA TN. «Mil ICATIOW . Tint • thr -q00 L.. Øl40 RENÅ C • å ' `.4 ‘‘LE F1 777 io- 6. A s iv M AK) LANDI AJ 61 • i . I 6i EA . ' ...Ina " " "" Is t Dap 12E- 0% u ‘ QC byte ar-r S go cr— tvre1/4.) cazum PotvGAJT • .• a•PLICAlllt PIC,IliestilTI ItI« immts• .,.. _ ~SD. FS4Z ZS. 3(33--301 CERTIFICATION • V•nle valiant. vianad4ay 'Waal*, .1 tan Adaniavai «I la iteawiaact 'rid naillaira na a, laatia• al app•iament asiar Pan 113 *Ion Nil& Aviation' alraltlaws, ilia nits.. Jan ad a attacked •Lreis;* ieni --.— kne bln isietsti ia"ataiediaci.filititiaaiikei aid Iowa 60 c.apir ril aialiiiWi ratrikeis iagatnnega *I tie Silent Aiiataaa Iligaiatial: • I < ' ' n 'lacteal.. d liarnal •I zbesidaaa 1;pli thra (eta .. 1 .. taLAnnin dais diem YOM ',MI OF D'Vens V PtHennialMG atnitairtaTNEs Ins3g.da Tic», miadaiainil ClaSUFICatiOmi - • ' . ØN 1" F:IL1 et!..CA1 s-wirr •-•rc I 4 fl — SDNY_GM Oii54155 - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,15-, and 17 EFTA 00241077 EFTA01326670

- - SDNY GM 02754158 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241078 EFTA01326671

•-serAtait. FAA AIRCRAFT REGISTRY CAREW* NO. 3 DATE: r//Y,A>?C— .-o•'t="-':--aR'SPe=n••nam•I0'''"''•...-. hinelnag OM Ms ittint 0 MAJOR REPAIR AND ALTERATION Pena Ma Os en ?ennoble!, Propeller, mese Mazda ewillIM (Airframe, or Apatite:1i) ame= MOINISNISR 5h. -hoo lasliteCTIONL rem or cove ail amen . See FAR 43.9. FAR 43 Appendix a. and AC 4341 (of subsequent :evasion thereof) lot invitation. ad dispositlen of this form. This moon Is required by law (49 US.0 I421). Failure to report can malt In a civil. Penalty not to exceed S 1000 for each sua violation (Section %l Federal Aviation Act or feel. I. Aireteft Mike GWfstream Aerospace Model Cr-IV Said No. INS . • Nalienably end Regientlion Mart - NSSGA 2. Owner Nemo (Al Soon on tesiarnion outs) Mellon Financial Service Corp 83 lokkess (As town celegiettelion wither) 4444 One Motion Rank Cater Pittsburgh, PA 15253 i For FAA Use Only 4. Vett Idoedibef 5. Tnie Una Make I Motlel I Sabi No. Rea Atarieloa4 X Airframe (As deeratd in Dem I above) ......ae• . Pontplant i--"; ?rood= . Appliance inal beembainer C Cirefemaley Statement A. Amalie Name red A4clom . B. Kant of Many C. Canilkma No. LANCE A. MATTESON • X U.S. Certificated Meetenie 1660 E. SAN FELIPE DRIVE Foreign Caen/one Mechanic - AP 1161041 K0175DALE, AZ 15251 Catificerted Repair Steffen - • .Manufacturer - D. I catty that the repair mit« aternion made to tha times) identified fahm 4 thaw ee4 deeded on the reverie or etadoneral ham ban been made In sxordeete yeah the reernmette of Pert 0 oft U.S. Pedal! Arians Regalaaacs ma that the infommice feembod hetet= ead cornet Co the beg o my knowledge. .. Due • / 2. ,A......4 //Per • Signature of . bdivickel /2 .4- 2 .----- ' • .7. Awed Me Remora se Sarin Plasma to the =dairy even p0 specified below the int identified is item 4 __ impend le the roam poarlst byes asimisuarit of Misses:el *visite Attennetranon and is DE APPROVED 0 REJECTED By FAA fk Swedente Smalls hienufectove . X taspacrion Anon:Lan Ole (394.14) I FAA Dnepr, - Ripe Maim Pesos Approve! by Tramped Nadir Airwoehin!drop Date ottipixovel a Rejection cetese swipe /A 6•--.69-526705* 4 IA ......_ .— -.. • --7- „erg/Pr die! _.../ . micbmb onneny • -se! • • :_ is • SDNY_GM_02754157 " 44 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241079 EFTA01326672

c s FAA AIRCRAFT REGISTRY CAM RA NO. j DATE: VAY/ 79 . 7.11101- NOTICE Wel* and balance or operating ilmatslion danger skid be entered in Me appropriate aircraft moon!. An Manton must to campanile mils al previous alientions to assure continued confoemity wish the applicable sizworthiness requiem:Is. S Desciipike rdWork Accomplished Minors sews ti required. meth salmi Ma ism* Mai Sad eatheadity sedregitralan mak and dam wart camplited.) February 8, 1995. Gulfstream Aerospace Corporation (CAC) Model G-IV, Saul Number 1085, N88GA, FAA Aircraft. Type Certificate Data Sheet Al2EA. Aircraft in-service data -- 1881.0 hours & 775 landings. Refer to the following FAA Approved Data: FAA Form 8110-3 date 02-01-95 for Gulfstream Model G-IV identifying Gulfstream Aerospace Corporation drawing numbei 1159SB20470 REV .71 REWORK VERT FIN COVERS - ACCESS - ATTACH FTGS (five ‘. Sheets), as FAA Approved data signed by John G. Wilder Structures DER SO 483; and' Gulfstream Aerospace Corp. {GAC) Aircraft Service Change (ASC) 230 SUBJECT: STABILJZERS (ATA 55) PER77CAL STABILIZER ACCESS COVERS - INSTALL4 77ON OF prototype copy dated January 20, 1994 <CM? CODE 972300> The purpose of this alteration is to install remc\ able access panels on the vertical stabilizer to improve the accessibility for corrosion inspection of the vertical stabilizer/fuselage fitting and attaching hardware (interior of stabilizer). It also provides a means for inspection of the hardware that attaches the tie strap to vertical stabilizer/fu lag. attach fittings (three bolts per side). Modified the aircraft in accordance with the instructions and data contained on the above referred to drawing. Installed parts were furnished in kit form by GAC product support Savannah, GA Recorded compliance with this FAA form 339 in the aircraffs maintenance'records and returned the aircraft to flight status. The effect of this change on the aircraft's weight andisalsfise was igibk. Sind no changes were made to the aircraft's basic weight and balance nsfigitt. • - , • • .S; • • Zig Jig sans sand tea inopindlir MSS Malty. IMOD - eatil3 Tani NO AIECyCKALIIIIIIIIISAliAITACIIID MOP ' O Addidonil MeAttaebed. • - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _0(1241080 EFTA01326673

r oak. no 0 MAJOR REPAIR AND ALTERATION Fee IAA Ur OS *IAr nn (Airframe, Powerphint, Propeller, or Appliance) um.. ...saga Or aflame se a 130) 0CSTRUCTONS: Rees bps el slat Sr FM U.I. FAR 43 kart B. as AZ 434-1 a Sawa nab arnerneems as enserson or this lam. llis mon b many by la (a U.S.C. 14213 Fan to mart en rat kt • as way a to nand $11000 ke each ea nobta (Saba so FessfslAanak a of 1030). I. Aircra8 Make C.uffstream Aerco Paw Model G-nr Sena] No. 1085 Nations* and Registration Matt NSSGA 7_ Owner Name (As shown on minion ccrolaa) Mellon Financial Service, Corp ff3 Address (As shoal on regamon aniffais) 4444 One Mak. Bank Caner Pittsburgh, PA 15291 3. Tea FAA Do cna, 4. lira Ideatfleadsia S. Trod Unit Make I Model Serial No. Rem Alaska Airframe (As desalcd in Item l above) , - I Powerplant N RopeBa 4. Cathnolty Staleopt A. Amnon Nan ad Alarm B. Bind of Apnoy. C. Osaka No. LANCE A. MATTESON X U.S. Cannoned Machado Ufa E. SAN FELRE DRIVE Fagg, Catifwated Mechanic ' AP Mad SCCITTSDALE.AZ SEMI Cgtifated Rana StaliCa Manitheturer D. I cat* tha tha agar andier anti= made to la Inn) lamina Mama then ad dedaslad on the rent. or attsekmanta Mao have bat tank id axonlanee with the requirentoa east 43 dais U.S. Pea* Astion Ragoaketa ad rat the ictfomtaia Maned area ins ad aerie, to the bee my knovadp. Date . /2- ar-ty sigor{ 6al " ate A - -- 7. Approval kr fan larded Natal tots rho* Sv pans upecillid below. is ma tanifisd in an 4 fa band la do ream Bred by tho Adariadwaarof as Pedal Make tartan at is m APPROVED C/ REJECTED BY •MA ft ante loa , Manufacturer s lag:action Andtaision Ode (Spot) FAA Donlan Papa Swim . Pao Approved by Tmepai Cana Manta Croup Pat of Approval pi-Rejection l - firer Clear* or Dassios ta IA a Aficba DonneBy SDNY_GM_02754159 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024108 I EFTA01326674

7. VAR AIRCRAFT REGTSTIT D - 2. - CAMERA NO. ATE* fPnit .ta. 4'11 - e• egit i 1 NOTICE Weight and balance or ORcoltnil limilatlen changes shall be entered in the appropriate lime word. An aeration must be compatible with all previous alterations to assize continued conformity with the andiable sicraroithiness requirements 8. Description of Work Accomplished or more spree is sash atittanal theta Wean? with iticral tutonality andointealeis nark ed dew wad complatad) in order to provide contnutly during future inspections, tramenance. and aneratorts a caw of Iris FM Fan 337 Ltaicr. Repair and Alteraton is required to be kept on board the aircraft as long as the alteration remains in coact December 27. 1994. Gulfstrutm Aerospace Corporation (GAC) Model G-IV, Serial Nwnba 1085, N88GA, FAA Musa Type Certificate Data Sheet Al2EA. Aircraft in-service data vi 1856.3 hours & 763 lantings. Refer to the following FAA Approved Data: Grulfetream Aerospace (ASC} 239 SUBJECT: ICE ANDflAN PROTECTION (ATA .30) RINDMIELD IWAT -DUAL CONTROL SWITCHES dated Asyut 25, 1994. s:CMP CODE 972390>; and Gulftrcam Aerospace GIV Airplane Flight Manual Section 5 - SYSTEMS, pne 5- 40 WINDSHIELD HEAT FAA APPROVE) 4 February 1994. The purpose of this alteration is to provide independent windshield heat control for the Id front-right side and right front-left side windows. This service change adds a switch and modifies the windshield heat system wiring. Performed all of ASC-239's modification instructions effective for aircraft SIN 1085 riccit for the folowing minor deviations: (see - figure 2. Page 9) • Wire 2H537A20N was changed to 2H537A22N in ceder to fit into ground block 54 position "S*; •. Was 2.11538A20N was changed to 211538A22N in orda to fit into ground block E2 position 'flr; • Wire 211110822 was Sated into 318A1P10 position -II" because position small "IC was not available; and • Wire 2.13/4 64A22 was inserted inns 3113A1 1) 10 position 1st because position small It was not available. Installed parts are listed on page 4 of ASC 239 and were furnished in kit form by GAC product support Savannah, GA. Successfully performed Windshield Heat —Operational Test in accordance with paragraph C. page 3 of ASC- 239's instructions. Recorded compliance with this FAA form 337 in the airerafts maintenance recort and rammed the aircraft to !tight status. Information on the dual switch system will be contained in Section 5 - SYSTEMS of the GPI • Airplane Flight Manual, revision dated 12 July 1991 or later issue. The effect of this change on the aircraft's electrical loading is negligible and no changes uric made to the arcraft's electrical load analysis report. The effect of this change on the aircraft's basic weight and balance was negligible and no changes were made to the airaaft's basic weight and balance report. This a • ecitiptan Reoamod form inspired by Mead Deafly. WORD 6.th 0LO2/95 3A9 Pal NO ADDMONAL SHEETS ARE ATTACHED. *DM* a Additional Sheets Are Attached 4 • ..• • a a. s • a SDNY:Gbl_02754160 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241082 EFTA01326675

FAA AIRCRAFT IIEG/STRT CAMERA WO. DATER 2 - 24 - cM . • . .e...+ q.14 er aser 0 MAJOR REPAIR AND ALTERATION resat Oat OS .. ......= (Airframe, Powerplant, Propel ler, or Appliance) I' alkni i .... ota= abet thateltatise 5»! -elk 54-Th.--nonsprs....,..... 5.. FAR Ca FAA 43 Irarials S. arid AC 4314 (a when*, man ainaf) for taborecta as rispostica crthb fern 111a non le required by Inv (40 U.S.C. 1421). Fenn to next ma resat radii only eat to eared 71 .000 for each at. station (karat 001 Friers arta M*410541. L Aarraft Make , Galan= Aerospace Model G-n, Serial No. 1085 Nancentity and Registration Mark • N88GA 2. Owner Name (As shown on natation cenifiate) Mellon Financial Services Corp #3 Address (As noon on narration cerrilleas) 4444 One Mellon Rank Center Ptttsburgh PA 15253 3. Far FAA Ust Only 4. US Idestillaitke S. Tree Unit Make I Model 1 Sall No. Ink Maim Airframe eon (As detailed in herniae* .' X Powerplat _ Propeller t 1,... —, Appliance TYR* Meaforass 4. CachnedlyStiluemeS A. Aany• Nom ad Aaiun B. Kind or Anna C. Curdles No. LANCE A. MATTESON X U.S. Certificated Mecharde MAL SAN FELIPE DRIVE Foreign Certificated Mechanic AP PUMP SCOTTSDALE. AZ NISI Certificated Remit Station Manufacturer D. lea* dim the mit. =Gs aeration roods IP the wSO) antigen a Wu 4 above and cliecabed on tha mat or thichraente line bass beat malt in secartbace with the naparemnea Mart 43 oF the U.S. Paden% Avarice Regabsfunis aid the the inform= renteted hint Is tree ad coma to the De my knowledge. Des /--- 2 1 -- eV • 4- r t Amoral for Rerun to Service Panama to the sabotity Oven pesos opocifrid below. Ike and identifier S Se 4 WY Mara baths mass pnecaboiby dm Ad:Manna of tba Faded Avalon Administer and ie CO APPROVED 0 REJECTED BY F43 Fla Iltmerh brew Mamaciuter x lassos Arabothrelon CemI Preedfin FAA Drips Resit Slides. Paso Approver by Trump's% Cada' Airerombrame amp Date of Approval or Rejection Coaxes.' / - it_re 5---- ! 526705494 IA Sigottose of Autkeizedn , Pre---e r Mithael Darnel& FAA Tes (01-14) SDNY_GM_02754161 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241083 EFTA01326676

FAA AIRCRAFT REGISTRY . CAMERA N0, DATE: -2- - NOTICE Weght and balance ar operatam bralterion changes shall be entered in the spiropriate aircraft record. An alnico artist be compliable with all prwitixtt litterOMOS to esame cormoned conformity with the applicable earworthiness xerroxraomti. S. Description d Work Accomplistatel (If mane mice is repay& ma= =Skald =two Woody with =matt emmohly rot 'evasion enszt sad data wort caresteied.) December 28, 1994. Gutfetrcam Aerospace Corporation (GAC) Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Cakficate Data Shea AI2EA. Aircraft in-service data = 1856.3 hours At 763 landing.- 'Refer to the following FAA Approved Data: Gulfaresm Aerospace Corp. {GAC) Aircraft Service Change , (ABC) 263 SUBJECT: PLIGHT CONTROLS (An 27) FIR VATOR BALLAST WEIGHT COVER - 'it: REYOVAL dated May 11, 1994 clalP CODE 97239th; GAC ASC-263AM1 SUBJECT: PLIGHT CONTROLS (ATA 27)21,11VATOR BALLAST WRIGHT COVES - REVOYAL dated July 15, 1994 <CMP CODE 972391)1 aid GAC ASC-263AM2 SUBJECT: PLIGHT COIVTROLS (4M 27) ELEVAPOR BALLAST WEIGHT COVER - REVOVAL dated August 26, 1994 <CMP CODE 9779yz>. Note: ASC263 Abe cancels and suPenedea ASC-263 AM1. The purpose of this Aircraft Service Change(s) is to remove ballast weight covers from the left and right elevators and rework the existing ballast weights. Removal of these Coven will provide easier access to the ballast weights for impaction purposes• thereby helping to detect and prevail the chance of corrosion in the Mire Removed left and right elevators from the aircraft in accordance with the GAC Computaized Maintenance Program (CMPI work codes 273007 and 273008. respectively. I.E.FT ELEVATOR RI El EVATOR DATE CODE 11-88 11.88 old PART No. 1159C820002-S9 1159CS10001-SIO new PART No. 1159SB40518-1 11595B40518-2 SERIAL No. 1086 1086 BALANCE DATA BEFORE ASC-243 AFTER ASC-263 0.01N/LBS NOSE HEAVY 0.0 INXISS NOSE HEAVY 17.6 INIBSNOSE HEAVY 14.6 BULBS NOSE HEAVY Performed all of ASC-203's modification instruction effective for secret S/N 1085. Installed parts are listed in ASC 263 pages 8 and 9 for Kit 1 end were furnished by GAC product support Savannah GA Performed required inaPection of both elevators end did ma fmd any conteloi Checked and balanced both clews:es in scardance with instruction Gpry Maintenance Manual Chapter 27. Installed the left and right elevators in accordance with GAC CMP codes 273007 and 273008 to tbeir proper positions on the aircraft Performed elevator control rigging check in accordance with GAC CM? code 273005 and performed gust lock system function ter in accordance with GAC Cliff code 277015. Recorded compliance with this FAA form 337 in the sixtraffs maintenance records and maenad the aircraft to flight status. • A weight change of + 10.0 pounds st horizontal arm 939 was made to the aircraft's Iconic weight and balance repot. 1= bats preyed fin "wind by: a Deadly =MD La% (WOW= 3S0 PM NO ADDITONAL MN= all ATTACHED. MOW 0 Additional Sheets Axe Attache] ‘4011116; t, • - SON Y_Gi.1 _02754162 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241084 EFTA01326677

lAA AIRCRAFT REGISTRY CAMERA NO. DATE, -2 - 3— 0 MAJOR REPAIR AND ALTERATION d ins (Airrinilei Powerplast. Pc0PcileT, Of APPIlloce) na...u.... aearem. gas a. ii Baia T. /mule oat, otrat mts. 5 -1 .... -If) 6.2 baSTRUCTIONS: Pitacetypa al mod. SA* FAR 43.9. FM 43 Mose B. ind AC 43 SI de ditampara naiads bad) for norm= era dmoseto of die toed Ills roxet is WS by law (49 U.S.C. 1421). Fein to report on road Medd PIMPLY net to 077.01 /I .000 b men add doted. (Soden 90i Federal Malian Ad of NMI I. Airasfr Make Gul (stream Aerospace Modal G-IV Saul No. INS Nabonabty and Reparation Mark NSSGA ' 2. Owns Name (Pd i/OWII on reparrabon batiks'.) Mann Financial Services Corp 03 Address (As shown on nigkitnnon terofinee) 4444 Om Menem Bank Ceiter Pbaaborgb. PA 15258 3. For FAA ties Only 4. US Idacolecalko 5. Tote Unit Make I Mudd I . Soial No. •.... RADS I allege Aidruld (As deaczthed in Item I above) na nn•• ••••""n" X PowaVant Propeller APPMeco TS,* abotaatarer • -' 6. Cahn* MatemaP - A. Allays Mars ad Sao B. KIM of May I C. Cobb:m14o. LANCE A. MATTESON X U.S. Certificated Mechanic 8560 E. SAN FELIPE DRIVE Foreign Certificated Malunie AP 1864049 SCOTTSDALE. AZ ansr- Catficesed Repair Station Maitufichner D. Reify dal dta cm* wird Merton mods to Oa SION idadiRad lb item 4 toys and daienbod m Wa maw a madam= Sao in teas mai la accordmea with We againeams of Put 43 of iba U.3. Folded Masan Raplaixo ad datOretefomsodon Rostatod halm is trot and mom to the be of kacodatip. Dale ' • /i - Ze fiv o, 7. AMOS ke Ran to Santos Pam tots dadaddy zWa. yam.' apocified Maw. S a lanai:din in 4 Will ibly4dAd al Ih• =MIN pluccibid by the Adaddausor °fed hard At Aelnsieldnom and is ID APPROVED C REJECTED BY - FAA Ma Rimini. later Alddllbalset z IM*4646 ARIlltpliba ober (5pACY) . ' YAADalipab Rapt Dem Pawn Approvad bj 'troupe CS Airoottbssa Orme Date otApprovd a Itcitebon i - if- fr . cetera, *t seemboNo 526105894 IA - ' Spume of ' " ' ' Malmel DalndllY FAA In /37 (03.94) 9 - 1111/41 1‘ .. A.: i1/4,44S,,,ak" .19 learela2kack-s,%.. : SDNY_GM_02754183 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241085 EFTA01326678

FAA AIRCRAFT RICERS'S CAMERA NO. DATES December 28, 1994. Gu&tram Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data 1856.3 hours & 763 bindle. Refer to the following FAA Approved Data: FAA Form 8110-3 date 12-3-93 for Gulfstream Model G-1V identifying Gulfstream Aerospace Corporation drawing number SE25201105 REPAIR, BLUED F5793.75 Rff (MAJOR) including E.O. Al dated 12/2/93, as FAA Approved data signed by John G. Wilder Structures DER SO-483. The purpose of this project is to repair damage to the Fuselage Station 793.75 bulkhead that was caused by improper engagement of the GUST LOCK system. Repaired the "-901 BLKHEAD" FS 793.75 to conform with the above listed drawing. Replaced GAC 1159C20509-26 bracket (located at Water Line 110) using MS20470AD5 rivets and optional HL18-5 hylock fasteners as required. Performed gust lock system function test in accordance with GAC CMP code 277015. Recorded compliance with this FAA form 337 in the aircraffs maintenance records and returned the aircraft to flight status. The effect of this change on the aircraft's weight and balance is negligible and no changes were made to aircraft's basic weight and balance report This is • compute mauled foon prepend by. Michael Donn*. . WORD 6.04; 01/02/95134 PM NO ADDITIONAL SHEETS ARE ATTACHED. gams D. Additional Sb:eis Are Attached • „ -airs ‘1.,;SNiertpkz., SDNY GA4 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,_0 an 2754164d 17 EFTA_002410116 EFTA01326679

el MAJOR REPAIR AND ALTERATION 0 ii Dgaris• (Airframe, PowerpLant, Propeller, or Appliance) d Triniermim riSd 'slim Adam/40•••• a.... a 4. onacid I* FAA ow Owls Ma Ilearthasiot 5)4. eCS 0 INSTRUCTIONS Frts wtat* ad 4,117109 5MFAR 43.9. FM 43 APlakt 8. arid AC 43 9.1 (or Man aka tot) for drat rind dsposliced of ahem. Ilia report 4 oanid by WA (49 ll S.C. 1421). Faa to ran as an 4 SF MIMS nal to mad SEWS Rs wa ad. at, (Sadon 901 Federal At Ad of 1958) I. Aircraft Make Gultstream Aerospace Modal C -IV Sand No. 1085 Nationality and Registration Mark MEGA 2. Owner Name (As shown on reargion =drama) Mellon Financial Services Corp lO Address (As shown on registration mite) 4444 One Mellon Bask Calder Mahwah. PA 15258 3. For FAA Use On) • R I DS Ideadaikation S. Too Unit Make . Model Scrod No. Reps Sage Airfhme (As descobed in Imo I above) X Powerplant • PropeDer . Apphanee The Materszr 8. Cadernall7 Mallernme • A. Agiall It ad Mare . B. Sled of Agency C. Coles No. LANCE A. MATTESON 150 L SAN FELIPE DRIVE SCOTTSDALE, Al. MSS X U.S Certificated Median° AP 1864049 FONIAP Certificated Mechanic Certificated Repair Station Mandamus D. I comfy Rs the reps atm shams made to the °nth) toned ea seen 4 above ad dmatted tette more or arm= bum We tom made in empress SA the sequireinexes of Pat 43 of the US Faded At Regahaims mid din We inf=oncm fornislutl hennas trot ad cooed radiate of_m, knowledge. _ Dent Snymuie g -' •2 54- tY Ce 7. Approval for %Moro to Bona Pursuant's, WKS Om person specified bdow, the nail Sated is km 4 seer isiqoaad laths ems proositod by dis A na albs Pedant Arledge Athrdsdansion ode T APPROVED O REJECTED BY MARL DES* Rymer Minufactuter inapiciice Anaolizstkei COS (Spa) , FAA Doormat Reps Swim pan Approved by fl agon Clear Mrworthlas 0roop Date of Approval a Rejection I .7k . it Coolies et ClagmlitS146. - 52670504 IA Aril= Or . . . . ..... .....--.. Weasel balmily NI* .:+a 40 111S 110 1.%t-t.s. A EDIritaM_0275416 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241087 EFTA01326680

FAA AIRCRAFT REGISTRY CAMERA NO. 3111 DATES - 2-9 (145 NOTICE Wright and balance or operating honttoon charms shall be entered in the appropriate eirmen record. An skeleton roust be compatible with all previous alterations to assure conimued conformity with the applicable Swarthiness requirements Dnatptko of Work Accomplished Of mon sax is required. tech addctional glues Identify wish &mart ratiorckty red mom= mat end Si work completed.) November 30, 1994 Goats= Aerospace Corporation ic.Aci Model G-IV. Serial Number l06S, I.O3BGA, FAA Aircraft Type Cediticate Data Sheet AI 2EA. Aircraft in-service des - 1856.3 hours and 763 landings. Refer to the following FAA Approved Data. FAA Form 8110-3 date 12-22-93 for Gulfstreant Model G-IV identifying Gulfstream Aerospace Corp drawing number SE05813101 CORROSION REPAIR BALANCE WEIGHT INSTL AILERON as FAA Appruvcd data signed by John G. Wilder, Structures DER SO-483. The purpose of this project is to inspect and (if necessary) repair all balance weights and holding straps of the LH and RH ailerons. This inspection/repair involves: A. The removal of the left and right aileron from the aircraft B. Removing and identifying the straps and ballast weights to gain access to the balance beam assembly; C. Inspecting the weights, straps, balance beam, and attaching hardware for corrosion; D. If corrosion is found, the removal, preparation and/or treatment of the affected areas; and E. The proper. re- assembly, balancing, and attachment of the aileron control surfaces to the aircraft. In accordance with the GAC Computerized Maintenance Program (CMP} coda 271013 and 271014 removed left and right ailerons from the aircraft Removed the 1159=0602 straps and balance weights from both Maus. Identified all taps and ballast weights for proper re-assembly and inspected balance bans assemblies. Paformal inspection of both aileron assemblies and attaching parts in accordance with the above referral to GAC Repair Dwg The inspection revealed: balance weight straps had no corrosion and Wand weights had corrosion. Performed REPAIR PROCEDURES of above relayed GAC Repair Ds% step 4. for BALANCE WEIGHTS, including um:ructions contained at Engineering Order Al for the drawing SE05813101, dated 11/21/94. Using the original I I59CS20602 straps. installed the treated aileron ballast weights to their original position with new attaching hardware. In accordance with the GAC Maintenance Manual Chapter 27-0, Flight Control Symms, check the balance of both ailerons; LH aileron 20.05 inAbs. NOSE HEAVY and RH aileron 21.89 in-Abs. NOSE HEAVY (tolawice 0-32 in/lbs ) In accordance with GAC CMP codes 271013 and 271014 re-installed the left and right ailerons to their tipper positions on the aircraft. Patterned aileron control rigging check in accordance with GAC CMP code 271005, Performed aileron manual and power system operational tests in accordance with GAC CMP coda 271001 and 271002 respectively. and performed gist lock system (erosion test in woad:ma with GAC O3.(P cede 277015. The aircraft was tan Down by two appropriately rated pilots and it was determined that the repair did not change the flight charadaistics or substantially affect the flight operation of the aircraft Recorded compliance with this FM form 337 in the aircraft's enaidenance records and =mudd the aircraft to flight status. No changes to the aintraffs weight and balance resulted from this repair. This I • mews. sad fen wpm.] by flits I Daselly. Mord t Oc OVUM 31/ fie NO ADDITICROL StIEETS AM ATTACHED. IND. AdektionallSheets Are Amidst .v?..Crtai. • SDN Y_GM_02754 166 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241088 EFTA01326681

1‘ 1431 bar --3r AA AIRC CAMERA NO. DATn 12-7-94 0 MA.JORREPAIR ADO Alin RATION us tn... - 4 ....... (Airframe, Pan-plant Propeller, or Appliance) 7444 A4... - . . Mialens.• WIN. 2115013) Twat Use Ody OSC• 1416thalit* 9c - e :. il 1 inSTRuCT0NS Print or type all entries. See FAR 43.9. FAR 43 Append:A O. and AC 43.9-1 or subsequent IVYS len thereof) for illitIlaCti011S and dispootion of this form. This report is required by law (49 U.S C. 1421). Fain to report can result Ina civil penalty not to used $1000 lot each such violation (Section 901 federal Aviation Act of 19583 I. Airmail Make Gull-stream Aerospace SciaLNo. VMS Model' G-IV Nationality and Registration Mark PIMA 2. Owner Name (As shown on remotion caufiate) . MELLON FINANCIAL SERVICES CORI' 1O Address (As shown on zegimmian certalost0 4444 ONE MELLON BANK CENTER PITTSBURQL PA 157.31 3. For FAA U se (My A Don Ideonfkaaloo 5. Type Unit Make Model I Serial No. Repair I Minion Airframe .1 (As demated in Item I above) . z. . X Powerplard . . . - PropcDer • Apphance - Type. bbnatenner - IA Geothermal, Statement - _ .. A. AnneysI4aee i mad Addnea B. X Kind of Agency C. Cenifecets No. LANCE A. MATTFSON 1560 F. SAN FELIPE DRIVE SCOTTSDALE, AZ 8.5291 U.S. Certificated Mechanic - 1164049 - - Fenian Catenated Mechanic AP Coat:mated Repair Station . *Mainifactitta i D. I certify that the repast Sot Samoa made to the atri(a) identified in hem a above eat chanalied on the reverse or anectnnetas henna have been made in err:edam" with the rocrairesomus of Pin 43 of the US. Federal Aiitin Ripsistions and dim the biformoon forrisbed herein is mu and correct to the bat of isiknowlecbtA Dust 06 2 7- fly Signana c}sjit i utbonzed ' T. Approval to Rem te Servke Parsee* .1dmithansits BY the amhority given pants specified ban. the well idsmified in item 4 ow nmpened M the manna presmbed by the of the Federal Ablation Adenainion god is LEI APPROVED O REJECTED - FAA 111- S:Ndsd, bspeaer 'manufacturer r ile/peon= Ainhonation . I Other (Spsify) FAA Dengue Rept Station Palos Approved by Tramport Cards Airwatlainam Orono Dale of Amcor' or Rejection centhno• • . . Slipmtne of Authorized • ' "IPS". - . IrCrIs i Miami Dino* . FAA Perm III (9144) -- " 4 •442C4k }RFC"- rilrat lane - . SDNY GM_02754167 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241089 EFTA01326682

sells743144Wfisan661opiaafte„. eszro- 2,1 : NOTICE Wright and balance or operating !mutton changes than be entered in the appnapide aircraft record An alteration must be compatible with all previous Litt:canons to assure continued callow* with the apphcable airworthiness remonements. _ I. Desertptlen °Mork Accomplished (If mat spere is reman& mach eictitiocim slaws Wen* coat aircraft =Monate,' ad resisinsion mark en4 etas work completed) In older fp provide continuity during &Rule inspection;, maintenance. and alterations a true copy of this FM Emil 337 is fecund to be kept on board the Smart as Song as the alteration remain in effect. AUGUST 26, 1994. Gulfstreare Aerospace Corporation 'CAC} Model Cr-IV, Serial Number 1085, NM& FAA - Aircraft (Type Certificate Data Sheet Al2EA Aircraft ill-Set data - 17116.6 hours & 736 landinp. • Refer to the Mowing FAA Approved Data:- FAA Fonn 8110-3 DATE 7-1R-94, MAKE Crulfstrearn, MODEL GIV TYPE Airplane, NAME OF APPLICANT Cruftgream Aerospace Corporation, LIST OF DATA IDENTIFICATION 115%841296 (Engineering Order Al), TALE BRAKE ENHANCEMENTS, DER- R. IPESSON- SO761, SYSTEMS & EQUIP, and GAO Aircraft Seniee Change 296, Part 12 Drawing 11591430036 BO 63 Ground Spoiler Reanictor and PartM Drawing 1159SB40560 Bnkc Bungee. The purpose of this alteration is to improve `brake-by-wire ' operation by installing restrictors in series with the ground spoiler actuator input pressure ports to alleviate hydraulic demand mid modifying the brake pedal bungee's to obtain increased tension. Performed an of modification istmuctions for Part 11 and Pert Dl orGIV ASC 296 <OAP 977960>. AD pas were instaBed new and obtained from Gullet:cam Mosinee Product Support, Savannah, GA. - Removed four each Pal MS21916164 union &tato from the press= input ports (PI and P2) of the two ground spode( actuators and installed four each PM MHX031590013A R.estrictor &Pap with new "0" ring pickings, 1159020011-06let accotdance wit the instructions contained on GAC Drawing /1550430036. Reworked d each GAC P/N 1139CA0040-x Brake Pedal Butte's to P/N 11595B40560-x confagurabon in accordance with the insbuctions contained on CACThawing 11398B40503, 0W8RACEPETtea, BlthiGEE BIUKEOUT &KNEE FORCE .ADJUSTMENT Sheets 1, 2, & 3 34•3. Installed the Bake Pedal Bonne's as follows: poonort • • P/N - .WMALMNSIOti Pia MINE ccer coog Pilot's Left 1159%40360-1 0211 241 LBS. 43S LBS: 324171 Pilot's Right 1/39SB40360-2 C039 . 24.2 LBS. 43.6 LBS. 324172 Co-pilot's Lel 1159313405601 03197: ,..- 244 LBS. 433 LB& 324173 Co-plot's Right 1139SB40360-2 0337 243 LBS. 43.4 LBS. 324174 Successfully performed GAC <CMP 276001>'Caound Spodet Sittet Operatiag:fort enentiot> Whed Brake Systais- Panaion Test and <CAW 324103> AntiSkid System-Fonction Test. • • . A Cammd Taxi operational test was conducted by two appropiately tided pilots: The pilots tested for ptoper blue response at =Ma taxi speeds from plot and copilot positions while opaaring wing flaps, goad spotless, and nose wheal steainq. No ainVI620 409600t”cFenwitcti • Recorded compliance with this FAA form 337 in the aireratts trtailnalat/Ct to:aidsend retuned the aircraft to digit status The ef&et of this dense on the ant:ars basic weight end balance wait neftlagTh-ble end no Merges were made to the a “ad's base 'stied end baba= report. Ns hese/Poe named kiwi senewirs by. Wood bcaially. watt) ass. 01024,1;43 tai - _ NO ADDITIONAL MIMS AiLL AITAOIED. -O -Additional Shall NeAtiebat ' --7a•IrTvik SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8 SONY G , 9, 10, 15, and 17 G502754168 EFTA ornai non EFTA01326683

toured OIOD ... oda C MAJOR REPAIR AND ALTERATION ler FAA Theo oyes (Althaver, Powerplant, Propeller, or Appliance) ,............ . .... Oen 14eadmiee .0 C- r -510 evSTRUCTIONT Print Or type all entries. See FM 43.9, FM 43 Appendix 9. and AC 41.9.1 (or subsequent revision thereof) for instructiOrn and disposition of this form. This report is required by Imo (49 USG 1421). Failure t0 report can result In a cUll Penalty not to need 51.000 for each such violation (Section 90l federal Aviation Act of 1954). I. Aircraft Make Colrain:P.M Aerospace ,Model G-IV Sail No. 1085 Nationality and Registration Mark NSSGA 2. Owna Name (As aberion on repatrwion arrtificata) MELLON FINANCIAL SERVICES CORP BD Address (As thorn on reamine,n cen.Lime) 4444 ONE MELLON BANK CENTER PITTSBURGH. PA 15153 3 For FAA Vieth* .4. Uole Ideal/Ratko - - Line Unt Make I Model I Sall No. • Repair Ann Airframe (Ai described in Item I above) X . • Powaplant , \ ... Propeller Anoltance TYPe Mmttfattarer - a. Cadermay Matemeor A. Matey, Sc. end Addreas .. • A. KW of Niamey . C. Octilkela No. LANCE A. MATTESON X U.S. Catifaceled Weber& 8548 E. SAN FELIPE DRIVE port Lea ca4theatal Mechanic AP 1864149 SCOTTSDALE, AZ ISM Catfitated Rata &Mae I Martufaataa D. I ratify t the repair mar Mention node to the onn(s) identified m non 4 stow and &Shed oa the muse or gtschwints hem have two made in r.conLince wilt the napineemm of Pan 43 of ths US. Faded ArketooltecoMions me that the incantation furnished hem" is true nod coned to thebera 0 my lascrwiedge Owe g 7- ft( friPernrefirralrifrldrE . -----.7e.C„ C, 7. Approval for Reran le awake Ps MIS wrap &V pemommacifiM below. the unit HSU! la item 4 was torplaae ha the mew prescolve by the . Ahead. Attie Petted Avilioe Adoiron and S 0 APPROVED 0 REJECTED BY FAA Pk Or WS taps Mandictura x lxvictica AildiCS31% .0her(Srpeci(y) . I: FAA Dmipm Rise; 48691 . . .. . Pawn Approved by Tnospxt CisinAtecedirsettittop . Dale plApprova or Rejection .8 — Z9' -s V °AIM. IF " , DeOritialt.- SISM5491 Lt gpaRpm Of Michael Donnefry • I M-4.D.O/I0/4..",.. • •••• • ••••• SONY GM_02754169 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00241091 EFTA01326684

FM AIRCRAFT CAMTRA NO. ISIKY DATE: 12 -9- 74 • NOTICE Weight and balance or operating thretabon changes shall be entered in the appropriate airerae reconi An alteration must be cons pa olge with all previous alterations to ass= continued cantos:miry with the applicable airworthiness 11881801:Mall3. 8. Dvscriptlec of Work Accomplished of more spice is remand. each adduiciutl them. thmtity with that mdonally and mist mark and dee work completed.) in order to provide cordhurty during future inspections, maintenance, and alterations a true copy of this FAA Form 337 is required to be kept on board the aircraft as long as the alteration remain in effect AUGUST:26. 1994. Gulhtream Aerospace Corporation (GAC) Model G-IV. Said Number 1085, N880A, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-savice data ••• 1786.6 hours. & 736 landings. Refs to the following FAA Approved Dalt GAC Aircraft Service Change (MC} 232, SUBJECT: ICE AND RAIN PROTECTION (ATA 30) WING TEMPERAWRE LOW MESSAGE — PROVISIONS, dated December 17, 1993. The purpose of this alteration is to activate the "WING TEMP LOW" message (Amber) on the Engine Instruments Crew Alerting System (EICAS) and mask alert if the wing has not reached 100 &tors Fahrenheit after two minutes from being selected ON. Performed all of ASC 232's modification instructions effective fOr A/C 1085 except for the following minor dm.iations: • Coacplt Overhead Panel: Existing wires1H151D20, IFINA20, 2H151C20, and 2E126A20 were replaced with new NSW. 22759116-17 to ft GA0335)4L22DS contacts provided with new wing anti-ice:wit. Avioniat Shelf Assemblies: Al added wire connections to the Fault Warning Computer(s) and Data Acquisition Diggs) 'Mt made directly to the rack <on:tenons) Stead or through the shelf disconnects. Main Junction and Relay Panel: Wets IH152F22 and I.H152X22 was remove from T113M positions If and G respectively and spliced together. Win 2H152.1G2 and 2H152F22 way rand from T720 position G and K respectively and spliced Wither. Wire H9076B22 was spike to wire 1H1S2Y22 near Data Acquisition US MI, 95A4PIB pia, 17. Wire H9071322 was spliced to wire 211i 32T22 near Dan Acquisition Und 12, 95A5FIB pin 17. Wen /49078A22 and H9078AA22 were spliced bribe( with wire I HI87D22 nor connector NAINC pin 89. Wires k19079A22 and 119079AA22 were spliced togetha with wire 2H1I37Dn near connector Nmptc pin 91. . AU of the deviations that wire made to the apprerred design %Senecessary to provide for compatibility with existing approved configurations: It has been determined that the deviation made did no after the intent or operation of the approved eiraeft savice change, • • -- - • • All parts were provided in kit fotro and obtained from Gulf:strain Arrospece Produh Ruppert, Savannah, GA Sucossfully performed ASC 732's operational lest. Recorded compliance with this FAA loon 337 in the aircraft's rneintenan ce records and reigned the aircraft to flight . . _ The effort of thirchange at the aircraft's basic weight and balance was negligible and no changes sect rna..te to the aircraft's hthic weight and balance mon. lli.as =war romiud fonaprrmul br. aOdsI Omani,' WOAD 6 Oa 01/2691Strt PY NO ADDMONAL stores AtEMTACIIED •E`te 0 Additional Sheets Are Atractu:d • • ST-,- .• • ....atejalate-, . .klietialHAPP4 1 7:7- -.7 J . • 4 . ••• ' -1;4 • • • • SDNY GM_02754170 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241092 EFTA01326685

P =nth • DATE: I 2 _7_ 94 CA1CRA SO. I ram Cow :If On I2 MAJOR REPAIR AND ALTERATION Fiera manse us tarown en ' -- - (Airframe, Powerplatot, Plojoeller, Or Appliance) sr...seer ..... Me kleatifisetian 2e (,- ics4 O INSTRUCTIONS: Mot of type an entries. See FAR 41% FAA 43 Appendix U. and AC 43.91 (or subsequent revision !Steen for insqintions and disposition of this form. This report Is required by Una (49 US C. 1421K Failure t report Can result Is a civil mobil, not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1950). 1. Aircraft Mats Gulfstream Aerospace- Model ' G-IV Said No. 1085 Nae003MY DM Rogistsation Matt NSSGA 2. Owner Name (As Amen on Illtalle01/ califlone) ' MELLON FINANCIAL SERVICES CORP ICI Address (As shown on DOS:Sion Patina.) 4444 ONE MELLON BANK CENTER PITTSBURGH. PA 15253 3—For FAA Uwe Ott A Unit Mead:Sena= 5. Tne • ' . Unit Make I Model I Sail No. papa Minion Airttame *r n :•• ••••••••"'• (As desenled in Item:above) X Pow*** Propeller TYPe hernefieraree 6. ConterenttY Swetweseed A. AP:00 9 Tleme and Address B. Rind of Amoy C. Cctk*s No. LANCE A. MATTESON X US. Certificated Mechanic. A - 856$ E. SAN FELIPE DRIVE FeeWen Catifioded Mechmic ' AP 1364049 SCOTTSDALE, AZ 332.58 Certificated Rosa SUM* Manufacturer : D. I certify that the rep* endior ekeraion male to the noi(e) identified in item 4 tow end detailed on the &vav or enachmenu lino have tem male hi leatednoce with the :Neiman= *Pr 43 of the U.S. Fedenl Avisean Replaeom and via the infixivenon fornithed her* earn wad coma to the bed of my Dunned* 9 -,77 rr G. 7.' Apart:9M for Return to Savke Patio the ember* given moons specified Mk* the ant identified in son 4 win hopeaed in the wanner tresedbed by the Aflisizeloratthe Fail Avid= Admlainice and IF OD APPROVED 0 REJECTED BY FAA De an* Menu:Setae* X **Mon Awhothation Other (speedy) FAA Nips Rep& Station I Paton Approved by Troop* CUBIC" MIWOOkillall. Cecesp Date of Apperef or RMection • - 9 —a9-- IY comma., Brit= of Deeps* we . 526705494 IA' • Michael Dcamay SDNY GM 02754171 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241093 EFTA01326686

-=.;,17.17...-4.-fttrftralle„wPnenaNCeinwinvan'7"-'7, IM Allts.RAnlatTgr - - CAHEPA NO. DATE: 1 2_ 7_ 94 NOTICE • Wright and balance or operating limitation changes shall be entered in the amperage aircraft record. An alteration tut be compatible with all previous aluranons to assure continued conformity with the applicable airworthiness re:pit-tents. I. Desaiptien el Work Accomplished (if more span b required, attach addeacual sheet identify wida entry and regnewrion mark rid der a work compleuct.) In order to provide continuity during future inspections, maintenance, and alterations a true copy of this FAA Fame 3371$ required to be kept on boird the aircraft as king as the alteration remain in effect. AUGUST 26, 1990. Gulfstream Aerospace Corporation (GAC} Model O-1V. Serial Number 1085, N886A, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 1786.6 hours & 736 landings. Refer to the following FAA Approved Data GAC Aircraft Sent Change (5C) 255,.SUIEUECT: INSTRUMENTS (ATA 31) SNAPSHOT SWITCH INSTALLATION, dated May 5, 1994. - The purpose of this alteration is to provide thc crew with a switch that recants engine parameten in both Fault Warning Computer's (FWC) non VI)Litilc memory. Paformcd all of ASC 255's modification instmcdons effective for A/C 1085 except for the following minor deviations: • • Cockpit Overhead Panel: Installed - SNAPSHOT- switch ASC255DSI on overhead panel in the spare vacant position adjacent to APU fire test switch. Comucted ASC2.55XDSI switch tin wiring as follows: Pint...are FD9030A22N to ground block E2 pin W; in 2 wire FD90213A22 to 318A1P7 pin small U; no why Jumper 22 to Pin IT, all wire FD9030B12 to ground block E2 pint Pins 5 79 All no connections: MA wire W5281.022 to172N Pin D: punB wcc FD9029A22 to ocancrior 31ILAIP7 pin small V; and pin 1p wire FD9031A22 to commenter 318A1P7* small W. • Avionics Shelf Assemblies: Connected wins from 318A1P7J1 ai follows: pin small U wire F09028B22 to Annannator tights Dim and Test Box- 29AIP2C pat 11; pin small V wise Fusvats/2 spliced to wires FD9029C22 and FC9029D22connected to FWC I I •95A IPIA pin 81 and FWC a 2 95A2P1A pin 81, respectively, and pm tan W wire FD9031B22 to Annunciator Dan and Test Box-29AIP2C pin 64. All added wire connections to the Fault Warning Computer(s) and Annunciator Lights Dim ted Test Box were made directly to the rack conneenx(s) instead of through the shelf diatom:Cs. All of the deviations that were made to the appnived design Were necessary to provide for compatibility with aiding approved eccfignaticra and allow both pilots access to the - SNAPSHOT" switch. It has been determined that the deviations made did not alter the intent or operation of the appoval aircraft service change. . • .. • - All parts were ptirdiased from GulfstrearnAaraiiiiiiProdurit finning. Sawing, GA. Successfully_perfamed ASC 255'S nperational test Recorded compliance witlithis FAA form 337 in the aircraft matte reteds and retuned the aircraft to flight stains. • • The effect of ibis their 'dotal load =WW2's %alibi =abaft. Fair fair t eNAFSHOr swath indieaas, is from the o' HEAD LTS PWR 02 aieuit breaker -8HAPRHOr Sint lamp mane &ow (When snapshot switch is prayed or during wanting fights tesOkssthan 02 ats in tnighit10.05 till in . . . The effect of this change on the aircraft's basic weight aid balance w@ negligible wid charges were made to the ainitaft's basic weight and balance report • - . NO ADDMONAL man, An AlTACRED •19-496 a Pidmonal MO= Are Attached z..s. - •yrv.ne!-I;+wfrr- ti ' I • -en h •-J-h 4i l % SDNY_GM_02754172 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241094 EFTA01326687

Fe .... csa X. norm 0 MAJOR REPAIR AND ALTERATION r 1 r nAth•oute (Airframe, Powerplant, Propeller, or Appliance) terns tilat••••• des,, siScarica 4 ts c ,. / .0 " iRSTRuCTIONS: Print or type all entries. See FAR 43.9: FAR 43 Appendix El. and AC 43.91 (or subsequehe revision thereat for instructions an disposition of this lone. This report ts required by Ire (49 US C. I421). Falun to report can result loaded penalty not to exceed 51,000 for each s Leh 'violation (Section 901 Federal Artaterin Act of 1950). I. Aircraft Make CulTstream Aerospace Model G-IV Said No. 1085 Natisnably aid Reettalion Mack MISGA 2. Owner Name (A. shown on repartee enflame) MELLON FINANCIAL SERVICES CORE' SS Address (As town orimgetricion eatiame) 4441 ONE MELLON BANK CENTER ' PITTSBURGH, PA 15253 1 For FAA Us• °ray 4. Unk Ideonacetke 5. Tmee LIM Mt I Model I Sail No. Repro APCIelon Mfrs (As dosentedis It •••••••••• ... . X Pomp= Proper -.. , Appellate TYPe Mamba= 6. CaMormity Staley= - ... - A. Aspera Nine and Addis B. Kind of Apnc C COMPlitlo: ' LANCE A. MATTESON X U.S. Caicos Mecksinic , 1360 E. SAN FELIPE DRIVE. Foram Catifteatesi Med= AP ISSN= SCOTTSDALE, AZ ISISS Catificated Repair Stag m —Manufsetura D. I catty Mt the rep & and/or aced= rude to the asps) idatitud ict item 4 above ad deaMed on the mime or metements hereto bevy been made m read= wilt the repherrenta of Pert 43 of the U.S. Pedant Let Replalems end dm the informar forentiest hicas is troe and cord to the Mom knowledge. , Date V /eV ------- r r 7. Approval for Remo to Sas Pmassatw the =MeV given ponces specified below the MI Acidified to dome me impeded SS razor preembest by dm Methstamor calm Federal Awallcm Adrolestralice ands 02 APPROVED O REJECTED BY FAA SR palm& ars Nasseactunr x thapciSionAtabodation c ater(Spedy) , FAADeepene . t Peprix &Rion Pawn Approved by Trietsgoet Casts Airouthiosse cheap Dine of Approve( or Rejection 8 —/s--- 5° se Ccormft.wN .' Desiengtee .526" M S IA • Signature of Assatotized ' - r SDNY_CM_027541T3 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241095 EFTA01326688

NOTICE Weals and balance or operating limitation changes shall be entered in the appropiate aircraft record. An alteration must be • compatible with all previous alterations to asnre continued conformity with the applicable airworthiness requirements. & Dentriptlea of Work Accompllthed - at more epee is required. each deuced Mesta dairy web secret ciacualny and minion mat and die work peefeiseet.) In order to provide continuity during future inspections, maintenance. and alterationfsv anlioopy of this FM Finn 337 is required to be kept on board the aircraft as long as the alteration ' in effect. AUGUST 14. 1994. Galant:am Aerospace Corporation (CAC) Model O.1V, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet AI 2EA. Aircraft in-snee data = 1786.6 hours & 736 landioid.' Refer to the following FAA Approved Data: Gulfstrcam Aerospace Corporation Aircraft Service Change (ASC} 295 SUBJECT: AIR CONDIT7010110 (ATA 21) CABIN PRESSURE* MANUAL CONTROL DVS7'ALLA77ON dated JULY 22, 1994. <CM? CODE 972950> The purpose of this alteration is to allow the cabin 'air pressure control to revert to snuff operation in the event 115 VAC power to the pressurization system is lost. Presently, if 115 VAC power is lost, the air pressure transducer and the outflow valve will fat - 32.5AI KI 0 MODIFICATION: Price to preforming ASC-295's modification instantiate modified the eating mita Ray & lunction pond to provide for expansion Removed 8, discarded Sating May 315A1K10, Deutsch P/N E4104 385; Exacted all of the wires from socket 315AI XXI°, and Removed te discarded relay socket 315A1XKIO, Damsels P/N 65009004.513. Installed a new Deutsch P/N 65009001.513 relay soda at eft position 32.5AIXKI0 & connected existing wires as follows: WI33D22 • A1; W132F22 - A2; H9014A20 - B1; H9015A2ON - 82; H9013A20 - B3; 09056A20 XI; & G52A2ON - XL ASC 295 DEVIATIONS: Instant:dancer Deutsch P/N 65039-008-513 relay socket adjacent to nil position 325A DOC 10 (see above) and identified as ASC295XKI instead of the relay, socket and bit listed in ASC 295. Perforated all of the wising changes shown on Figure 4 of ASC 295's irectructiont amp wires DU/113B20V and DIOICC2OV wee asserted into 326A I P200 and 326A112.00 (espectively) potation P instead of era T. After completing edam and ring out. installed a new Leach P/N 1A-W4F-005 (aka GA11335590 unto socket ASC295XX1. All of the entailed pasts were purchased from GAC Product Support Savannah, GA. Successfully pained the installation checkout listed in Paragraph B pages 4, 5. and 6 of ASC 295 instructions. Recanted =Same with the FAA font 337th thitherafrs maintenance records and returned the aircraft to flight sums. It has been detennined that the intarebaimehip between this dungy and any previously approved cooftpration will not introduce any adverse effect upon the arworthinionfthe aircraft This deemxinalion includes, but is not boded to. My modifications or deviations made did not atter Pa EMI of the approved ancralt service change; Mum performing its maided functions the operation is augment; No %at manual smedameras are require& and the installation is compatible at all previous therations assuring continuous conformity with the appleable ithWOOthilleSS requiremmts. The effect of this change on the airgartelicititial lee4ing twill be 0.03 amps added to the CABIN PRESS 115V thieuit breaker, essential 115 VACIstes:j...s, _ • ... She act of this change on the airtisfei basic weight and bitten — negligible and no changes were made to the aircraft's busk weight and balancereport • - . . .. • aercaor pared En nal by. Itdst 'Decal WOIUM ON - tandem SAMS - NO ADDMONAL !MEM All Ansium tat 0 Additional Sheets Art Attached • "fr,'. _ st: .e' • -a • _art....c-s,--?entifilsaselleSill*Pere7 . . • . .t • -44, :•••• SDNY_GM_02754 1 74 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241096 EFTA01326689

0 MAJOR REPAIR AND ALTERATION ,.....",4 MOM tine= /It IAA Ono Oily Oilkelocoirsaise . 4-ec - t's % fnoea (Airframe, Powerplant, Propeller, or Appliance) ,..SAME 'Simla MIR insminions and penalty not to Print or type an entries. See FAR 43.9. FAR 43 Appendix It and AC 43.9.1 (or subse trent revision thew!) for disposition of thks form. This report is required by law (49 uS.C. 1421). failure to report no result Ina clod weed 51,000 foe taco such violation (Section 901 federal Aviation Act of 19S 0). I. Antraft Mae Gulfstream Aerospace Model G-IV No. 1085 Nationalny and Registration Matt NSSGA 2. Owned Name (As thorn on niftstraticat arena) MELLON FINANCIAL SERVICES CORPUS Addams (AS IbOVIa 011ttOttri011 OlitiliCOW) 4444 ONE MELLON BANK CENTER ' PITTSBURGH, PA 152.58 3.. For FAA Use Thdl 4. US IdeollIcanon S. Type Unit Mae Repair Aturadon Akers (At da 1. miadin Itmn I Mon) "'in n " ********** X Powaplant Practise .. Ng Msarthamer • . — fa Coneamily Surat A. Aisayb Nine and Addreee IS KIM Mir C. Caeca No. LANCE A. MATTESON $560 E. SAN FELIPE DRIVE SCOTTSDALE, AZ 11525$ X US. Certificated Mechanic AP MOMS Patio Catificared Mechanic Cation& Pamir Station Minobetatex D. I nary IS me rapt and/or anion made to the imiaNdaithed in Eno 4 Mon and deeedbed on the myna or inedanento beneo have boa wade in sem= nth the requiems= of Put 43 of the U.S-Fedeni MIS= Rem and that the informetioo fandsbad tonin is tree =ad =tett° the bac my lamededid Dan )—ts,-5,y SiPar d 418 7. Anomalies Rearm to Scoriae Parent to the ..homy given perms specified barer. W non Modified an in 4 misspend Isi dome= preamlied by the Azteanmeor ate Facet minion Adman:aim =dal Ila APPROVED 0 REJECTED .. BY AAA Ft Semd•d• boon Memitactunar I Inspechou Ambocintion 9!1, 1(3$410 Empalme* Rent Mann Person wawa by Daemon • • • Camila Anwortkbas Oran Data of Approval ar Rejection efrr/95 1 mama. or - RearefiaaM . ST 6703494 IA Sipoovre of _... .- 7 otti ,„,," MichaelDonndly tareen511(0.494) • SIJNY' brA 0175417r • teces_1-•• • ...-.:Atalusa.: • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241097 EFTA01326690

• - • Icis,vksoi.:,:;1 AttarrAfgYegir,it M AIRC CA KERA NO. i • 12-7-94 -• • Nana Weight and balance or °Mating Limitation changes dun be altered in the appropriate atrcraR reo,rd. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable throcorthiness ro:ryercmcnts. S. tamertyttea of Week Accomplished (If more apaar a main& math %attired thects. Itlesity with siren& nsionatity and "misuse= an and claw wed cors[plaied.) in older to provide continuity during Mute inspections, maintenance, and altmations a true copy of this FAA ram 337 is requited to be kept on baud the aircraft as bog as the alteration tetnain in effect . AUGUST 14, 1994. Gulf:ream Aerospace Cbrporation (GAC) Model G-1V, Serial Number 1085, P/88GA, FAA Aircraft Type Certificate Data Sheet Al 2EA Artraft in-service data - 1786.6 hours & 736 hmdings. Refer to the following FAA Appired Data: Gulfstrcam Aerospace Corporation Aircraft Service Change fASC) 313 SUBJECT: P 4TICS (4E4 3e9 OWN PRESSURI Z477QMSTABILIZaj77ON dged DECEMBER 17, 1994. ••• aCODE 973130> - 7 The purpose of this alteration is to reduce the cabin pressure rate changes that cocoa dicing rapid power lever reductions at high altitude. This alteration provides an electrical circuit to reset bleed air pressure regulation from 18 PSIG to 30 PSIG when the power levers are retarded below pedestal quadrant angle In • retarded power lever descent. without ANTI-ICE oft manifold pressure is maintained above 20 FS1G. This circuit is routed through the 2500 FT AGL horn mute relay, disabling the circuit when this relay is activated Selection of any AN1T-ICE function also disables this circuit. ASC 313 INSTALLATION AND DEVIATIONS: Installed • new Death P/N 65009-001.513 relay socket into a vacant tad position near 32.3AIXKS8 and identified the socket as ASC31350: I instead of the relay, socket end thicket hued m ASC 313. Performed all of the wiring changes shown on Figures 3 and 6 of ASC 31Ts ismachons. wept for the following deviations: Wires D0002820 and 09002A20 were insetted into 326AI P200 and 326A11200 (respectively) positions instead of maga; Warm D9004A20 and D9004B20 were inserted into 326AIP2OP and 326A11200 (respectively) position It instead of small/ Vises D9004820.139004C20. and H428C20 was inserted into 326AIT/16 M positions K. L, & AI Despettively)-, Wire D9007A22N was emoted into ground block El position/AMOS of El 1 positio' n lit After completing weirs and rigout, installed a new leach P/N .1-W4N005 relay (aka. OAR833NRI) Ito socket ASC313XK1. AD of the installed pars were parbased from GAC Prod= Support Swainish. GA. SurionsfullY Performed the instatheion checkout hated mEaragnph E pee 3 of ASC 313's instructiess. Note-Athed Signal • Service Basin Numbs 3399022-36-1646 has ban previously comPled wild Valves 541.1 and Sala we accessible by removing UPPER pylon panel 2 on the impactive side. Recorded compliance with this FAA form 337 in the Scat's roShmance records and returned the aircraft to flight status. It has been determined that the intentiarionslths between this change rd any pthiously approved configuration , fla not /misdate any adverse effect upon the airworthiness of the aircraft This determination indudes, but is not limited to: My modifications or deviations made did not aka the intimt of the approved aircraft service Mange, What performing Its intended fime5orts the operation a automatic No flight manual supplement! are required; and the instillation is compotthle with al • previous durations assuring continuous cont.:achy with the applicabk airworthiness requarements. The effect of this change en the airmars dectried le:dinged] be 1.7 crops added to the etseraid de bid (0.1t7•5 apgsb CB 242 SPEED BRAKEFLAP ALARM and 0225 to CB 262 SINGLE PACK). " The effect of this change on the aimata basic Weigth and botanic was regfigilde and no changes were made to aiseraft's basic wthda and balance repth. nit • sthow wens twos w4nNel . . woometiiiitareniAsAgraiatcr'laar 0 Addi6ortal Meets 4r6 Matited 1 • SDNY_GM_02754176 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00741098 EFTA01326691

MIMMIUME CAA A J. *WRAF I ELGISIR ' • • _ SSW Cif -LI__ • - - 410 MAJOR REPAIR AND ALTERATION I......... 010 Wm IFeC Yet IAA CM OM con anasnaaos -k -elio (Alston., Prewarplant, Propeller, at Appliance) .17nme•••• n....... .5 =IONS: Mat at type as autos. St• FAA 43.9. FAA 43 APMMix F. and inunations and disposition of tint fn. This report's swim! by Lt. (49 U. penalty me 10 o(4•4 SI.000 N4 atell such Sanaa Manion SO I NOM' Avi9 AC 43.9.1 lot subsequitot nation thentoh for C. 14214 Nan to report tan rank initial. Ion Act of 195t. I. Mud Mac • Gal Wean Aerospace Model GEV Saul No. IOU ?humbly and Registration Nick NRSGA 2. Ouns ;we on nentenatai cenifcia) MIANCIAL SERVICES CORP CI Address (Ai shorn on nista= catalog') 4444 ONE MELLON RANK CENTER PITTSBURGH, PA Ina 1 VAR rm Use 0.1, i Ts US Nib Met ( Sod No Ramat Alan -...• . I Airtnans ii hem I 'bow) ••••••••••••••"*" Amanita • • Propsila Aglow • / - Paseasst ik• clear hA. mows to el Mira 1 a Kad of Any C. Lea A. MA11111074 I U.S Catiticated Metric • BMA E. RAN MAT Darn Foreign Cated Modal* 3COTTSDALE. AZ MSS Cataloged Raw Stet MCGLaktita D. I amity Os ma ncnr Sas alma ion. iii en tint(s) tataitt le 4 eon mod dtecolect asactinata bona bap on ends a .ccida• Ina the rapzirentan of Pot 43 of as Us Feint Nat dr adeassecc Monad bac A Cup isl carat to ths falconry teowk4Alt Drs e- 1 7- f y sis ottaiis . . 2 r7 4"1C.S. 7. Afarenitse Rani liana Mfluml IF 41* 4411A4sY lima A MASS Sow. tap ana itathid ia Ilmi 4 Me arapiard a is !me pandasa ages Aiwa of tht Fadden Avalon Asa•tatfon ad in IS APPROVED 0 REJECTED . BY " IAA. goon sir c bon ltscan z talon Acarsige . . IFAA Dagen taps Oro- PO= Ascend by halm dadamworttrnan Oro. Du of Approni a Rejection I . - ? ta -sr O..§...- osem...N. OWNS M -:- • sone of Alameda II41;iC: 01 edictal Donnelly Sigiczaldifida;a ss SDNY_GPA_02754 177 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241099 EFTA01326692

-,› - • -." 11~ ""4- • .iii;!~~1h‘4 - ir> NOTICE Weght and balance or opetalang I/sic:ion chars& shell be as in the approrrale sacral mooed M alteration must be 0'i:imperilla wØ al previous iheriaoniiii aware ~cod conformity mA the applicable erwarchiness requirements. . IL Deeertentia at week AconaplIdad (If mon spice ie required. such Slams Mesta Idera4 tab meal ~ay tad ~es mat wad ear wort complated3 In ceder to provide conanurty during Mure Inspections. manteranoe. and Wistaria:a a true copy of this FM Form 337 is requited to In kept on board the aircraft as king as the alteration remain in effect. AUGUST 26, I Amapa Corporation (CAC) Model G-IV. Serial Number 1085. N88GA, FAA Aircraft Type Sheet Al 2EA. Aircraft ia-testcc der. - 1786.6 bows & 736 landings. Refer to the f Approved Da FAA Fin 8110-3 DATE 7-18-94, MAICE Gudaream. MODEL GIV, NAME OF APPLICANT Glace= Aerospace Corporal" LIST OF DATA IDE N 11595B41296 (Er#coring Order Al), TITLE BRAKE ENHANCEMENTS, DER- R. 1 761, SYSTEMS & EQUIP; and GAC Aireraft Service Change 296, part II Drawing 11391130036 EO Spoiler Restrica and Pal III Drawing 1159SH40560 Brake Beppu The purpose of this alteration t ss ve 'brake-by-wire' operation by inctalling i • restrictors in series with the actuator input pressure ports to alkriate hydraulic demand and mod e pedal bungec's to obtain increased tension. Removed fox each P/N 14521916164 union the prom= and ~led four tech P/N 1111X0515900BA Pernietor anew with new the inetructims oanlainal on GAC Draw" 1159H30036 Rorocked 4 each GAC PJN 1159C40040-x Bake PØ Bunsee's to P/N in:new-tiros contal on GAC Gnaws- 113951340503 GIV BRAKE P ADJUSTMENT Shea 1,2, d 3 of 3 installed the large Pedal Sungois POQITION PM Noes Left 11395B405c0-1 Plot's RIP! 1159584)540-2 Co-plot's Led 115958405681 Co-pkit's Pistil 115958405682 Soccaufully performed GAC <CUP 226001> Gromid Spot System Operaliaral-TaL <CUP 3241 ~ton Tat w CUP 324103> Araararl Syslan-Fonetion Test A Ground Ttn operator* ten toes conducted by two mar* need pion. The pion tested rap:sued normal tam speeds from pilot and copilot par vitae apaazo wars 6W, ground galas, and nom wheel mama No Randal omsprnrice with am FAA km 337 oM acerbailiess ~is allleallhe Smart to tit& tar: The effect of eta Sir ante cafes be ale ett ben sup ~sit and es Saw we :irk b the as at, taus weight and laince report main emsear mews as orned by MSS De* rap 911 182 ArlaaeaL fl An ardzsan • O Adderana Shaft An Attached SDNY GM_027541 78 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241100 EFTA01326693

4 4.1MV:4-. - " COS4Ir SDNY GM 02754179. r........d PO. 1 . zsara 0 MAJOR REPAIR AND ALTERATION for 'AA UM 0ST of trmiore (Alsfrome, Power',lant, Propeller, or Appliance) odes sort= ••••••• - • • once stem. .OC -Tc9o. INSTRUCTIONS Rant Of (We ap hisries. Sae FAR 43.9, FM 43 rsIMehdit I, and AC 43.9.1 for subsequent revision thereof) for instructions and dhposirion of t tons. This repott Is rrpoinKI in law 09 U.S.C. 14213 Fare t report can nook in a civil ONINNY nor to xreed 51,04:* for sigh sigh violation (Section al lederld knal_Kin MI Or 195 M. I. Airettit Stake • Gulfstresin Aerospace Mudd G -IV &coal No 1085 Netionthrysnd Repstntion Dar NM IGA 2. Owner on mama astfaa FINANCIAL SERVICES CORP ID Address (As am on tearoom merwast 4444 ONE MELLON BANE CENTER ' PITIIISURGM PA 15153 • . re FAA Us Or V( ern ..... ..,.... 3 --e—r tin. Unr bake E. ' z Model i Sala No. Roar ARM Aillinne 3.z. r in Ilan I MOM) .""nnann....4) X Power*/ Pads Appian. TYP4 leadmin -.. • - . 46 Carlear ii A. Adencys ram ad Addams ' B. lad of Apia C W. e• LANCE A. RIATTEXPI X C 5. Calthairod - ass L SAN nun DRIVE Foam Cat&ad Manic . sco th at's.. AZ suss Cantina Rani St . Monufocturcr - D. I cettifytho the repel Sot nemoott may to 1b ads) identad Sao 4 toe. .4 a: Ma andsnato tonso lim Oa easy is exordia ea a mamas of Put 41010o U.S. Total Aviata the leforrace fined ems a vois a coma to IS aro amass. . - • ig- 7T PV -........ , - t to ocaerete the Pm to tat =dairy pat pima spaled tolom the Ens tarifa bar 4 am lacral Idea m presinal by Oa Ariziammos ads Federal Mince Abollstrean rod I le APPROVED CI REJECTED • ... BY rna no nem . bent I gessax r z moon Ammo I Dan Oran . FAA D*We , Ferep in . • Peen Aparmay Tampa Can oinnerdos thump 1 DSc of Amaral or ROMS . • . 8 - it -1 ef . • Dolblia' 130". to copsol• Spaof .--- . -laicbod Dandy SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 00241101 EFTA01326694

• . - ..••••••=0,C-- S. Discerns el Week AoremplIsbal Of more smog is rent& cab elation& ass. Mandy anni vane neanaley and memo. ant sad ids work complseed.) In order to provide continuity during future inspecans, maintenance, and Mashers a true copy of thri. FAA Form 337 is isduesd to be kept an board the ant at long es the effetattan remain rn effect. AUGUST 26, 1994. dulfstraan Aerospace Corporation (GACI Mole 0-IV. Sant Number 1085, NIOIGA, FAA Aircraft Type Catifi Al2EA. Aircraft iirt,irdas - 1786.6 hours 736 ender Refer to the Ze.t b L / GAC Aircraft Service One {ASO S. SUBJECT': ICE AND RAIN 1/49EltATURE LOW MESSACiE - PAW/MONS. dead Dextriba 17, 1993. Thu pnapose of this n to activate the "WING TEMP LOW" message (Amber) on the &tax (EICAS) and await ahartinse W4 ha net reached 100 degree' Fahrcmhrit of err two ".:,: from bean selected ON. Main Junction and Relay Punt Wires I/4152222 and 1H1525C2 was and spliced together. Wires 2/4151202 and 2/1152922 wee removed from together Wee 49076W vas salsa trifle IH152Y22 near Data Accpsisibm 1, 95MPIB pm 17. Rive 1{907-E 22 wr spaced to win 211I321'22 rear Data acepaintion Unit al, 95A5PIEI pia 17. VT together yeah win 1H IIDDI2 rear connseur Z9A !PIC pa 29. The MN 2H127021 near armada 29A1P1C pa 91. All of the devatiorn tint were mode to the approved design were prinide for rotting append configundiens hint been dreamt:bad tic the dentin neck did not alts the of the approved strain service dew All parts were prodded in kit form ad obtained from Galina Aerospace Predict Support. Staessfolly performed ASC 232's operatieral test • Reorded compliance with thin FAA Co@ 337 m the Irate essantermai meads aid maned to night Altus The etTect of this chaise on the wen& a basic weir sod beamed we saaphigaiie sod no dames were made to the surcrafra name weight and balm report .• sew. gene eine pnind kbanal Deal, WOW it Sam 12i MI ACIDECENALSts a MLLE* Vla, - . - - - igui.ake'S • - .42 : - cre,triLl MbNyfiM_ 02764180 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241102 EFTA01326695

.Nragitr • Agt5,O3c-stki-: •PJAU• giCa • • .•IrrnAr ican ft.. - O MAJOR REPAIR AND ALTERATION tart* Ms Ody strnmoorma (Aldine. Powerplant. Propeller, or Appliance) karat " SIIIISSIL caw ension <SC-IC:SO a INSTRUCTIONS: Print or type all entries. See FM 43 43. fah 43 Appendix B. and irstructiom and disposition of this form. Thin report is required be a (49 U S renal' not to $1,000 for each such violation (Section 901 reclitral Arial lon AC 43.94 lot subsequent revision thereon for C. 1421) Failure to report can result inst.& Act o119$8), ....tfted I. Arad Make . . Gullatreasa Aerospace - Mood . &Iv • i Sol No. f I i.: . - - Nerionelity mid Registration Meek • NIIIIGA 2. Owner N •• . ; 2%9. (WPM awakes) ?....,.. ME r • N . - ANCIAL SERVICES CORP Ni Address (Astor' on regltrIDOTI rands.) 4444 ONE MELLON BANK CENTER - PITTSBURGH, PA 13251 IA Li!, 3. Fee IAA Use OWE •.• . . id. 4. 4 . '3. Eno Mee Make I I - MOM No. • Riper Monies Airbag • . .• • ..................... kem I above) ""•• •••44'.•••5••• • I ' Parepleat 4? Panels -'' • Afars rAlle - e ne Wein. , • A. ava . C soil A lean Ned Adana , B. KIM essay - C. Cedar LANCE A. nunnot4 . L U.S. CerOficated Meekest - IMO E. SAN FILM DRIVE Foreits Catibrated Mecheltie AP iCOTTSOA&S, AZ CUSS .... Caticated Repast &Mx° •• ' D.' I ready OM the rep* gator Swami sea to Os moo) itateed is lea 4 Move al dessolool as Ike• Lain hew bee =do is ecconlosse wee Oa loam of Pen 43 of dr U.3. Feast Avalon Repletion fniskett haat Simi ad eat MS toe ofem keesderce i i~ • Owe 8-27 Tr' • - 7. Antwel lar Rents MUM= Pecom la Ms MilmaY Pva PKocia vides Wow. die me ideemilotbea 4 rt e sweat S a pemobel by the Admeriersor of do Peeing Minion Adiseserneas ode IC APPIIOVED CI REJECTED .. FAA Pril lo lawn Meoutectusu x tropecocei Aatkorabos COM (MediY) .•: BY e. FAA Cram . a Repot Meioa Puma Approved by Ira,* . Clesdeknortkixo. arose- .• f . ' Due olApprorel Or Rqsdion . • . , .0-/P: ety ,: claienencle BiOriYe of. a , is--- UMW li .. Milton Domani), e ••••••C A 401 aunt _ 1/4,1V12/4 r a . / i SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241103 EFTA01326696

ran. OncirlIV•Cilttlil "Mr Or S. Eleserlptha of Aoosatellead Of more spa is walks& wrack alatione then karata Mm acre carnally wet regent= @t ins dee wort completed.) In order to provide continuity dung future inspections mainteranCe. and atterabons a true copy of MIA FAA Form 337 m requited to be kept on board the aircraft as long as the alteration remain 07 effect. AUGUST 26, 1994. Gulfs-bozo Aerospace Corporation (GAC) Mryfrl G.W. Serial Number 1085. N88GA. FAA Aircraft Type Sheet A 12EA Allyn* in-urn= deta - 1786.6 holm 4 736 Landings • GAC Aetna Sense Chace IAJC1 255. SUBJECT. INSIROMENTSCATASI). SNAPSHOT TION, dead May 5, 1924 The putpae of a to provide the an wattles/rich that meta engine parameters in both Fait Wunmg C) tita What memory • swath ASC2.55DSI on overhead penal in the spot Watt position 1 nvitch socket wince se fakers: bid want FD9030AZ/N to groutal small U; an,2 wee Jumper 72 totall bp..! wire P090)0822 to bred SII521041022 to Dv Pn D pia wire FD9029A22 to CODDSCIDI 31/A1111 On ail W. Avkaske Shelf Asa/sales: Connected • 31/A1P7.11 Who Dim and Tee Box - VA1F2C pit 11; pa small V win FD90298 to F9/C a 1 -95A1FIA pm 81 tad riVC 12 - 95A2F1A pin SI, rospece Dim sod Tat Scot - 29A1P2C pit 64. AD added wee oomeetara to th and Toe Box were trade deo* to the rack con:to(s) instead ofthn All of the &viatica, die was made to the spermod Jess was approved ocinftgurations aid allow both pilots soca, to the deviations mode did is alter the intent or %cram of the The effect of this chapati& brash'. decd load imelya, ml be cesais. Poser it the 01- switch macaw! b from the O'HEAD LTS MR 12 an totter. - SNAPSHOT* Slaw Sop ONUS doe (when snaphot math a pressed or dorms amnia haws tea) a kas than 0.1 amps in hoe/ wid 9.05 amp 4 dia. The e ffeet of this Mange on the turaaft's basic triad rat Saes wee timalaiat Sat orb Ohara were made to the ureraft's belie weight and balance report. Tao Ammar swired Da 'mond Y. ISSN Dear. VOIDGAD - - -araftavarvit. - " SDNY_GM_02754182 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 164 EFTA01326697

-"finfar. 4"0 1/47,MLFTM t pilsesal MO ii• 'MO 0 • MAJOR REPAIR AND ALTERATION """Oi°" album...N. (Metros, Poweeplawf, Propeller, et Appilmmt) I ol l Sulam . oats iiaftaa Ps C. cit) -' IMSTaut. lama Print or type a atria. Sera FAA 43.9. ma 43 hofaCilY I. and C. 0 .04 (Co 7 revision thereof) for imtnakon and disposition of tiro fora. This report b Cro a (49 US C. 1421). Foam to mart can result Mocha Mar nbc to flied $ 1 000 for each such Vaal (Socha a I Fedora Avalon Act of Phi A. Mahe I. Aland • Cantinas AerospaCe Modd C-IV Seril No IOW lalicaity tad Regiongan Mach MEGA Name (A• than on raposica calicia) 2. Ow= FINANCIAL SERVICES CORP ID Address (As Sm on ropengeo cseakos) 4444 ONZ MELLON BANK ONTER ' PITTSBURGH. PA IS= K Fe FAA Moamar • 3. T Use MIS MOOd i TO No. Ems Aberaton Aflame ii lam I above) • X Powniot Nopio Appleton TIPP ear & Calliallif A hag, as al Adam B. Cad of Aorta C Oaks Na. LANCE A. MATTLIOPI I U.S. Colligated ISM L SAN MAIM DRIVE Fonda Catificaled ' SCOTTSDALE. AZ na Certificated Rept Swim Mamba= D. I catty Oa the ea* aka dna ads to ra sa(4) trassad in tan4 tow a chicasd atachtsas tea ay Ear aide is oxonlatat a a sk taantats of PEI 43 of the U.S. Falai Arta a Cam toad area a free ad coma to a toot of ley ardatap Dia g/i 574V Seam of - r 7. Manna he Rao an Serb Palacio a sakarysia pa= sada bast ink madled nes 4 es saidai ia r as pada by is AtIsmanta arch' Fad At Adamant:a ad a NI APPROVED 0 REJECTED BY arta aria ~ oar Maatiams i havato• Athcastaa Car (acity) FAA lawn Emir San Pm Amara by Tim - A•liall= Croup Dub MN:rani or Rooftop <9 —/s---tre (Noises toosumato SWOON IA Sessen of Aabooad .ti LadDcrttny :440;;.• SDNY_GM_027S4183 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241105 EFTA01326698

• ••••••laellWat 0-AL--tzww f - SDNY GM_02754184 L Osseripliso tifWarkAcomplishwl (r moo specs is ropiest. WI adorned raw teisaelip sin secret swot wit rssinormo mR wet de week completed) In ader to provide contmudy during Uwe inspections, maintenance. and alterations a bus copy a this FM Fare 337 is' raptured tote kept on bored the acre as en; as the alteration remain m effect. AUGUST 14, 1994. Gukstrean Aerospace Corporation (GACI Model G-N, Serial Number 1085, NSSGA, FAA Ain:raft Type Grams. Dm Sheet AMA. Attest in-ten-ice dots 1716.6 Ian & 736 Labs", Rr1aW the f• Approved Data: Gulfs:ram Aerospace Corporation Aircraft Service Change (MC) ECT: AIR CONDITIONING (4 TA 21) CABIN PRESSURE MANUAL 27ON dated JULY 22, 1994. <CKI3 CODE 972930> is to agow the cabin a prams control 10 mat to manual operation in the the Pronorialace sYllao s lot Pow*, d l l s VAC power is lost, the prance trordocu'' the outflow 1. fast Gre -295's modification irstractesas aiodified the existing 325AI Relay & Skins relay 3.25AIK10, Datoch P/N E4161383; Waded .1 relay socket 325A 'XXI°, Dana& P/N 65009-004513, nil position 325AI X1(10 a connected miens wires es folows ON - ft2, HS0BA20 83; GPOSSA20 - XI; tG52A2ON - JCL A3C 795 DEVIATIONS: binged& new tort 500O421.513 Sty socket .4—S to tad position 325A DO(IO (see Wee) and identical as ASC295)3C I instead , socket sod chops shown on Papa 4 of ASC 295's outruceons, orator wets DI01 306AI P200 Grid 326A11200 (vispectrody) pontoon P 'mead of ma/ Leecii P/N )A-W4P-005 fake GASSUSV I) Sao wicket ASC295XILL Proctoo Support Saverrsh. Safully performed the installation cluck= lined in It has been determined that the intentimonship between this Mere and my previa.* approved introduce my adverse effect upon the sinvotainess of Ur sacral Thu dconeznation includes, tea modifications or damsons made did not aka tee ouent of a y e approved acrid Sat comae, finis the operation n cal-WC; No .y..anal Illadat. an Ian. al a instslistion mynas thereon wwiame comnisous conframsy with the applicable lindens requittrena The effect of this change on the turcists electrical leading sill be 0.03 ads .dried to the circuit breaker. mental 115 VAC bus, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241106 EFTA01326699

CAPTLl AVE CIE* t I I tit'ArWli 0 MAJOR REPAIR AND ALTERATION dit...p.om, QUrfreeee, Poweeplant, Propeller, or Appliance) si... sea eassem ISseeecimi Per >Maw - fa /AA CS 0.7 Ma Swedes Oc - r'5 N: rPISTRUCT1ONS: Print a type all *Win See FAR • 3.9. FM 43 Appendix 8. and AC 43.91 (or subsequent revision Immo for 1miructions and disposition or this tom. Tile report a required by La (49 U.S C. 1421). Failure to tenon can Mule In a dull penally nor to ineetlyi)00 for each wan violation (Section 901 federal Aviation Art of 19$03 I. Ararat Mat! . GUItlatItOl Aerostat Model G-IV Said No. INS Neicasfaty ad Repose= Me& NESGA • Name (As eon on reqiernlion ainifiese) 2 On, FINANCIAL SERVICES CORP 83 Address (Moot oe spite CM/OW 4444 ONE MELLON BANK CEYTtE ' PITTSBURGH, PA ln,5$ 3. Per FAA Da OAF 1441180:alleei Sin. lat IM .1,4. Model I Sal No Ian Alan Aida in IC I non •4•4••••••••••••••• X Pollan Ropier Awing tr L ...... th Ceedweein A. las Hafaa ad Ada B. InSof Ma C Cant No. LANCE A. MATIII3ON la L. SAN PXLI72 DRIVE SCDITSDALL AZ I52 X U.S. Cancan M oda Fora Carnicated Coat:aged Recta Stilton Meaufectura D. I catty Os LS Mai laSS Ca =an COI Sant a is 4 non ad Cad sac Into a Co ton ta nora wit In intonate of Put 43 of the U.S. Feta Annia dr ietosaina rand balsa ad correa to tbr On of dry Inntolda. De sr?" , n r 7. Anent Ihir Roan 14 Sinn Panto Athreirrair BY S. aciry wee roan speccese Wort d at at an and ma 4 we spa al as clad by dit of the Foal Avan Ack•irrairs sad if TH APPROVED 0 REJECTED PA* Ft Vine ales Ineadlacera x Cocoon tontonan C84(39 442) FAADonate Rata Ca Pa Apron by Tact Coda AnOrda Group IC of Awron or Ration eln-A7 Catama a' We s Dia SWAM% IA f - - ad.." Mai Dan! SDNY_GM_02754 185 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241107 EFTA01326700

cmam knout? itionike - 7st NOTICE • • Weight and balance or operating Enutation change shall be eared in to appropriate aircraft mead An ateranon must be compete with all previous alterations to assure continued confonsity with the triable Sworthiness reqtarments. & Dratelpelir fl ak Asearlabed at mole Nee a Molted and elationst tees Ids* wan at Mosley ad mite= eark ed des wart scallt&) In order to provide continuity dunng future inspections. marrtenenoe, and alterations a true copy of Ss FAA Form 337 is' required to be kept on board the amnia as by as the alteration remain in t. AUGUST 14, 1594. Chaste= Aerospace Corporation (CAC) Model G-1V, Serial Number 1085, N8SGA, FAA Aims& Type Certificate Dsta Sheet Al2EA. Auctift meertia Si - 3736.6 hors & 736 landuigs. Rder to the f (ASC) 313 S DECEMBER 1 Approved Data: Whitman Aaospace Corporation Aircraft Service Change NEUM,477CS (ATA 36) CABIN PRESSURIZ427ONSTABIILZa71ON dated <-CMP CODE 973130> The ptirpose of on is to reduce the cabin prelate rite changes thud occur during maid power lever reductions at high This situation provides/selected came to reset bleed air pressure regulation from 18 PSIG to 30 PSI the power leen at retard below pedestal guide= angle. Ina retarded power Ice descent, without ont manifold is saintsical above 20 PSIG. This cured is tuned through the 2.500 FT Ala ban mute relay, nen this relay is sciarded. Selection of any Awn-ICE function also disables this camas. ASC 313 PLSTALLATICAN AND portion near 315AIRKSB and idattified Performed all of the wiring changes shown • new Deulach PIN 65009-001-513 relay socket ins a scant veil 13XK1 indeed of the relay, scar and basket listed in ASC 313. 6 of ASC 313's insertions, except fir the following deviriena Wan D9002B20 and D9002A30 iltre - P200 sod 326A11203 (rospectivdy) potion S Used ofd: Wee D9004A20 ad D9004820 were I F200 and 326A (reepectiwely) position R hued of nag Woes D9004820, D9061C20. ad H4D3C20 we anted into 326A1T/1 R. L. & ht (respectivdy); Ws D9007A22N was Seated Son Wound 1110& E2 Parton M Sued of El a Ala completer war and erg a insad a new Leh P/N 1-W4N-005 relay (aka GAR835NRI) into 13XK1. Al of the staled pats wee µnehued from GAC Pet Dawn Savannah, GA Suocessfuly performed the szatim checkout toted in Pesegark E p ASC 311's weruchons Note- Athed Signal Service Bolen Number 3395012-36-1646 hie been ;mks* complied Veins 54/1 and 5412 ire accesuble by remota UPPER pylon pod I on be reapers stele Recorded complasoce at. this FAA loan 137 n the masts so elmave rant end tamed the It has been daermerad that the ersernelstionstup beta= this damps and say previolaty appeared introduce any 'draw act upon the *wartime* dee Sat 7Ls debaxeration artudes, but incekfrations or ember reide did not aka the thank athe approval swath service change, fimetems the opcestion es automata; No Oar m.mdagWbmno are nescirot, and the instance prrnous allenziors estanng tie ceakanity Mt tie sppwatietimatticest rearms. - . • bar The act °Ishii chore on the saszar's SAMS lotd.. will be 1.75sssd as the sate SPEED BRAKETLAP ALA1Ud ad 0275 ki CB 20 44.014 Pa . . status. Any its intended at an S imps to CB 2C The as of els charge on the raarabatMasi✓tetalSSekgR selidre are was ode to the .Stmt's bre wage and Slam apart . Ths • • aria 'seal in needale INSI9TiS TARDY% ,.a. .imismiscrion. ocAddikvo.kkens As!. - • . etlt raintsgtiatoaarief irarstirrz --zi _nj* • 2:40vjz;,: .c.,.2 • Geo:4_027541R SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 I 08 EFTA01326701

lntar ' eV' FAA AIRCRAFT REGISTRY nien,,, CAMERA NO. / DATE: 5' - /7 - O MAJOR REPAIR AND ALTEEATION - Cracow= (Airframe, Powerplant, Propeller, or trace) re..... .......... .. ".......... own. Ila4a . ....AA visor, • OM. Mereneeriaa - - - 63° ra 4,,, 0L INSIRuODONS: Prat or type el flies. See FM .3.9. FM 43 Appease 8. sed AC 43 9-I (aassns! Mann Mt banlanns ad trnensmen a this lam 1S read is rebind by lav (MI U.S.C. t421! Fates to typal as real Ins di pasty not to eragied SLOW breath Bah seam (Seem. 901 Federal Melton Ns of MM. • I. Aircraft Mike Collette= Aertasptce Modd - C-IV Serial No. 1085 Nalionsbly and Reese:Woo Mark NMIGA 2. Ovals Name (As show a reparation an -am) ACFIUM LEASING CORP Adam (As sawn on remake certacas) FOUR EMBARCADERO CTR SAN FRANCISCO, CA 94111 3. For FAA Fry Only 4. Volt Ithogaleadoe 5. Type Ural Ma I Modd I &dal No. Repair Mat= Airframe • 4•••••••••••••••• (As dosed:4d in 11 I above) see...... X Powaplant Propeller - Appiamca 1 '. Alsobtrans • A Cakemilly Stien=8/1 • 'A Stilt and Address B. Kind of Away C Cantata No. LANCE A MATEESON • . 9560 E. SAN FELIPE DRIVE SCOMDALE, AZ MSS X U.S. Caticated Me trans .,-• AP.1164049 F044881Cartthesleil Medmmic CatSated Emma Station liamaimturer D. Inesty Math/mak wellor Mormon waft so the eat(s) identified mama above and 6nenlad m the rasa a ancesawn kneto an lam mens in acerdiace Caul nquiteemas or Pat 43 of Ma at Fare ' Itagalskaw aid tha the informs:on forawhorl baron is mu ad coma lo the beet o my lambda& Date .1-ff-ty . .&gitatal f f ri - 7. Anneal for Rearm *Arles Persosot to the antharty given peon specified below. Me onit idatiEsd in be 4 vs Spa mare Ana pass wad by the Mitnineracer of the Federal Ariake talon and is XI APPROVED C EMCEED BY FAA Ft ausbrei twat Mandato= ' x laspecOmMahceimicas . sons (Spicily) FAA Dadposa Rep* Station Pam Approve! by Tr dada Afrwarthinea Oroap Den Approval or Ftewtoon WO V --- - . eat Dmielam am 3267950% IA MbNYCM 027541g7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241109 EFTA01326702

"ra- t eflitigf rY FAA AIRCRAFT REGISTRY a y CAMERA NO. / DATE: 4 NOTICE WM& and bolus a °Paging limilabon dears ant be :raced in the sisnipsu lir alf LIMOS. An austionroust be compeale with a0 previous altastiont to assure continued conformity with the applicable airwortbineas remoraocnts. & Desoiptke of Work Aromapllabed (rm= apace b oppoired. cad: eddtionet aka Ida* with &ad rsiterty act ranmaion mart ad de wort _.plead.) March 18, 1994. Gotham-am Aerospace Corporation {GAC} Model G-IV, Saul Number 1085, NUGA, FAA Aircraft Type Catificate Data Sherd AMA.. Aircraft ea-service data = 1629.9 hours & 669 landinp. Refer to the following FAA Approved Data: Oulfstream Aerospace Corporation Aircraft Service Change {ASC} 298 SUBJECT: PNEUMATICS (ATA 36) BLEED AIR ISOLATION VALVE RELAY- POWER SOURCE MODIFICATION dated February 16, 1994. <CMP CODE 972980> • The purpose of this alters\ on is to separate the power source fete bleed air isolation valve control relay from the bleed air isolation valve relay. Presently, both relays are powered from the same 28 VDC circuit breaker. This ASC installs an 'AC' control relay for the valve control relay which will eliminate the possibility of a single fault causing a false cockpit indication. Performed all of ASC-298's modification instructions effective for aircraft Say: 1085. Installed parts are listed in ASC 225 page 8 and were furnished in kit form by GAC product support Savannah, GA- Successfully performed GAC CMP code 361064 Bleed Air Isolation Shut Off Valve operational tests. Using the FAA Approved G-IV Aircraft Flight Manual operated the Auxiliary Power Unit and started both main engines and verified that the APU AIR. LOAD, ENGINE START or CRANK, and the ISOLATION. VALVE cockpit switches performed their intended &actions. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. The effect of this change on the aircraft's electrical loading is negligible and no changes were made to the aircraft's electrical load analySis report The effect of this change on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report as a caupgar anered Am nand W waded DNS* WOW It - mliS%roll AM. NO AOCIELMAL =EU ARS ATIACHIZI *DM' O Atationd Sheet Are Attached SDNY_GM_02754188 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241110 EFTA01326703

ITMlEartj .,. `‘N FAA AIRCRAFT REGISTRY CAMERA NO. /A/ DATE : 7. 7y @ MAJOR REPAIR AND ALTERATION 011 Nall esommomi (Airframe, Powerplant, Propeller, or Appliance) rain Jae - rain tat spas PO to alga larAA On CI* MN Idadfuriee SOL "Frf 04 7 nismucTIONS: Pont or type all entries. See FM 43.9. FAR 43 Appendix II and AC 43.9-1 (or subsequent revision Menial for instructions and dii position of this form. This report is required by law (49 US C. 1421). Failure t report on result In a civil not to exceed 51.000 for each such violation (Season 901 Federal Aviation Act of 19SM. _penalty I. Mace{ -/ Maki Gurnee-earn Aerospace Model t G-IV . __ _ Said No. 1085 Natiornfity and Registration Mark N88GA 2. Owner Name (As shown on registration itertillette) • ACEIUNI LEASING CORP Adam (As Omni on rewaration cannons) FOUR EMBARCADERO CTR SAN FRANCISCO, CA %III 3. For FAA Dee Only 4. Unit liken/Ronan S. Taft unit . Make i Model I Saial No. Repair ( Murton Airframe (As described in Item I above) X Powerplent Propelkr Appliance 1Wo .... Mcderesar 4 6. Carkirozety Steteroad A. Mean Nome and Masai B. Kind of Agony. C. Certaczne No. LANCE A. MATTESON IMO E. SAN FELIPE DRIVE SCOTTSDALE, AZ 35253 X U.S. Catiksted Mechanic AP Ilan Foreign Catilicated Mechanic Catifacated Repair Station Manufacturer D. leanly that the repo mace ammo =de to due mai) Identified in bane above sod described o the reverse armaments hereto have been made in accord= with the To:Orem/nu of Pone) of the U.S FLOM Mama Regithikas aid tha the inkemetion famished bate is ow sad Ceelitt lo the ben of my knowledge. Dale . . . 15/ signor s2: _.......4 i• 7. Approval for Ran to Pnn to the orthodry given groom spooned below. the toth'clemithed in Om 4 era inspected ia the re= pracrOxd by the Achennirwar of du Federal Mission Attraninion sada CII APPROVED 0 REJECTED BY FAA FILM..Mt Sinew Mamtfacturer x basevaion Azahodation Other (ePedY) FAA Designee - Repair Station Pews Approved by Tampon Cola Mit Group Cote of Approve/ or Rejection -4 -1 Ct' -- , y Ovens o or Signals{ of Mahatma Yydividtrajf nisstise. . - 52670504 IA P r a<a Michael Donnelly 47-Ca5V4ilinrmt44 44emt :4 "1" Biarrinerre gi lW4 9WY,4.79"'"'"" - ).. SDNY_CM:027541EIS SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFIA_00241111 EFTA01326704

"2"."-": TE'443E-A"r FAA AIRCRAFT REGISTRY • CAMERA NO. A DATE: V: Z 5.4 79 NOTICE Weight and balance or operating limitation changes null be attend in the appropriate aircraft teoxd An alteration must be compatible with all previous alterations to assure continued conftxmity with the embattle airwoethiness poluiremalb. a. DesaiptIon of Work Accomplished (If mom space is reqvized meat adtmenal abeam Wan* with eiremft atmaayaadrapsomlon mark and drat wort completed) February 42, 1994 Gulfstrearn Aerospace Corporation (GAC) Model G-1V, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet AI2EA. Aircraft in-service data • 1611.7 hours & 6611andings. I- -- Rettig° the following FAA Approved Data: Aircraft Service Change {ASC} 225 SUBJECT: LIGHTS mu 33) NOSE GEAR TAXI LIGHTS MODIFICATION dated November 1, 1993. CMP CODE 972250> The purpose of this alteration is to modify the nose gear taxi light mounting bmck,etry to provide optimum visibility. It also changes-the center taxi light from a spot light to a flood light which will eliminate shadows. This service change also replaces an existing circuit breaker and taxi light housing assemblies. Performed all of ASC-225's modification instructions effective for aircraft SiN -1085. Installed parts are listed in ASC 225 page 4 and were furnished in kit form by GAC product.support Savannah GA. Performed Al of die steps listed hi paragraph "C. Perform nose landing gear retraction to ensure clearance of taxi lights" and noted an interference problem between the GAC P/N 1159EL20064 Wire Bundle Support Bracket, refer to Page 6 Figure 2 View A-A and the Nose 1. ceding Gear fruition assembly. Corrected problem by trimming the leading edge of the bracket to provide properclearance and noted no other abnormal or unusual conditions. Successfully; performed all of the steps listed in paragraph "D. Perform operational test as follows:" and noted no abnormal or unusual results. In addition, checked taxi light operation individually and collectively to verify proper circuit breaker configuration; and Checked the operation of the Nose Wheel Stearog System with taxi lights ON and OFF and noted no abnormal or unusual results. Recorded compliance with this FAA fora 337 in the aircraft's marntenance records and returned the aircraft to night status. The effect of this change on the aircraft's electrical loading is -150 VA (watts) added to the Right Main AC BUS during tan light operation. Note: Taxi light operation is inhibited if the landing gear is not down and rocked; See ASC 131 <CMP cede 971310> TAXI LT POSMVE CONTROL for details. The effect of this change on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. This u “ 0900 gonad In cosmos er blictrel Dawn". wow) re 01/12/94 AM NO ADDITICNAI MEM% AU AlTACHID •@C. O Adcbtanal Shona Are Attached -et, r ----taeArremila;visatiarlerlpreltroSta 4.•- •”:—n-el:t • ?••‘•• SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SDNY_GM 15,_0 an 2754190d 17 EFTA_00241 112 EFTA01326705

FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3.3'_ 94 . . 44.. , a MAJOR REPAIR AND ALTERATION US Down arraspras s (Airframe, Powerplant, Propeller, or Appliance) IMMO Minn ...A... ..••••••• ars liii imam Per FAA 136.047 Mee Idesidoeics 5 6t -Fl; e INSTRUCTIONS: Instructions and penalty not to Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent tuition thereof) for disposition of this form. This report is readied by LtIV (49 USG 14211. Failure to report an result In a civil aceecl S1.000 for each such violation ISection 901 Federal Aviation ACt of 19581. . . I. Aircraft Make . Gulfstrearn Aerospace Modd G-IV Serial No. 1095 , Nationality end Registration Mark N8SGA 2. Owner Name (As shown on resimsion cattate) BA Leasing & Capital Corp. Address (As 'bon on on cache) Two Embareadero Center San Fraoelsco, Ca 94111 3. For FAA Use Only 4. Unit laden/Ranee S. Two Unit Mike I Model I Serial No. Repair Abrasion Ai sine (As desinbed in Ilan F above) X Powerplant Propeller • AppiAnce TYPe. Manufacturer 6. Cordonsity Statemeat 2,6trays Nano end &Mpg. B Kind of Agency I C. Candle= No. - LANCE A. MATTESON SSW E. SAN PXLIPE DPJFE SCoTTSDALEAZ 957.59 X I U.S. Certificated Mechanic I Fo ten Catificated Mechanic • AP 1964049 I Certificated Repair Stition I ./donut:wrote: • D. I Cc* that the repair ounce akeration made to the ak(e) Mantled in done above mid demntied on the name or smechmada hut° have been made in accordance ..t the requiratoma of Pun 43 of the U.S. Federal Aviation Revelations and that the infcmtation ft:mashed herein is trot and coma to the beat a my knowledge Date 5 7, /94- , Signaltne e° dged hl&i2 `s.3 C .. / 7. ApproerJ for Return to Service Pornau to the anthoray peen persons Adminssiraa of ihe Federal Aviation spoofed below. the tmi Waged la kern 4 was maponed in the =OM poncaled by the Administration and is On APPROVED 0 REJECTED BY FAA Flt. Seaderds I learn manutu er rw x ineptennn Andwason Ma (Specify) FAADesignee Repair Sudan Poison Approved by Tampon Coale Atribeti1 Oro Date of Approval of Rejection 5,5-7 4-- 7./9 193 rostrums re Dettgataa. No. • S2670S494 IA l . :, . of A ' 'air Illiire- -- - ../ ' ...--P Michmi Doll:WHY -riAliewarliaek4.1169(Gtogniper-aas • SDNY_GM_02754191. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_002411 l3 EFTA01326706

FAA AIRCRAFT REGISTRY CAMERA NO. 3 tun: 3- 3- 94- NOTICE Weight and balance or operating limitabon changes shall be entered in the appropriate aircraft motel. An attention rough< compatible with z0 previous alterations to assize continued conics:miry with du applicable einenntencas requirements. S. Desorption of Work Accompllsbed (If more space a recpung oh additional theets. Way* with trawl nitionalny and regstrzion mart and data work completed.) September 7, 1993, Gulfstream Aerospace Corporation {GAC} Model G-IV S/N 1085, N88GA, FAA Type Certificate Data Sheet AI2EA, Revision 18. Airmail total time in service 1493.6 hourt and 608 landings. Refer to: FAA Approved GAC Aircraft Service Change (ASC) No. 176 Subject: LANDING GEAR (ATA 32) NOSE WHEEL STEERING FAILURE - ANNUNCIATION dated February 23, 1993. Effective for Aircraft serial numbers 1000-1214. The purpose of this alteration is to add a pressure switch and circuitry to alert the crew of a problem in the nose wheel steering system prior to takeoff and/or landing. The pressure switch and additional circuitry allow additional parameters to be monitored. The amber STEER BY WIRE FAIL message will be displayed on the Engine Instrument Crew Alerting System when one of the following conditions exist: (a) Nose wheel nutcracker switch snack in the ground mode; (b) Nose wheel steering shutoff valve(s) stuck in the open position; (c) Nose wheel steering system inoperative due to loss of power, (d) Improperly installed steer-by-wire ECU or ECU connectors. Using the instructions and parts provided with the GAC ASC 176 Kit, performed all of the instructions applicable for aircraft S/N 1085, except (see Figure 5, Page 13) installed a GAC P/N 1159SB20223-11 BRACKET in place of the GAC P/N 1159F41094-39 BRACKET furnished with the kit This minor deviation allows the Relay Bracket to be removed for maintenance without having to drill attaching rivets. SDNY GeS4_02/5410 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 Successfully performed ASC 176 installation checkout (Paragraph H. Pages 6 and 7) and noted no abnormal or unusual conditions. Returned the aircraft to flight status and recorded compliance with this FAA Form 337.in the aircraft's ' maintenance records. F It has been determined that the interrelationship between this change and any previously approved • • configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to: There are no changes to the operational limitations; The existing aircraft flight manual provides Migration for dealing with the STEER BY WIRE FAIL EICAS message; and the change is compatible with all previous configurations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the aircraft's electrical load analysis and weight and balance data is negligible. This Saco:vow generator form Bled ea ASCIT6DOC: SPS4 Chambers. prepared by Michael Donnelly NO ADDITIONAL SHEETS ARE ATTACHED. *END' O Additional Shxts Are Amen:6 EFTA_00241114 EFTA01326707

FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3.S @ hi.i. poem.. 1 ./L2POR REPAIR AND ALTERATION (Ak'ri amp, Powmplant, Propeller, or Appliance) ,,PET me... c•c", " ,,a ,s Fa FAA Thie Only c 0 L- r 5 .9 - ' • swarms ,samosa INSTRUCTIONS: cam or type all entries. See FAR 43.9. FAR 41 Amanda S. and AC 441 (or tutdehoeitt revision thereof) for Instructions end disposition of this Form. This report b required by law (49 US C. 1421). 'Mims to report can result in a civd penalty not to exceed $1,000 for each such violation (Sefton 901 Federal Aviation Ad 0(1954 I. Mardi Make ' Golfstream Aerospace Mold G-IV Sala! No. . 1085 Nationality and FtsaMennice Mark Nitl3GA 2. Owner Name (As stows co registration certificate) B A Leasing & Capital Corp. Addnsta (M shown cm regionalism eatiforate) Two Enobarcielero Center San Francais Ca 94111 ....- isaatJaier SA042151wanly: :seta . 4....s Riverihman infrewarts id b amrovrO ea :le oe Ova dmerbrd =Fa ailmt to cooterrny irspetho a z 'Erma a Nefas e -91114--v v -..).0 -43 _.:t- OAR 4. Usk Identification 5. Type Ufa . Milks I Model 1 Said No. Repair Altendico ?Whom (As daubed in Item I above) ********** ••••46499 X 1 Powerplent proi can. t AiVisTice t Two . . • simorasamw 6. Cesiminity Slonement • 21...pparta NO and Address B. IOW of Astaicv C. Catlin No. LANCE A. MATTESON . . 65600 E. SAN FELIPE DRIVE SC01173DALE, AZ MO • ' . X U.S. Certifiated Metairie AP 1664049 .r Fortino Certificated Methane Certificated Repair Station , Mat= DAD:eery that the repaa Nadler iiieralice made I o On mit) idedirs1 in von 4 above mai casented on the mom er madam_- hems bavc been male ist atientarce with the tespinemet of Part 43 of tte U.S. Foleral Aviation Regoltioni ad the de informant° fiatiated bran is owed coma do the born dray 171O.thit- 7 Date tt -ft —cr.) Signature 0M/thorned ‘ec je:S......... • 7. Approval for Return to Service Pirate oars Fatal BY to lb: =hairy given panes sprified bdow, de mil identified in item 4 ern laspected is dm 'rarer preeenled by de Athninistrztor Avidice Admin.:rice as OD APPROVE) 0 REJECTED FAA Ft 3adertis Impar \ AID x Insmenos Authorization Odicr(SMOM FAA Daiiiime - 1 Repair Stance Pastei Appened by Trasport Canada Ainarthiness Gram Date of Approval or Rajemion . -il.ilry . adtholin DmipsamiRis 5267054,14 IA Emanate of Audio Nfichaei Dcrrneth. • . . . • • ..___ - - . SONY CM 62754193 _ SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241115 EFTA01326708

FAA AIRCRAFT REGISTRY . CAMERA NO. 3 DATE: 3_3 -_94 NOTICE Weight and tehmce or operating hesitation changes Ad be emend in the appropriate aircraft record M thermion mist be compatible with N previous Antrim to assure continued conformity with the appraarek airworthiness requirements. Daalpriom of Week Accomplished 123/1 space l? required, meth *Mean stmts. Irks* swath sinzica snorer* ad reguntime mat Nal tie win aopleigri) August 11, 1993, Gulfstream Aerospace Corporation (CAC} Model G-IV, SIN 1085, HUG& FAA Type Certificate Data Sheet Al2F_A This change requires FAA Field Approval The ptapose of this change is to update this aircraft's fuel booretptpitp vent hose system to the current production standard. This modification-will eliminate the need for4W-erdiffenitit'pert number hoses in spare stock and provide for a neater sadiste logical initaffati6C; Modified the LEFT and RIGHT Main ea AfftglittflentEntister-fsnapVint System by. Removing and discarding the existing four each vent hoses that connect each fuel booster pump to a wing tank; Removing and discarding the number 6 AN Fitting and Os ring packing Stalled in each of the four booster pump vent ports; Installing a new MS295I 2-06 Ce ring packing on four each new AN8I5-61) Union Finings and installing one fitting ('O' ring packing side toward the booster. pump vent port) into each of the four booster pump vent ports; and Installing a new Gulfstrum Aerospace Pan Number 115H40200- 143 Vent Hose between each new booster pump vent port and the closest existing wing tank port Secured all newly installed ports and hose fittings by torquing to the current maintenance manual torque value and identified with torque stripe. All parts were new when Stalled and purchased from GAC Product Support Savannah, GA 31402. Performed a leak chock visual inspection of all four fuel booster pumps and attaching hoses while doing FUEL CONTROL SYSTEM FUNCTION TEST in accordance with CMP maintenance code 280005 (card 28-01) and noted no leakage or abnormal operation. Returned the aircraft to flight status and recorded compliance with this FAA Form 337 inthWilloriffs - maintenance records. It has been determined that the interrelationship between thischange and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, bin is not limited to: When performing it's intended functions the operation is automatic; There are no changes to the operational limitations; No flight manual suPPlements arc required; end the thosnation is compatible with current production standards and 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. This areptaer mentor torte filed a VeiniOSEdot; 5, 99 CbgeWas. PrcPand by. Kahn Deo* NO ADDITIONAL SHEETS ARE ATTACHED. 'END' Q Addend Shea. Are Anached sbAiTeii:briD41§V SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 I 16 EFTA01326709

FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3_ - 94 A il) MAJOR REPAIR AND ALTERATION v i dun= a -as.pat (Airframe, Powerplant, Propeller, or Applies's(*) / slal MISR mean. lai Mem' . 01014 727)40/ hellall•Coly Officeidadliesemos t5-BC -a? INSTRUCI1ONS: Instructions and penalty not to Print or type all ewes. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent revision thereof) for disposition of this form. nib repon is requited by law 149 USG 14214 Failure to repon can mutt in a civil xceed $1.000 for each such violation (Section 901 Federal Aviation An of 19501. . I. Arad Mahe - Gtillatream Aerospace . Model G-1V ' Serial No. 1085 Nationality and Registration Madc N8SGA 2. Owner .' • Name (As shown on mist:raw anificets) B A Leasing & Capital Corp. Address (As shown on rerasmitoo catifonte) Two Embarcadero Cram. San Francisco. Ca 94111 • 3. For FAA Uwe Cady • • 4. Unit Identification . 5. Type Unit Mein I Model i Setae No. Repair Merton Airframe .... (As des gibed in Item 1 above) ' - X Powell:plant • . . PropeRer a Appliance T* Manure:nun A. Ceitereelly Statement A. Agenryel Nana and Address R. Mod of Agway . C. Cara:eta No. • LANCE A. MATTESON 8560 F- SAN FELIPE DRIVE SCOTTSDALE, AZ 85258 , X , U.S. Catificated Mt:claret AP 1864449 . Foreign Certificated Mechanic Catificatcd Repair Stance ' Manufacturer IN I am* dot dm weir nadior Manisa made to the mike) idereffied in item 4 Move aed deathbed on the reverse or aratenems hens here been made In axcedeom with ra :mei:amens of Pat 43 of the U.S. Federal Avalon Ragelations and that the information feeedded herein is tree nreleoraia to damat eiT my ImoMedea Pale „9 ,7 7 :irri • 7. Approval for Retro te Service Pumcmi to tbe milbeety given pions specified below. the and illersined in Mesa was inspected ha We maw prsaMed by the Adrnisescrace Maw Federal Anxion Admousalcion ands IK1 APPROVED 0 REJECTED BY PMdik Sewiatea Spence Mane/masa i I baPeciwn Arthwawann Other (Speedy) FAA Designee' Repair Mama I PetiOn Approved by Tampon I Canada Airwatbinin Group Date of Approval or Rejection 547 f 72. Certifiers ar• - Owieries No. 526705494 IA Signs of A ideal Michael DonneRy SDNY_CM:02754195 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241117 EFTA01326710

FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: 3_ 3- 94 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alb:radon must be compatibk with all previous alterations to assure continued conformity willa the applicable airworthiness requirentogs. • S. Daseripdon a Work Accomplished (Snore space is reqviroi mach additional sheen. Identify with aircraft natio:lay and reginnuon sit and else work completed) September 7, 1993, Gulfstream Aerospace Corporation (GAC) Model G-IV, SIN 1085, N88GA, FAA Type Certificate Data Sheet Al2EA, Revision 18. Aircraft total time in service 1493.6 hours and 608 landings. Refer to: FAA Approved GAC c-ry Aircraft Service Change {ASC} No. 3 Amendment 2 Subject ICE AND RAIN PROTECTION (ATA 30) WINDSHIELD HEAT - • TEMPERATURE SENSOR TEST SWITCH - INSTALLATION dated February 26, 1993. Effective for Aircraft serial numbers 1000.1155 having ASC 3. . ) The purpose of this alteration is to modify the wiring to the windskiiikheat to perature sensor test circuits installed by GAC ASC 3 so that both temperature nsors o each cockpit window can be tested. Using the instructions and parts provided with the GAC ASC 3 Amendment 2 Kit, performed all of the instructions applicable for aircraft SIN 1085. Successfully performed ASC 3 Amendment 2 operation test (Paragraph C. Page 3) and noted no abnormal or unusual conditions. Returned the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's maintenance records. It has been determined that the interrelationship between this change end any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to?There are no changes to the operational limitations; No changes to the aircraft flight man\qal are required; and the change is compatible with all previous configurations assuring continuous conformity with the applicable airworthiness requirements. • The effect of this change on the aircraft's electrical load analysis and weight and balance data is negligible.. This Sacco:pan generator them Ned as AScsAvn rm a n aen. prep .4 by bads Da,„,b,ur NO ADDITIONAL SHEETS ARE ATIISCHED. 'END* CI Addidonal Sheets Are Attached • . • . SDNY_GM_027Sti SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241118 EFTA01326711

Pa Asa.. .... an Ma. 7.17PMX , @ • MAJOR REPAIR AND ALTUtATION - Toe IAA the Only us this ' (Airframe, PowerpIat, Pittprlier, mr APPIalla) er.......,.. Polinl Aar ...-- as= •kmarathe .5-.? c • ,-<sz 2 INSTRUCTIONS: Print or type all entries. Se* FAR 43.9. fAil 43 Appendix B. ad AC 43.9-I (or subsequent mislon thereof) for Instruction; an on of this form. This report Is required by lea (49 US C 1421). Fealty* to report can result in a civil penalty not to exceed S 1,0001= tad such ylolathM (Section %I Federal Aviation Add 1958). I. Airalf) Mac ' Golfstream Aerospace Medd G-IV Stria No. loss Nationality 0 Registrstioo Mule N88GA 2. O Name (Al dries on regime:ion oaths) B A Leasing & Capital Corp. Address (As on on repontice catficee) Two Reabanadero Cm1Cr Saa Francisco, CS 94111 3. For FAA Ese Orly 4. Unit Ida -dilation 5. Type' licit Mat I Model I Said No. Repair Al= Airframe (As detertlxd in Item 1 above) X Powaplent Propeller Appliance Type Manidatarer 6. Casformity Statemart - A. µstye Nese al Addis B. Kat of Agoicy C Catificate No. LANCE A. MATITSON 1560 E. SAN FELIFE DRIVE SCOTTSDALE AZ 65256 X I U S. Cerakaed Mectamic AP 1644049 j Fen* Certificated Medmic TCatificated Remit Station I Maaufacturer D. lertly diathermia mint elms= nude/oft tee=(.) identified in des 4 above cd 6=nbed cede creme a etuchaeces ham his tem made in accerderice 0 the rotaramits of Pm 11 0(5 y.s. R&M Attie Reptant dim the iefernotis fimieled tent S int aid arta to de tea dory towledet Dam Y---N-F Sigmlur loift2a i 7. Approval for Retro to Service Passed to the asloity given pima tprified blow. the me ideaihed in eat I me capeeted in the name preceded by de Athatiso car of dm Fetal Anton Ackrionaba ma is Cgl APPROVED 0 REJECTED BY FAA Ft Sumba bass Mtalfaconer i baps= Axidatatesi Other (Brady) FAA Designee Repos Stabs Pence Append by Titspert Canada Mn . dtea Cisco Date of Approve/ or Ridection 81/4 2193 Gots or Deilotre No 526705494 IA Signature of Authorized r ?ached Dannelly •.“ r=7;' . V .tr. • • zr . ”5 in hi: 't lt . na • SDNY_GM_02754197 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241119 EFTA01326712

NOTICE Weight and balsam or operating liaimtioa changes shall be emend in the awroprime aitcrillrecord. An sheralion meat be compatible with all previous alterations to assure continued conformity with the applicable Unworthiness requireameas /I Description of Work Accomplished Of mere spar is required. math odd:kcal deem. loss* each antral ruescoltry ad rcgaraa mak ad due work ccepleteM) August II, 1993, Gulfstream Aerospace Corporation (GAC) Model G-1V, SIN 1085, MAGA, FM Type Certificate Data Sheet A 12EA, Revision 18. Aircraft total time in service 1481.6 hours and 600 landings. • - Refer to: FAA DER Approved GAC Repair Drawing Number SE05201903 REV. A, STANDARD REPAIR - SPHERICAL BEARING, N.LG., FS 119., BL 0.0 Sheets 1 and 2 of 2, dated 5.5-92, Effective for this aircraft and signed by John G. Wilder, FAA Structures DER SO-483. The purpose of this repair is to prevent torsional movement of the Nose Landing Gear Brace Assembly (GAC P/N 1159L40801-5) and the Nose Landing GearDrag Brace Assembly (GAC P/N 1159LM40588- I I) that causes the loosening of the existing bearing (P/N GB146-10) in the Drag Brace Fitting at fuselage station 119.0. Removed the Nose landing Gear Assembly from the aircraft. Performed removal of existing bearing PIN GB14G-10. Inspected and reworked existing Drag Brace Fitting, PIN 159B10053 per GAC Drawing Number SE05201903-901, Standard Installation. Installed new K210-3 Bearing Assembly and torqued to 110 in. lbs. Installed Nose Landing Gear, Drag Brace and Dovmlock Assemblies per GAC Gulfstream IV Maintenance Manual, Chapter 32-2-0, page 204; pant 3. Successfully performed landing Gear Normal Function Test in accordance with GAC Gulfstream IV Maintenance Manual, Chapter 32-0, page 201, pan 2 and Nose Wheel Steering Function Check in • accordance with GAC Gulfstream IV Maintenance Manual. Chapter 32.500. page 201;para I. Returned the aircraft to flight status and recorded oaeopliaer.t with this FAA Form 337 in the aircraft's maintenance records. It has been determined that the interrelationship between this ;emir and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft This determination includes, but is not limited to: There arc no changes to the operational limitations; No flight manual supplements are required; and the repair is compatible with all preyious configurations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the aircraft's night and balance data is negligible. This nacos:pester manta form filed as N0SEGEARD0C: 5769 Ono= prepasd by 16:;tral DbeooJy NO ADD MONAL SHEETS ARE ATTACHED.. !END*. ^ SDNV_GM_02754198 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241120 EFTA01326713

*ra ~Vink" Lts-nrts rkower•--..00m us *wan miNTOrwarninT~ . TRA Alanten RECISTRT CAMERA AD. DATE: 6- -(13 e ALTERATION Pon, Rporoml OMB fia 2120~ • MAJOR REPAIR AND ufatarnon Por PAA Ure Ody cd anmemarn (Alrframe, Powerplant, Propeller, or Appliarice) name een Menseno War tinCe 4 41 (5 e - se orstaucnOtis,Prim or tYPII Ill•eltihs. Sa FAFT43.9. PAR43~mM e. and AC Ci-I falitaguenlreamonowometer Manntions and doonallon d tha We:Mommen b ~Ome in law On USCAKM h Panda nalfannat Man in ltdd MOUW mtalwand KOM Mor mok mach vadatim (34rnhon Int Naleal ~Me Ad d len). 1. arend Mike GULFSTREAM AEROSPACE wam G-IV ~d Na 1085 Nimonarny anlirgr uee repya ' Z Crnmer Name fernsMwn On ~4~ 01/PEVaD BA LEASING 8 CAPITAL CORP. Aanleg Ms Oom On rontratko ~Ko" TVO EMBARCADERO CENTER SAN FRANCISCO, CA 94111 3. Per PAA Uwe Satd4. ,...........27„, ayi aaya aa 4.,,,,aa Sv' "ffs ITTIKORI3 M a aan eg n Mr •::.•• descrod Ihn Sa ~Irae race~ br • or•rt la NOrilán Ka. Y- -F25 InTE a. om Itle.ntilletbod S. Type UNI Mere owm &NO No. kawa Mbmmm ~RAKE e a Wo n 1 nor') mornemm....mo ram, X POWERPLANT PROPELLER MOUANCE Type Manuladuret ...., 4 C. COrdendel naland A. Agencyk Name and Jans e. Kind of Agency C Canna* No. LANCE A. MATTESON 8560 EAST SAN FELIPE DRIVE SCOTTSDALE. Al 85258 x u9 Caturcatee Naam AP 1864049 Nmon Catereed nweema ~zo Roomt Sims• wo.s.a, 0 . 10e~~ 140,04"TO/0~~1"de WIKT un ROmomwed in Omm 4 More and drocroDed en me oreme of anmNmem homo fan Man node we Itecorhhhhe milt th* thChlitentleaS of Pan C dl die V.S. F innam %quines,* and t the Informat•on , lum~il neem re na and Ca nal to Me ben Of my nowledge. -...."" OM. APRIL 20. 1993 Dr' loomOmi • L ---,—, 4... c c..... . x.mprows Re Rdne Te imisib. rammelt to tam imum e Ily Olm pemems speolied ~AAM unit Woed« In dam a Ht immarn,n me nameet Prnsfand By K» Adaruniftwor of Ina Pedro Athibon ANnimstration and is »PPROVED Cl REJECTED FAA PrilMimes.% inspeaor Urnunclumr I MIrnarSma•al BV PA* ~gnoe . Now Stalen PemoNmenONTantadat Canada ammarnas Group Da* 0 kommen *a Repelen • WASA3 ~ma m DwrOMOOn Na 6 2 0 0 rttri7fr Signalur. of Autroved lno r - 191C.744 1 1)Pentredir SOI•iY dá4j27 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,0 an g41ór d 17 - EFTA_00241121 EFTA01326714

• • '`r.-77,7,74.1litanOW7Cr#14,,lit Illes„ TAR AIRCItATT REGISTRY ... ...a. I CAMERA NO. S I DATE: VP --- -- -sit 9- NOTICE Waters: and balance or operating Imitation [banessnail be enteral in the appropriate aircraft record. Anther:monmust be compatible with all previous altelations to assure continued conformity with the applicable airworthiness requirements. a. Oesenaten of weft acteepane III more spec, me required mach additional mesa. identity min aircraft nano/urn and registration mart and data work completed.) 0420193 Guff strewn Aerospace Corporation {CAC) Model G-IV. Stria/ Nunn es 1085. NDIGA, FAA Anaaft Type Cando:ate Data Shea AI2EA, Revidor IS. FAA Append Data: FAA Form 8I10-3 Statement of Compllaret with the Federal Aviation lb:gala:ions dated 2/3/92 for Gulfs= Model GV. 1159. d 1159A; listing GACRtpair Dwg 11595BM 189 REV. C title CORROSION REPAIRTBALLAST COME. SURF. ELEVATOR sniped by Struction DER John G. Wilt ex, Designation Number SO 683. FAA Acceptable Data: GAC Productioe Dwg 11590520002 REV. E, duets I and 2, inhading through Engineering Orda (EO) RI; dated 1113/92. these drawinp append forprod•wwiew by FM form 8110-3 dated 1118/92 for Gulfureatn Cr4V Anna by FranIt Salmon! SG-7034 Strunna DER GAC C-IV Meicaterme Masai (MM) -Interim Revision 16-1, dated 30 Mardi 1992; OACCeIVMINIYel, I. REVISION 16 dated 6 DECEMBEt 1991; GAC Pe:chain Dwg. 159CS20434, titled SIGN INS7L CODRROt..47YRE-FIEV-STA 1100 a 168.78 LE. MI& 2 rf 2, REV 0 dated 1240-91; and GAC Production Doug- 1159CS20443, titled BALEPTSVS7/. CONTROL SURFACE - ELEYAMR, Ail& 2 of 2 REV F dated 10/28/84. ThentrpeseefilepeieirtetreolaceeitiaMinedinboard nifing edge assembly on the left devisor.. This repair involves: A. The removal the left deviator from the istertee, B. The removal of • inboard trailing edge riveted assembly; C The installation of a new inboard outing edge riveted assembly; D. The removal of a Medan of tbt leading edge riveted skin to pin soon to the balm trim weight attach pond E. Assembly. painting balancing end attachment of the elevator control surface to the aircraft. In accordance with the GAC Conatterized Munn= Program ICBM code 2736.07 anvil the left deviator, GAC P/N 1159CS20022-59, S/N IOW dated I 1 /88. from the anent Flemmed the toned riming edge assembly, GAC EN I 159051120400, S114 1113. date/ Aug 23, 1988. from the left elevator by dribs( ow the attaching rivets Installed a new inboard trailing edge assembly. GAC PIN I59CSM20400-89/F-2/01, SRN 1400, dun holt 1993, onto the demo( by riveting in acht MAPCO with the applicable instructions contained on GAC drawing 11590520002. Rimmed leafing age skin a the balance at wight enact points by drilling ram n rivets to gain meets to the balance trim weight and: pone sad added I each GAC PIN I IS9CS20443.5I (0.5 pound) weighs and -53 doubler in accordance with data cormiood on GAC Dwg. I I 59CS20443. REV F. snouts:id 2, dated 10/11/68. BALLAST ITVEIGH7717,571. CONTROL IRFACE-ELEVAIDR. In accordance with the above referred to GAC Product:cmDee& detailing SKIN NM mstalkd original elevator leading edge to by Mang. Trated, sealed, primed sal painted tetrarch all bare meal. In accordance with the GAC NMI ATA 27-0 Flight Cootrol Systems decked balanced elevator; final balance data after paintin LH elevator 0.0 in.Abt NOSE HEAVY. In accotsbnee with GAC CMP codes 273007 installed be maned left elevator. GAC PIN 1I 59C520002-59, SRN 1086, dated I1/88, to the proper position on the aircraft The mad was not tat flown because it vets disenimd that the tate dal was dote would not change the flight cliamatristies or 0mo/tonally aft xt the Bight operation of the ant This determination inchaded, bin was not lintel to, anderation that the repaired elevator tamale balance, shape. mega and original type =fame design was cot changed. Recorded compliant with this FAA form 337 in de sinnit's maintenaam records and =mod the aircraft to flight tame. Aarall Total Tent: 1362.6 heat Aarah Cycles 547 landings. Changes to the artralTs weight and balance was negSgible Ttm morear ecorraird 6:0 prepond by Mathool Pau idly teen a Pc M at/50. Midas CLUAY112073ELD3C.,1555 Calm • ADVTIONAL SHEETS ARE AITACHErt na.ar Addazontit ShWrIt Ai. AitaErtycl r . • • kiwistit.- • f. agt., :1 & Fit . 41/4, a • 1 • • •'-•!..217 15 ' • : SDNY GM 02754200 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241122 EFTA01326715

FAA AIRCRAFT AIRCRAFT REGISTRY , CAMERA IRO. DATE: 40 a tr" ' Sgi Nisi 0.1*.119402. @ MAJOR REPAIR AND ALTERATION Far/AA US. Oa, uac....cus (Airframe, Powtrplant, Propther, or Appliance) erspoils Aillall OtEse Idemdcown Z) 1 ttr i/. 2) INSTRUCTIONS: Print or type all entries. See FAA 419, FAR 43 Appendix R. and instructions wvi disposition of this forrn. This moon is required by law (49 US.0 Peray to to acted 11.000 for each such viotulon (SecOon 901 Rola AC 43.9-1 (or subsequent reviCon ifsenc4) for 1411). Failure to ninon can result m • civil Act of 195/1 I. Aircrati Make ' Galfstream Aerospace Model G-IV • Serial No. • TOES Noionably ad Registration Mark MICA - 2. Owner Name (As shown co toptinunn ciro.5mtc) B A Leasing & Capital Corp. Address (As doom cm *strata outdate) Two Embaraidao Caner San Francisco. Ca 94111 3. For FAA Use Only 4. Unit Identification S. Type US Make I Model I Saul No. Reps Altermam Airframe (As desaThed in Item I above) • I PowapLarit - Propekr Appbsecc ' Type Madam= C Conformity Statemaa A Agemis Name al Address B Kird or Agiscv C. Cates. No. LANCE A. MATTESON /560 E SAN FELIPE DRIVE SCOTTSDALE, AZ MSS X USCertiScated Meths* . AP 1861049 Foreign Calibrated Mothasic Certificated Repair Stab= Mazufactura a I catty that the mut andke abernice made to do =Ms) idadifiod in mei 4 dote mddesailed ce the Mint Ot °tea berm bin beCti mat to oxcart= with de nstprenamts or Part 43 ciT dic US Federal Mimi= Repack:4w al dads infamatica fonistoTtenia is me and correct beta tot at my Roma /age Date Ci : 2 / '' ?..., Signatia t 7. Approval for Retry to Service Pinson dm mitbrily pm persons spec:del Sow. the ma ideetifee in dm 4 arto imps old in the r natal by the Adminanore °fan Federal An Adman:sire and is CM APPROVED 0 REJECTED BY FAA D. Stmlurdi bcost. • Manufictister R ingo= Askant= Otter (SpolgY) FAA Drama Rcpt Stake Pc Amoral by Traimert Comae AirocatioasCiosp Due clApprovg or Reamial Ili ZIP , cot rs Onipasims Nu 324705494 LA &pat of Malrituni — - - -- — — Nfrined Dome& - - 13 r pilan7f44474C:re . . . SONY GM 02754201 L SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241123 EFTA01326716