........x. 0 MAJOR REPAIR AND ALTERATION uS Department (Airframe, Powerplant, Propeller, or Appliance) I of Transportation Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only OM Ide?tif ation INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE Model G1159B Serial No. 151 Nationality and Registration Mark U.S.A. N908JE 2. Owner - Name (As shown on registration certificate) • HYPERION AIR INC. Address (As shown on registration certificate) 3. For FAA Use On y 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. JET AVIATION ASSOCIATES LTD. WEST PALM BEACH. FL. 33406 _ U.S. Certified Mechanic CRS EYKR782D Foreign Certified Mechanic X Certificated Repair Station Manufacturer - - D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date $ - 6/28/00 Signature of Authorized Individual _,L6(34- 7 RONALD K BYSTROM MGR QUALITY CONTROL 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 X APPROVED K REJECTED : FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 6/28/00 Certificate or Designation No. EYKR782D Signature of Authorized Individual RONALD K BYSTROM, MGR UALITY CONTR '"2-z-r- FAA Form 337 02-88) EFTA00278235

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 accomplished.) G-IIB S/N 151, REG N908,1E, W/O # 15278, ACFT TT8831.9 LANDINGS 4792 THE FOLLOWING WORK WAS ACCOMPLISHED UNDER THE ABOVE WORK ORDER NO. 15278. THE AIRCELL PHONE HANDSET INSTALLED IN THE CONFERENCE TABLE AT F.S STA. 305.25 BY F.A.A FORM 337 DATED 4/21/00 WAS RELOCATED TO THE LEFT DRINKLEDGE AT F.S STATION 305.25. THE EXISTING WIRING WAS ROUTED IN ACCORDANCE WITH JET AVIATION MODIFICATION DRAWING ACS20001-1. THE INSTALLATION OF THE AIRCELL HANDSET WAS ACCOMPLISHED IN ACCORDANCE WITH THE FOLLOWING JET AVIATION DRAWING WHICH IS SUBSTANTIATED BY F.A.A FORM 8110-3. STRUCTURAL DRAWING • HBPA00008 REV "IR" DATED 6/27/00 SHEETS 1 OF 1 TITLED AIRCELL HANDSET RELOCATION REF F.A.A FORM 8110-3 DATED 6/27/2000 BY STRUCTURES DER DERT-510159-CE. A OPERATIONAL CHECK OF THE AIRCELL PHONE SYSTEM WAS ACCOMPLISHED IN ACCORDANCE WITH THE AIRCELL INSTALLATION MANUAL AGT.O1 A LOG BOOK ENTRY HAS BEEN MADE REFLECTING THIS MODIFICATION THE AIRCRAFT EQUIPMENT LIST WAS AMENDED AND THERE WAS NO APPRECIABLE CHANGE IN THE WEIGHT AND BALANCE. THIS MODIFICATION DOES NOT CHANGE THE MANUFACTURER'S CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS. END K Additional Sheets Are Attached U.S. G.P.O 1990-761-753 EFTA00278236

• . • r DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 27, 2000 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream MODEL NO. G1159B TYPE (Airplane, Radio, Helicopter, etc.) Aircraft NAME OF APPLICANT Jet Aviation LIST OF DATA IDENTIFICATION TITLE HPA00008 ,-_ _ . Aircell Handset Relocation, Sht 1, Rev IR Note: 1. This approval is for structural aspects only. 2. After the alteration, the aircraft must be returned to service by FAA authorized personnel. 3. This approval is based on-drawing review and comparison to similar installations. . PURPOSE OF DATA To approve structural aspects of an alteration to G1159B S/N 151 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.307 25.561(c) 25.601 25.603 25.605 25.609 25.789 under Part 183 of the Federal Aviation been examined in accordance with Regulations. I ( ) Therefore Regulations, data listed above and on attached sheets numbered established procedures and found to comply with applicable I Recommend approval of these data Approve these data. 0 have requirements of the Federal Aviation SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Structural David E. Haralson p,_„:ee-: 11,„_,L,.._._ DERT-510159-CE FAA Form R11 n . (11-70) SUPERSEDES PREVIOUS EDITION ER0112:1doc EFTA00278237

s• •L t EFTA00278238

2r; ' MAJOR REPAIR, A -AND LTERATION - ,,. Form Approved OMB No. 2120-0020 us Department - (Airframe, Pow- erplant, Propeller, or Appliance) _ . Transportation -.-, u For,FAA Use Only. • of ,Federal Aviation— - - • - — -- Office Identification — -- -- • — - — - Administration INSTRUCTIONS: Print 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 this form. This form is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM AEROSPACE — ' . Model G1159B ... _ Serial No. 151 . - Nationality and Registration Mark N908JE . . . 2. Owner , Name (As shown on registration certificate) . , HYPERION AIR INC _ . . ... Address (As shown on registration certificate) 1013 CENTRE ROAD SUITE 300 WILMINGTON, DE 19805 - 3. For FAA Use Only. The data identified herein complies with the applicable airworthiness requirements and is approved only for the ..se,_,r_sav_v_7 above described aircraft, subject to conformity inspection / by a person authorized in FAR 43, Section 43.7. (g I rig a. Yom, --- 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME . ... ..",.....„.„ (As described in item 1 above) 4.0~480~0040480~~~~4181, X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES, LTD. ORT , 33406 U.S. Certificated Mechanic - CRS EYKR782D Foreign Certificated Mechanic x Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 03/19198 Sign re of Authorized Indiv" eery L. h ppard, Av. Mng . 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is LI in item 4 was inspected in the manner prescribed by the APPROVED El REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport Canadian Airworthiness Group Date of Approval or Rejection Oii0a/?8 Certificate or Designation No. CRS EYKR782D Signat e of horiz Individ al Henry L eppard, v. Mngr. AA 1-orm 331 (12-88) EFTA00278239

NOTICE Weight and balance or operating limitation changes shall be entered m the appropnate aircraft` record. An alteration must be compatibleWith 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) Aircraft: Gulfstream, Type: G-1159, SIN 151, Date: 03119/98, W.O. 12307 Page 1 oft Removed the existing Universal Avionics model UNS-1A FMS systems and Canadian Marconi VLF/Omega sensor, and installed new Universal Avionics UNS-D FMS systems. The existing Universal Radio Ttining Unit, Database Transfer Unit and the Universal Loran C sensor were retained. This installation was accomplished using Jet Aviation drawings, FIVIS98001, FMS98002 and IPB98001, Rev. IR, dated 01/20/98 are substantiated by FAA Forms 8110-3, dated 03/11/98 submitted by FAA D.E.R. Mr. Norman J. Curran, FAA D.E.R. No. SO-780. The structural installation of 'the GPS antennas was accomplished using Jet Aviation Drawing HPA98001, Rev. A, dated 03/02/98 and is _structurally substantiated by FAA Form 8110-3, dated 03/12/98 submitted by Lauren Napier, D.E.R. No. SO-815. -The CDU's replaced the removed units at the same station using the existing DZUZ rails installed by the airframe manufacture. The Navigation Computer Units replaced the existing UNS-1A NCU's using the same mounting technique and hardware. The required annunciators were furnished and installed. The following annunciators were installed: MSG (message) annunciator, color amber WPT (wayoint) annuciator, color amber APPR (approach), color white SX (parallel track), color amber HDG (heading), color blue INTEG (integrity) color amber The above annunciators were installed in each instrument panel for their associated system. The existing No. 4 airdata computer was interfaced to provide the required airspeed input and baro- corrected altitude. The existing Honeywell Laser-ref INS system was interfaced as a blended sensor as well as the existing Loran C sensor. The No. 1 compass system is interfaced to the No. 1 FMS and the No. 2 compass system is interfaced to the No. 2 FMS. This system, the Universal Avionics UNS-1D FMS system has been previously installed and 'has obtained a STC approval in another type of aircraft, which qualifies this installation as a follow on installation per AC 20-130A and is qualified for FAA Form 337 Field Approval. The Static Loading of the installed equipment meets the requirements of AC 43.13-2A, Chapter 1, Paragraph 3 and was found to meet the requirements of Paragraph 2. Materials and practices comply with Paragraphs 4 through 12. The Electrical Load Analysis was performed in accordance with 43.13-1A, Chapter 11, Section 2, Paragraph 424 and was found to meet the requirements of paragraph 424, 426 and 428. Aircraft Metal Work involving metal repair or alteration complies with AC 43.13-1A, Chapter 2, Section 1 and 3, Chapter 6, Paragraphs 248 and 249. Hardware and materials used the installation conform to AC 43.13-1A, Chapter 5 and 7, Sections 1, 4 and 5 as applicable. Circuit Breakers, switches and connectors are of the type recommended by the aircraft manufacture or are MIL SPEC approved for aircraft use and meet the requirements of AC 43.13-1A, Chapter 11, Paragraphs 429 and 430. Electrical/electronic wiring was selected and installed lAW AC 43.13-1A, Chapter 11 and AC 43.13-2A Chapter 2, Paragraph 21, 22 & 27. Routing, lacing and tying complies with AC 43.13-1A, Chapter 11, Section 7. Wire marking complies with Section 4. Electronic equipment installation complies with • • ''sv- c. yj Additional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012160157 EFTA00278240

. • 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. NOTICE 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Aircraft: Gulfstream, Type: G-1159, SIN 151, Date: 03119/98, W.O. 12307 Page 2 of 2 the aircraft and equipment manufacture's instructions and AC 43.13-2A, Chapter 2, Paragraphs 21 through 26 and Chapter 3, Paragraph 44. The aircraft static wicks and control surface bonding was tested per the manufacture's maintenance manual and no discrepancies were noted. The UNS-1D FMS systems were functionally tested and no discrepancies were noted. The UNS-1D FMS systems do not interfere with any other installed system and all of the existing systems do not interfere with the UNS-1D FMS systems. Magnetic direction indicators were checked for accuracy and compensated as necessary per AC 43.13-1A, Chapter 16, Section 5, Paragraphs 927, 928 and 929 and AC 43.13-2A Chapter 2, Paragraph 23f. The Equipment List was amended and the new Weight and Balance was computed and entered in the aircraft records IAW AC 43.13-1A, Chapter 13, Paragraphs 659 and AC 43.13-2A, Chapter 1 Paragraph 9. The UNS-1D systems have been show to meet the requirements of VFR11FR flight en route, RNAV, terminal, over water, in remote areas and for approach modes per AC 20-130A according to the limitations indicated in the aircraft flight manual supplement. The FAA Approved Flight Manual Supplement dated 14 I$ (5? must be installed in the aircraft flight manual with this installation. END Additional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00278241

EFTA00278242

; " MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) • of Transportation Federal Aviation . . _ . -- . - . - - Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification S 0 — F.S t O ^ li 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 of this form. This form 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 G1159B Serial No. 151 Nationality and Registration Mark N908JE 2. Owner Name (As shown on registration certificate) HYPERION AIR INC Address (As shown on registration certificate) 1013 CENTRE ROAD SUITE 300 WILMINGTON, DE 19805 3. For FAA Use Only The data identified herein complies with the applicable _VI 9j9 t' airworthiness requirements and is approved only for the So -rS1YJ—\`7 above described aircraft, subject to conformity inspection by a person authorized in FAR 43, Section 43.7. /3 :Y"-\ str•o- 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. JET AVIATION ASSOCIATES, LTD. ORT , 33406 U.S. Certificated Mechanic . CRS EYKR782D Foreign Certificated Mechanic 3( Certificated Repair Station Manufacturer a 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 • 03-19-1998 Signatur uth• - ed ndividual . , -Henry L. She ard, Av. Mngr. 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is tit in item 4 was inspected in the manner prescribed by the APPROVED REJECTED BY FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Appr d by Transport Canadian rthiness Date of Approval or Rejection 03/19/98 Certificate or Designation No. CRS EYKR782D Si• atur ut -d Individu- enry L. hep , Av. Mngr. OI'M X31 (12-88) EFTA00278243

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 c • : (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Aircraft: Gulfstream, Type: G-1159, SIN 151, Date: 03/19/98, W.O. 12307 Page 1 of 1 Removed the existing Universal Avionics model UNS-1A FMS systems and Canadian Marconi VLF/Omega sensor, and installed new Universal Avionics UNS-D FMS systems. The existing Universal Radio Tuning Unit, Database Transfer Unit and the Universal Loran C sensor were retained. This installation was accomplished using Jet Aviation drawings, FMS98001, FMS98002 and 1PB98001, Rev. IR, dated 01/20/98 are substantiated by FAA Forms 8110-3, dated 03/11/98 submitted by FAA D.E.R. Mr. Norman J. Curran, FAA D.E.R. No. SO-780. The structural installation of the GPS antennas was accomplished using Jet Aviation Drawing HPA98001, Rev. A, dated 03/02/98 and is structurally substantiated by FAA Form 8110-3, dated 03/12/98 submitted by Lauren Napier, D.E.R. No. SO-815. The CDU's replaced the removed units at the same station using the existing DZUZ rails installed by the airframe manufacture. The Navigation Computer Units replaced the existing UNS-1A NCU's using the same mounting technique and hardware. The UNS-1D circuit breakers were pulled and collared pending FAA Form 337 Field Approval of this installation. The CDU's are placarded "INOP". These systems are installed for provisions only. The Static Loading of the installed equipment meets the requirements of AC 43.13-2A, Chapter 1, Paragraph 3 and was found to meet the requirements of Paragraph 2. Materials and practices comply with Paragraphs 4 through 12. The Electrical Load Analysis was performed in accordance with 43.13-1A, Chapter 11, Section 2, Paragraph 424 and was found to meet the requirements of paragraph 424, 426 and 428. Aircraft Metal Work involving metal repair or alteration complies with AC 43.13-1A, Chapter 2, Section 1 and 3, Chapter 6, Paragraphs 248 and 249. Hardware and materials used the installation conform to AC 43.13-1A, Chapter 5 and 7, Sections 1, 4 and 5 as applicable. Circuit Breakers, switches and connectors are of the type recommended by the aircraft manufacture or are MIL SPEC approved for aircraft use and meet the requirements of AC 43.13-1A, Chapter 11, Paragraphs 429 and 430. Electrical/electronic wiring was selected and installed JAW AC 43.13-1A, Chapter 11 and AC 43.13-2A Chapter 2, Paragraph 21, 22 & 27. Routing, lacing and tying complies with AC 43.13-1A, Chapter 11, Section 7. Wire marking complies with Section 4. Electronic equipment installation complies with the aircraft and equipment manufacture's instructions and AC 43.13-2A, Chapter 2, Paragraphs 21 through 26 and Chapter 3, Paragraph 44. Magnetic direction indicators were checked for accuracy and compensated as necessary per AC 43.13-1A, Chapter 16, Section 5, Paragraphs 927, 928 and 929 and AC 43.13-2A Chapter 2, Paragraph 23f. The Equipment List was amended and the new Weight and Balance was computed and entered in the aircraft records JAW AC 43.13-1A, Chapter 13, Paragraphs 659 and AC 43.13-2A, Chapter 1 Paragraph 9. END Additional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE 1992-769-012=157 EFTA00278244

tck F el eV MAJOR REPAIR AND ALTERATION US Deportment of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification GEORGIA FSDO 11 e-u-1.1 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 of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make GULFSTREAM Model G11598 Serial No. 151 Nationality and Registration Mark U.S,A. N979RA 2. Owner Name (As shown on registration certificate) GULFSTREAM AEROSPACE CORPORATION Address (As shown on registration certificate) P. O. BOX 2206 SAVANNAH, GA 31402-2206 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ,....s."......................4.04,....N., (As described in Item 1 above) 4.,............................. X POWERPLANT ,-.---c 1, PROPELLER t,,,,, V131 et-•:-D \ , t; ; 1 1 — -`-\ 1. c ,,,,,, , ' 1.)•-) 0 , APPLIANCE Type ELEVATOR . '\ I/ _ '; 1159CS20002r 0, 1 -- WS0.0-R?1,1.„, 1159CS20002 -2 1 '-'-`t 1;1)L/H X '''151 -5 R/H Manufacturer GULFSTREAM 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. GULFSTREAM AEROSPACE CORPORATION P.O. BOX 2206 - TRAVIS FIELD SAVANNAH, GA 31402-2206 U.S. Certificated Mechanic GR4R216M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 08/31/93 Signature of Authorized Individual JIMMIE K. SMITH . - )( .027".e4 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 EX APPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 08/31/93 Certificate or Designation No. GR4R216M Signature of Authorized Individual JEFFREY C. NEVILLE FAA Form 337 112 RR) EFTA00278245

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) AIRCRAFT MODEL: G1159B AIRCRAFT SERIAL NO: 151 AIRCRAFT TAIL NO: N979RA AIRCRAFT TIME SINCE NEW: 7173 AIRCRAFT CYCLES SINCE NEW: 3959 REFERENCE: GULFSTREAM AEROSPACE CORPORATION WORK ORDER NO. CO2B-151-093-6035. 1. INCORPORATED GULFSTREAM AEROSPACE CORPORATION CUSTOMER BULLETINS CHANGES LISTED: CB NO. SUBJECT 357 CABIN FLOOR STRUCTURE AND INTERNAL INSTALLATION STRESS ANALYSES 374 INSPECTION & REINSTALLATION OF NONPRODUCTION BLADE ANTENNAS MOUNTED TO FUSELAGE STRUCTURE 2. COMPLIED WITH ELEVATOR BALLAST WEIGHT INSPECTION I/A/W GAC DWG NO. 1159SB30189 REV. D. 3. COMPLIED WITH BEAM STRENGTHENING AT F.S. 345.88 TO F.S. 379.00, BL 18.50 AND BL 30.50 L/H & R/H I/A/W GAC DWG NO SE25105105. THIS REWORK COMPLIES WITH CUSTOMER BULLETIN 357. REFERENCE REPORT NO. 1159SER93-177 FOR DETAILS OF THE ABOVE REWORK. 4. MANUFACTURED AND INSTALLED A DOUBLER P/N SE25202111-11 AT F.S. 630 BETWEEN STRINGER 23 AND 24 R/H I/A/W GAC DWG NO. SE25202111. THIS REWORK COMPLIES WITH CUSTOMER BULLETIN 374. -END- O Additional Sheets Are Attached IttU.S. GOVERNMENT PRINTING OFFICE: 1952-769-012/60157 EFTA00278246

. . • •CS • . • MAJOR REPAIR AND•ALTERATION US Deprxernent CI kanSx•anon (Airframe, Powerplant, Propeller, or Appliinte) • • Federal Aviation Administration - • Form Approved OMB No. 2120.0020 For FAA Use Only entificaalopz07 INSTRUCTIONS: Print or type all entries. Sei FAR 43.9, FAR 43 Appendix .B, and AC 43.9-1 (or subsequent revision thereof) for instructions and dispotition 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 1959). __ 1. Aircraft _ Make —GuIfstream Model Q-1159B ' Serial No. ' 151 Nalioricility and Registration Mark N908JE ' 2. Owner Name (As shown on registration certificate) • . , . HYPERION AIR,: INC. • Address (As shown on regiitration certificate) 1013 Centre Road, Suite 300 WIlmInton DE 19 8 05 • 3. For FAA Use Only • • ! ! h, . • ,; •,; • a7,-.!:?=. •,•,..•1 - 4. Unit Identification . . . 5. Type • Unit . . - • • . . . Make ' Model _. , -. • ••••• ' 1 Serial No. • • - • Repair Alteration AIRFRAME ..- . (As • : . . ._. , .. , described in item;1 above) ......:44........;..~....... • k . ' X . . • POWERPLANT . . , . ,',' • . PRDPELLER : ' '• _ . APPLIANCE Type • ..- . Manufacturer 6 Conformity Statement A. Agency's Name and Address - • •, • . - B: Kind of Agency C. Certi icate No. : Elcctrosonics Division - : - • • ^'.r: AiRadio Corporation '. • '-. • - • Port Columbus International' Airport , Columbus. Ohio 43219 U.S. C-ertiliCated Mechanic- • • • Repair Station AE1R005K ' Radio Class 1, 2, & 3 Limited • Instrtiments Limited Six.cialized Services • • - Foreign Certificated Mechanic X Certificated Repair Station Manufacturer • i3. .I certify that the repair andidetteration made lathe tin't(s)'dentif have been made in accordance with the requirements furnished herein is true and correct to the best of my kid in item 4 ibove of Part 43 of the U.S. Federal knowledge. • ,- Signature of Authorized 1--- iandieleribectiiii itierthrse or attachments hereto . Aviation Regulations and that the Information • • . .. .. . ._ . Date AUG 0 7 1994 : - yid I • • . 7. 4nit i nfed is 3:4 APPROVED Inspection Authorization nice Ptisiiant ' Administratorof BY • to the authority given persons specified the Federal Aviation Administration below,,the and in item 4 was inspected O REJECTED Other (Specify) . in the manner prescribed by the '. o., • FAA Fit Standards Inspector ' • • — : . . Maiiiiiacturer ' FAA Designee , • X Repair Station Person Approved by Transport Person Airworthiness Group Date of Approval or Rejection SEP 1 9: 1994 .. . Certificate or Signature of Authorized Ind • ual Designation No • • AEI R005K i . .... .. .2 ,. .. ... ..• . vi . Malt D. :Haycock re: EFTA00278247

.NOTICE Weight and balance or operating limitation changes shall be entered in the applopriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (It more space is required, attach additional sheets. Identify with aircraft nationality and A mark pistration and date work completed.) . • . . • PART NO. PART NAME . Sony Compact Oise- Changer 321-.50 EIS Drawing E Sony Digital Preamp • 355i50 Sony Digital Croisover ' 355:50 .: Sony Amplifier ' t • 385.50 Sony Amplifier . - • ,a85.50 --- 2 ea. 'Sony Amplifici ....:, :,7j ; ... c ,... . "34..56 :' • XESTI _ lea. Sony Timer - 385.50 •-:. QM25HC tea. Sony Speaker (Tweeter). -- - 7193.00 . Sony Speaker (Tweeter) ;4,12.60 Sony Speaker (Midrange) ..193M0 -, Sony-Speaker (Midrange)- .:.. ' ‘442.00 - ---,--'•-• • - -- - -5 • A404 2 ea. Precision Power Amplifier • -" •%-: 1 :- -: 383:50.'- . : a: --;- :- -.-- •--r: 1:ea. Stillwater Designs Subwoofer .... 193.00 -.: :.....". SIOA lea Stillwater Designs SubWricirei-h-t xr j--442M0-- g ea. MS Quart Speaker 193.00 2 ca. isIS Quart Speaker . 442.00 ' ,. . 4 ca. S DC-to-DC Cnverter , M0 :: KG Convener 580 . . . 1 ea. Audiolniemitional Tcmp Control . 275 00 - • VB/VDA - , i ea. Video Accessory Video Amplifier _ _ .. 93.00_ . 2. The above work was accomplished I.A.W. A.C. 43.1171A; Chapter: 11: and A.C. 43.13-2A, . Chapters 1, 2, and 3., , 3. Electrical load check LA.W. A.C.43.13-2A, Chapter 2, Paragi:aph-27 and found to be yithin lint This work his been accomplished under E/S W0rieggier442748, - The Cabin Entertainment System has been installed L'ANI: FAA Advisory Circular A.C. 25.10 and ElectroSonics Drawing #ES1159c151-90 dated April 25$1994. The aircraft has been weighted by Gulfstreath concurrent withihis installation. • Aircraft must be loaded:LA:W.. the prescribed loading information from the manufacturer. " -Tga7 ac t . co •ocic-2Ip-31 c ' '.CA-7 6 - • O Additional Sheets-Are/Ctratingt - EFTA00278248

h. J . . . . —, - — eve‘-••— — nes - -.- Form Approved - , ; .• . . . OMB No. 2120-0020 REPAIR AND : MAJOR ALTERATION:, itStiorehmers ' • For FAA Use Only • otsolsoonotor „.. v..-; (Airframe, Powerplant, Propeller; or tAtt• •••,.. ,, • office Identificathin' vliessfr iiii . . -,,----- .. .. . . ....— ...... , r51,0 ell of 7 i A. 6 4k, INSTRUCTIONS:Print or type all entries. See FAFI;t3.9:iiiR iiiithiendix e. and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required bylaw (49 U.S.C. 1421). Palliate terepcirl can result in a civil penalty nol to exceed $1.000 toreach such violation (Section 901 Federal Aviation Act of !got. , L. c , /: ; • Make . \ ' ?3..!3f0 T41..ir:AFAA . GULFSTREAM . . • . — Model . . . G1159B • . • _a-. i , .. ,.i • .i. s,.. 1. Skin Serial No. .. 151 - %.- Nationality and Registration Mark U.S A_ N908JF 1 ; 2. Censer !/1 (As, shown on cepstrstl,ppq!)550?5,eA.-,y 1 1.10 ., ,:. : . • • • • . HYPERION • AIR Ititis. attio--t.-. ZA 1371.;.:', )..... . , , . ,: . ....:::. 1 itoir.le.:0A- -; t se-1 kci.o.-:t. Address (AS shown on registration certificate), , . . , 1813 CENTRE ROAD SUITE .300 - WILMINGTON. DE 19805, • „ , .2 •..4 '%•n::.. .:.2f1. 272:0!fl773; FistFAA4,1sethity.. ..:., , .,.. . .; . „ . 7 .. / i): . LI ;A i E PI 111;4;b1 .w-,'t'i' LI' ;I :1131.i) itin: . . ..),:.•. ,:: ....11/4fr. . .. .:. 1, 3 .. ..);'..1litilit - 1.,..c ; l,.",? i Na; t! a Hi! I . i • I I 2 --• I II .2) 2. f .i 0 2 2•;` i - ... • .. ; 1 .- I i •, '11... '. ,-i / ;.: ‘' . 4: Ural IderUfficatkut .-. - i . , .- S. Type i - riiic . • - ••,, 1 ! f • •;;I, ' Make' • ' ' - •-• ' I 112.. : ., , ..-- -; ,,. - iitcy";•-1 . Model , • '! Serial No. !4 .Rapair . i7 Alteration • 1,Al4..-4: ;•, t , , . - ()A . described in Item 1 above) - . • . ... . .. t • • AIRFRAME .. ;,-..,;,...1.":-; .:,-.•• 7 11". (As •2 0 . • -.. POYVERPLANT . : :M. t! :: I, A!,! A ... . PROPELLER __ . _ _ _ . .. )1 A ',. ci l ',t,,t 1 ,Ai:4E,ii _ ,3 9V4 1 • ... I • ii4LiAtiCE Tre! •,:1f,-, i ,tr, :!•.)51.70? 1 , . . . ?i,c,f1:: _ 4_ 11 ;7.. ! 1. . ortiFSftr" 4 ektra it. • : t Manufacturer/4y.! • ; • \R tf“,;•! ;'..,...; II ; , -• . i , . 1 1 r :01 ; -. -if ;,'.5. 6. Confonnity Statement • . '- A.3Agencyi game and Address • 4 ,, .-'" if : ;_ . I in' EL,,Kind of Agency . . • C. Certificate No. . • :i , I s' , . I US. Certificated Mechanic : • i . GULFSTREAM AEROSPACE CORPORATION Foreign Certificated Mechanic i P.O. BOX 2206. - TRAVIS FIELD x Certificated Repair Station: , GR4R216M , :. SAVANNAH, GA 41402-2206.: J., • Manufacturer: , 6. I certify that the repair and/or alter:itkin made to the un I have been made,inace.Ordanrie with the requirements i furnished herein is true and eeriest to the best of my t(s) identified in item 4 above and described on the reverse or attachments hereto of Part 43 of the U.S..Fecteral Aviation Regulations and Mat the information knowledge. Date I, , . . ' . . I • 08/05/94 . i- I., -, " Signature of Authorized individua . • „ JAMES M. GRANT.. ... 7. Approve for Return To Service • Pursuant to the authority given persons specified beldw, the unit identified In item 4 w inspected in the manner prescribed by the Mmiriistrator of the Federal Aviation Administration antis .,. Ill APPROVED . 0 REJECTED , - - • . .. .. .. •• FAA Fit. Standards Inspector. . .. • ' ' MinufactOrei ... _. • ...,A , , • : Inspection Authorization' • Other (Specify) ' . . ,.. . i.J 84 t. • • FAA Detignee .. . . . Xi ),..-1, Repair Station Rep . • i Person Approved by Tranapon Canada Airworthiness,GrOvp ; .i - . . Lr. .. • Dee of Approval or Rejection i 08/05/94 Certificate or Designation NO. GR4R216M Bigneture of Authorized lnilivfdeel I' ; ' - _t._, - .. JIMME.K..... SMITH , . A...- ....(inj f itnniniaTh • " 1 ;:r". 4. AC•/%5 • • • • • • t r •tiCi EFTA00278249

• . • Weight and balance or operating limitation changes shall DO entered in the briptePriate aircraft record. An alteration must be Ctinipitibliii with previous alterations to assure contirkietitcohloiMily-Witfrtife apbliCableaitworthiness•raquirements. • DescdpUon of Work Accomplished' • •, ,., ; e r.= "..,:- 4 ;-_, •,. t• . % ' f If mOre anise is required, Attach additional sheets: Identify with tdrteaft nationality and registration mark and date work completed.) — • AIRCRAFT MODEL: G1159B . _. . --- ,- ---- - TIME SINCE NEW: 7224 ' ' .'':: ,.,'. ': AIRCRAFT. AIRCRAFT SERIAL NO: 151 . "'-' 1 -- AIRCRAFT CYCLES' SINCE NEW: 3992'; AIRCRAFT TAIL NO: N908JE(f.2;.', 10.. ____ 1-- . ' . ' '. • . ... . •,-.. ., •--:,,,r1;:.•,..-.•,.:.,- !,:r.f.,; I 1_ • REFERENCE: GULFSTREAM AEHOSPACi-CfliOIATION WORK' ORDER NO.- CO26-151-64673i; 1. INTERIOR FURNISHINGS:WERE REFURBISHED AS STATED_. BELOW. ALL MATERIAL MEETS AND- EXCEEDS F.Azie 25.853 (06/20/68); APPENDIX F (10/24/67):'FLAME _ RESISTANT STANDARDS. COPIES' OP_ LABORATORY REQUESTS AND BURN REPORTS ARE ON FILE UNDER THE ABOVE- WORK ORDER AT THIS REPAIR STATION. DRAWING NO. REVISION SC21 491001 _ . _N/C ___.__. SC21 551001 .. N/C ' SC21 581005 N/C - SC22 208006 N/C SC22 800002 N/C •• . SC22 236003 • , ! 11 USAGE Ii ~ FWD CABIN BULKHEAD'S__ I , IPSU &' H-EADLINERS %trazIAIDtiAnti-PANELS ' ! BR8100 DIVAN, AFT SINGLE.' SEATS • _ .FLOOR CARPET • .! BR8102 .• . . CHAIR BASE , .. AI R DUCT - BR8103 ... WINDOW PANEL, CLAM` SHELL INSULATION' BLANKET . • CARPET PADDING' . • CHAIR SHROUDS . f • TABLES, RADIO RACK _ • !COVER, CABNT BR8259.::r4,-)po rr;< •q-;, -% DIVAN CABINET;• R/111.-' • . BR8260 - - CABINET, '6ALLEr0/01 BR8261 LEDGES, CAOINET.ITOP-S„:---... BR8262 _ . . . , BULKHEAD -DECORAT.IVESLA.:'. 8R8262.-. • <, • DIVAN CABINET, CREDEN2Ar- BR8282 • TOILET SEAT- / SHROUD BR8283. .t CABIN SEATS . „. .; .BR8284 HORSE COLLAR MAIN POWER DISTRIBUTION ELECTRIC SEATS'(ERDA) CABIN INDIRECT LIGHTS' . CABIN SEATING INSTL-, .1/10 FLOORPLAN MID CABIN- STORAGE cA01,7 NATERIA NOMEX, FOAM; FABRIC FABRIC, METAL, FOAM FIBERGLASS; FABRIC',` ` FOAM FABRIC, FOAM::' • CARPET, WOOL . CARPET, METAL • FIBERGLASS; FABRIC NOMEX; ISO DAMP, GLUE NOMEX ' j-: • LEATHER; METAL;' GLUE • VENEER, FINISH, HONEY. • COMB • r LAMINATE, HONEYCOMB • PANEL " LAMINATE,- HONEYCOMB PANEL VENEER, GI LFAB, FINISH"..; A=LOOK MIRROR AL HONEYCOMB, LAMINATE LEATHER, NOMEX, FOAM' LEATHER; FOAM ; LEATHER;: METAL, FOAM AIRCRAFT ELECTRONICALLY WEIGHED: .' _ WEIGNT4N6!BftLANCE. OATA REVISED AND . INSERTED INTO THE. AIRCRAFT-WEIGH:FANO, BAL%NCE MANUAL. " G,. 1- END-'• 1 • • .1!: 0_1a2 • O.; '3 • *U.S. GOVERNMENT PRINTINGOFFICE: 1992-7fie,otaliam 't..;-,4afrl iFf userr•roar . „ . EFTA00278250

Att 'V. rrarre r f an • - . „ - - • -:isestri - UNITED STATES or a:mend* . ' • " 4 DEPARTMENT OF TRANSPORTATION -FEDERAL AVIATIOlt#312MINLSTRATION STANDARD AIRWO SS CERTIFICATE.- ' 4 MANUFACTURER AN 5. AUTHORITY AND BASIS FOR ISSUAN This airworthiness certificate is • • dote of issuance, the aircraft • therefor, to be in condition f • • comprehensin and detailed Aviation, except as noted Exceptions: it 6. TERMS AND CONDITIONS Unless sooner surrendered, su this airworthiness certificat performed in accordance aircraft is registered in tyj and certifies that as of the form to the type artifice% ufrements of the applicable on International Civil ablished by the Administrate(;' intenonce, and alterations ate— ationa, as appropriate, and the Any alftratione reproduction, or misuser of this °Mikan be pure by a Snit no exceeding 51.000. Or km prisonment not exceeding 3 yews. or both. THIS CERTIFI TE MUST BE DISPLAYED IN THE AlltatAFFINI3ONDIQ1 • ANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. • 'Aste r•-- ' _ — '"!"-"'iTtrr • • .. -3Sr%w / . ."• 11-rwrodiniayse ;'. -..j.se ; ex EFTA00278251

• • • • ' • . • • t.e.. ."-c -Ite7eFi; EFTA00278252

• UNITED STATES OF AMERCA DEPARTMENT OF TRANSPORT AT ION—FEDERAL /ORATION ACIASSTRAT ION , STANDARD AIRWORTHINESS CERTIFICATE AUTHORITY AND BASIS FOR ISSUANCE Ths torwortinness certificate a ctsued pursuant to the Fetters' Avrahon Act 01958 and rendes *Lateits den of ISSWITCO. The me raft to witch axed ha been respected and COMM to ccintorrn to the type certificate theroba. tkbe el coition tor sale operation and ha been shown to meet me redo:Icemen of the applicable comprehensive and Staled arworthress code a Perded by Annex a to the Convention on Internat.:nal CAI Anton. excePt as noted teen Exceptions TERMS AND CONDITIONS i Unless soarer surrendered. suspended. choked or a termrnatiorf date is oMeninse eStabtaned by the Ad:nu-testator. the tenvortruness cenrfr-ate a effective n Icing es Ito maintenance preventative mantenance. wed alterations we performed n accordance with Parts 2l. C. and 9l of the Federal Anton Rego Latons. as apgrgp4aIe. end Me thrUa ft a regained m the Une] Sayers Any Vleraimn reproduchon or misuse altars certtlata may S ponaltabie by alts not execcdong $11:00. or empraonmerd not exceecing3 leis or bah THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH. APPLICABLE FEDERAL. AVIATION REGULATIONS . EFTA00278253

_ • ;-: • ' ‘• ; • "r t 74 hT•eilfi- = lir; "i• •••tn .. "...A j•••ANg •.. • • •.•+. gi•••-•••. ., • • lass. a i't • •i• • • • illiillam•aarCieleala•• •-• . • • • • • EFTA00278254

• UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 4 CATEGORY S AUTHORITY AND BASIS FOR ISSUANCE This a iiwonniness centhcate is essuedborsuant tO FederalAviationAct of 1958andceneesMat, otthedete of issuancethe • ; eircran to whin issued has been inspected and loon' To contr.- ',to the type certificate therefor. to be in COnditen for sale „. ePeranOn and has been shown to awe the requ:rements at the ilibcticabite comprehensive and detailed airwOrthineSSCOdeaS r.sc-ndad by Annex 8 to the Convention onIntenetiore Cml Aviation. except as noted herein Exceptions f 6 TERMS AND CONDITIONS - Unless sooner surrendered. suspended. revoked. Or a termination dates otherwise 4 taNrshed by the Administratoc thn afrworthiness certificate U etteimn.; as tong as vie maintenance. preven:ative maintenance. and alterations are perfOntied acconsance with Pans 2I.43.and St of Me Federal Aviation Rezifations. as top? ie. and the aircraft is registeredintheUnited • States AT= ; I 'A DESIGNATION NUMBER O352 ... I . Any alteration. reproduction. Of MI use Oi this cerhficale may be puns .:-' by a line not eaceecang ST000. o imprisonment notWeedinga .i years or both THIS CERTIFICATE MUST 8E DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL ! ' AVIATION REGULATIONS i 1 -- -./ , FAA Form 81O0-2 18-62) °DPI" *U.S. GPO: 1989-662-97* i • L. ./ i • r ';' : : .. ..o.". • • ...mr 0. ... ' re l5c 4librAA,tom : . • •=r•-•- . ••:•••• ' • 1 . - . EFTA00278255

. ; • EFTA00278256

.• • UNITED STATES OF AMER lc* DEP.MiTMENT OF TRANSPORTATION—FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE . AUTHCRITY Ase.BASIS FCR ISSUANCE . ' . . ... nt.'s airtienhiness certif.:ate is issued puritan: tof he Fsderal Aiiation • '''' &imp?: to Writah issued has been itopected and lecnd to Ctr -• 0pera:manta has been ShtSn to meet Me recuirenems - . a rov:ded ty Anrerefl h the Comer:tic:a on Inferrar Snipers . t ISPORT . . . , . evil-lesthat as of the date°, issuance. in, cirtifi te thireter. to be in condition for safe - - comcrehensive and detailed airworthiness Cede as - • 1, cri except as rated herein. . . . - . • 6: TSAI/SAND CCNCITICNS Unless-sooner Wein• ..susoened.• revoked, cr a terhunat4n dee h otherwise established by. the Administrator. this .. : ; • ... saw:Minos% e is illicit* as lvig as the maintenance: oreventarnnt ma•ntenance.-and et/Mimi are performed in ;" % - • . . .accoreince ans21.43.and9.1 oltheitederalAviaticnReeutatrons.asanorconate. and theraircrihriregeterir4IntheUoted f f . . . • DATEOr) DESIGNATION NUMBER: rfr • " 7-689 STL-FSDO .• •-•., Any ai;eration. reproduct;ch cr mi use crtnis certificate may be punisnabv by a Lne not exceeding SIDDII.or imprisavnent not escisedarg 3 I 'years. or bosh. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCR.A.:T IN ACCORWICE WITH APPLICABLE TEDEflAc. PrIATiOi:RSGULATIOMS. • . . • • - v.rstiati. as* EFTA00278257

- • - - - • . t - - • EFTA00278258

• MAJOR REPAIR AND ALTERATION Form Approved OMB No• 2120-0020 US OenCarlene acintoonorcn Powerplant, Propeller, or Appliance) For FAA Usie Only or (Airframe, Newel iberafron ,.. geninistroecet 0,(fice Identificati &N, STL-F 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 of ?hit form. This report is required by law (49),I.S.C. 1421). Failure to report can result in a civil penalty not to exceed stair for each such violatIoil (Section 901 Federal Aviation Act or 1958). 1. Aircraft Make • • . . Gulf stream Aerospade Corporation Model • G-1159B • , Saha; No 151 • - Nationality and Registration Mark N979RA 2. Owner Name (As shown on registration certificate) : . _ . , Ogden Managemeit serviceii,Inc. • Address (As shown on registration certificate) • Westchester COunty Airport, Hgr D3 White Plains, New York 10604 3. For FAA Use Only • - C. - - 4. Unit Identification 5. Type Unit II I Make I Model 'Serial No. Repair Alteration AIRFRAME -.... (As described in Item 1 above) X POWERPLANT '1'. • • PROPELLER • . ert Cretr:: ', L• @t' . fit ". A: ; APPLIANCE Type , AlPf? 1 3 499e Manufacturer . Si/ - /Si 6. Conformity Statement j u A. Agency's Name and Address . . I B. Kind of Agency I C. Certificate . I U.S Certificated Mechanic Midcoast AviatiOn, Inc. I Foreign Certificated Mechanic # 8 Archivew Drive Certificated Repair Station ZtO3R822L Cahokia, IL 62206 . I 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 • April 1, 1992 Signature of Authorized Individual Joseph L. Allen 2 11--- 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 6 APPROVED 0 REJECTED I 4 FAA Flt. Standards Inspector Manufacturer Other qpecity.). Inspection Authorization BY 4- FAA Designee Repair Station . Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection ., • 4-1-92 ' Certificate or Designation No. . RO3R9221. S' ture_of Authorized Individual ....,ent i s,/,‘ ; a -- 07c dor__ Jimmie A. McCrary - ▪ "• • - • • • _ • • • . . • - . _._-_.- • - • ' EFTA00278259

. . . NOTICE . . . . . Weight and balance or oPeraring 4mitation changes Thall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued Conformity with the applicable airworthiness requirements. . , • B. Description of Work Accomplished (If more space is required, attacr additionalsheine. Identify with aircraft nationality and registration mark and date work completed) 1.) Removed left eievatbr P/N 1159CS20002-1 S/N 151 and riaht:elevatcir P/N 1159C920002-2 9/N 151, 'Conducted inspection for corrosion 'on balance beams, no corrosionjound.• Performed _steps 1, 2, and 3 of Sulfstream Drawing No. 1159S830189 Revision "C" date, 2-4-92 "Corrosion Repair - Ballast Instl., Cont. Surf., Elevator". Balanc,:. checked aoth ' eleVatOrs, found to be within liMiti per Maintenance Manual chapter 27. Reinstalled elevator_ same part number .and serial number, op's checked DR. 2.) An appropriate entry was made in the aircraft records. - :7 aCt ..7. ::e.v=S: :7 (f!q: :t;te,r :sterns a,. ors: t.: :.1 r e eo: • ' ^:' - ••• ty;:i? •;:t • . . tft . ‘C • • l. titsRs,,:4 ..P•v..1 1- : oil ar.vi .!. flyig‘t.ett ,1/2.volod Ocift2urea • . ' in • 0 -.7 .';')SS-t1A ) . • rif r' 7' ' 234!2) C.04.r.:11C es;:vt% . .:tin:. ...: ":fell • 77•1::.::::!-:;r1.1;.°•tOutrT;;; C:j: '" O Addrtionel sheasAitAttactied tt• r• %.0? " t EFTA00278260

iy - MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-0O20 US Otoortment Appliance) For FAA Use Only a Irani= =hal (Airframe, Powerplant,- Propeller, or . Moroi Mb don Admhnistmtlon 1 Office Ident:rcation. cfPrZ-fS: • .. . ... .. _ . .. INSTRUCTIONS: Print or type all entries:See FAR 43.9. FAR 43 Apc-endix B. andAC 43.9-1 (or subsequent revision thereof) for instrittions and disposition of this form. This report is required by law (491.J•S.6.1421). Failure to report can result in acivil penalty not to exceed 51,000 for each such violation (Section 901 Federal. Aviation Act of 1958). 1. Aircraft Make Gulf stream Aerosoace Corporation Model G-11598 Serial No. . 151 Nationality and Registration Mark N979RA • 2. Owner Name (As'shown on registration certificate) . Ogden Manageiaent Servicts, Inc. - Address (As shown on registration certificate) Westchester County Airport, Hgr D3 White Plains, NY 10604 "The••alteration identified ho44;i0hFA4-kriFto,ntr, flip A pp;irphta airworthiness requirement's and is approved for the above thscribzd 'eirc..r.Ift: sk,b-fect to :nntormity inspection by a person authorized in. FAR rat •!1:32 Section 43.7..."- 5-1 - ic3 A9 -3 -4' Se;" ezete44 7 -District Office Qat? - EALL4aspector • 4 tint Identification . 5. Type Unit - Make L • Model . Serial No. Repair I Alteration ... (As described in Item 1 above) X AIRFRAME • ... POWERPLANT . • . --- PROPELLER • • APPLIANCE Type Manufacturer • . _ ----- •-• : ; 6. Confo'rmity Statement .. A. Agency's Name and Address B. Kind of Agency C. Certificate No. Midcoast Aviation, Inc. # 8 Archview Drive Cahokia, IL 62206 U.S. Certificated Mechanic Airframe Class 3, Limited RO3R822L • Foreigntertificated Mechanic X Certificated Repair Station . - Manufacturer D. I certify thatthe repair and/or alteration made :o 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 knowledge. Date Seotember 13. 1991 Signature of Authorized Individual Barry D: Griffin ' • 7. Approval for Return To.Service Pu suant to the authority given persons speCified be:ow, the unit identified in item 4 was inspected the manner p cr ed by the Administrator of the Federal Aviation Administration and is IR APPROVED .O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization , .. . Other (Specify) • BY • FAA Designee x Repair Station Person Approved by Transport Airworthiness Group ' Date of Approval or Rejection /O - ; 7 - el/ Certificate or Designation No. RO3R822L Signature of Authorized'Individu o-.... \/ .,.. •• EFTA00278261

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 ) Updated the existing C011ins'AVR-101tockpit•Voice'Recorder System which was previously approved on FAA Form- 337 dated' March 14, 1975 and. STC #SA999SW, inaccordanCe with.Midtoatt-Aviation, Inc. wiring diagram no. 02-344W011 Rev A. "CVR Mod (WD)", and . the manufacturer's - AVR-101 Airborne Voice-Recorder. SyttemjMaintenance Manual # 523- . 0757366-201114 2nd Revision1.5.Feb.' 196.8 and•Baker Electronics Manual # 23-50-08 Rev. .1 InStallation and Operating Instructions. The update complies with FAR 25.1457. . A satisfactory preflight-functional check was conducted per Midcoast Aviation, Inc. report .no AB910001.-A.satisfactory ground and flight -test was conducted per FAA CVR 6round and Flight Test Procedure and the recording was down - loaded on two. (2) cassette tapes. All channels'operated.normal. The tapes are on file at this facility. The operator was supplied with "Pilots Operation Instructions" for Collins AVR-101 Cockpit Voice Recorder", report no. A8910001. This report must be aboard.the aircraft during all flight operations. The above mentioned installation drawings were D.E.R. approved on Form 8110-3 dated 9-1.3-91, Midcoast File No. MC910261. Inspection requirements per Collins AVR-101 Airborne Voice, Recorder System Maintenance Manual .* 523-0757366-201114 15 Feb. 1968 2nd Revision. Perform the "Preflight Functional Test" and the "Additional System Test" every 30 calendar daySas-prescribed in the manual. *B: -The-Underwater Locator Beacon Battery is to be replaced years from the date of fabrication. . . An Appropriate entry was made in the -aircraft records. O Additional Sheeti Are Attachicl .• !• •-khrfj-: • EFTA00278262

MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) for fAA u. Office loentitication • • • INSTRUCTIONS' Print or type au entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and Disposition of this form This mon is requiredby law (49 U.S.C. 1421 ):Failuretti report can result in a civil penalty not to exceed 31.000 tor each such violation (Section 901 Feoeral Aviation Act of 1958). . c.... 7.- N979RA .7 :‘•' 7. AaareSS (As shown on rep:strewn certificate/ . 4-.. iv. 1,4 . Westchester County Airport, Mgr D3' • .';-.:-,:....c.;“. '. White Plains, New York 1O6O4 Midcoast Aviation; Inc: * 8 Archview Drive Cahokia, IL 622O6 ' D. t cent' ytnat tne repair anttoe alteration mace to ine Linitis) ioentifiet in item 4 abcive andbescribec on Ine reverse or attacnmerns nereto have been mace in accoroance with the reouirements of Pan •43 of the U.S. Fecieral Aviation Regulations anc mat me informatioh furntsned herein is irue anc correct to the DP—S1 Of my knowieope. . . Pursuant to the authority given pei-sonispecified below.line.Unit. Identified in. item 4 was inspected in the manner prescribed by tne Acministrator of the FeoeralAviation Aommistration ant is' APPROVED ' p REJECTED :Signature of Authorize0 inowicual IL.C.77.,tyr.(..; • at fit EFTA00278263

:•• •• . NOTICE Weigir and balance Of orienting limitation chansfeistuilebe entered in the appropriate aircraft record. An alteration must be corntotible with ell-prewiouS alterations to assure continued conformity with.the applicable airworthiness requirements. • • ., .. , . • . 1. Dosnption of Vera Accomoissobso (If more space a required, atiao additionsl sheets: ldentilywith aircraft nationality and registration mark and date work completed.) 1HC• upcatec tna e:;iszinc czil4ne:Atrn-*ol ;:eciceit Recoroer System .which. was previOltslyHappro-4ed on .FAA Form 537 dated Marc;, 145.1975 and accordance . with- Midcoast- Avi at-ion. . Inc. wiring ioram ho. 13 344W0!1 "CVR Moo ..(WD) " • land '-the mental acturer s AYR-101 'Airborne':cite Rscfrtsr aystem Maintensnce Manuel # CM-0757:68-201114 .'2nd Revieion 15 Feb: 1 .959 -mind T.Iii?er.ElecironicE Manua. 4.- den-5c---JS Rew. zvzi on- ..q.mc Dperati Hp :ns.tructicirise he update tompIiet witn. • -s y' unczi br s, check per: MlOccast report no: AB91(≥c,Q1.fending a satisfactory ground And cfi ipht C1-5R Arks/PI sht, TeSi. firoeenurs. 7ie system • k 87 -zr.E. CirCtO,breaker. SULirei 1 ek 4:1h "Pi lotr... Operation Instructions. for • :plains 1WR-1:01 ;cc !pit . Voi ce Recorder:', recur. t-• no.. AB910001.. report must be-.41-card 'the' cur no all fliont operations. - . . The. above raentiOnedinstal I ti on drawings Were D.E.R. approved. on:FAA Form eliciz dated J-22-91. midcdast Fie No. mp9loo26.'• .L.:...1a.4.,.insoection_requirements per Collins. AVR-101:Afcbortie Voice Retorder. . . ey..tem F.sintonante. Mantis! 523L0757754 -1i0t114. 15 Feb:. 196E 2nd • Ravi . , vi a i cn . . ‘ . . . - . ' • . ' . • , . . . .- • • .. _ _. A. Fat-form' the "Preflight - Functional Test" and the "Additional System Test" every 3(0 caiendarYdays as prescribed in' the manual... , _The weight .46.0 balance was .revised 5 .and an apprOPr4 Ate. entry 'was. made the aircraft.-records. • . . _ EFTA00278264

wl & US Osocerreenr asavoravomors evevraes mar asernemaavaren MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) INSTRUCTIONS: Print or type ail enures. See FAR 43.9. FAR 43 Appendix 8.-end AC43.9-1 (or subsequent revision thereof) for mat:Litton; and disbo%ition of Mis form This report is required by law (49 U.S.C.1421). aiitore to report can result in a civit penalty not to exceed S1.000 far aeon such vioiation (Section 901 Federal Aviation Act Ct 1958) Make Gulf stream Aerospace Serial No. Name (As shown on registration certificate( Ogden Management Services, Inc. AIRFRAME. PROPELLER • APPLIANCE A. Agency s Name anc Acoress Midcoast Aviation, - Inc. # 8 Archview Drive, Cahokia, IL 62206 G-1159B Nationality and Registration Mark N979RA Address (As snows on registration certificate( Westchester County Airport, Hgr D3 White Plains, New York 10604 3. For FAA Use Only 4. Unit Identification 15. 'type .f U.S. Certificate, Mectranc I Foresaw. Censlicare0 Methane: Certificates Atom'. Station , manufacture. I C. Certificate No CRS R03R822L O. I canny mat me repair ands or alteration mace to the unit l s) ibintilied in item 4 above and described on the reverse or attacnments nevem have been maoe in accoroance with me requirements at Part 43 ol me U.S. Federal Aviation Regulations and that me intormatton lurntsned herein is true and correct toUte best of cm/ knowieoge. January 24, 1991. . Approval torfietum Service Pursuant t0 the at:thorny given persons soecitied below; me unit identified in item A was inspected in the manner prescriber; by the Administrator of the Federal Aviation Administration and is QC APPROVED C REJECTED IFAA Fit. Stan=ros I }Inspector - ! • 'manufacturer • BY , . 1 I FAA Designee I x 'Repair Station Date of Approval or Remotion 1-24-91 . 1Ceniiicate or . Signature Autriorized inonnouai 1Designation No. _ey CRS R03R822L 1 e•C Cif., Sief . pate. . • • 4 EFTA00278265

F.-:4 ; f kw NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration ritual be Compatible with all previous alterations to assure continues Conk:trinity with the applicable airworthiness reotnietpents. 8. D•scnpuon of Wort Accomphistea . (h more :pith* rs mound. attach additional sheets. Identity with aircraft nationality and registration mark and dale work complitad.) . 1.0 ‘Instaned, a Sensor System Lt. VHF TV Antenna.VM 865-8282721 It 2.3 Lbs TSGNo. C37b and.C3Sb in accordance.wiin Midcoast Aviation, ine. structural drawing-.no. 02-139F005 s!T.V. Antenna • The data 4cr the aboVe.insial.lizion approved on FAA Ford) :8810-3 dated 1-24791 Midcoast AviE.tion..File No.; MCS10026.. • . 3.0>•ifiaight and balan•ze wai an pr oar ;Ay entry was :Ana aircraft recorc..s. - - Y. • 1.• I. A Olit tat i i 674 L.• ••• liar - hi •I tird ili.j; . • • . • EFTA00278266

I. • :i.y.e•••-, • yeeorqtzgSt.f O MAJOR Sr.,PAIR AND ALTERATION Form Approved OMB No. 2120-0020 • US Deoceirrem For FAA Use On!) or licriscorximn (Airframe, Powerplant, Propeller, or Appliance). haseeer eimemen e . ; • - . . .., . . mwne, ftm Off' Idenc ication 6 - 03 • - , . . INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 A ppendix 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 muff in a civil penalty not to exceed $1.000 for eachaisch violation (Section 901 Federal Aviation Act of 1958). Aircraft • Make . Guifstreara Aerospace • Model G-11598 ' 1. Serial No. • 151 . ! . ... , Nationality and Registration Mark N979RA • 2. Owner Name (As shown on registration emeriti:ate) Ogden Management Services; Inc.' . •. .. ... -. ••• - Address (As shown on registration certificate) • Westchester County Airport, Hgr D3 :White Plains, New York 10604 . , --:" 3. For FAA Use Only • • . . 1 4. Unit Identification S. Type Unit ' Make • • 1 Model Serial No: • . Repair Alteration . • AIRFRAME (As . .• • • described in Item 1 above) ~mow« " • • - •• . • • • • • X . . • POWERPLANT •• . , ' • • • PROPELLER • ,.- - .. _ . . • • _ TYpe .... - • •. ' APPLIANCE - • • Manufacturer _ • • _ _. ._____ _ _ s 6. Cant ormi Statement A. Agency's Name and Address • I B. Kind of Agency C. Certificate No. Midcoast Aviation, Inc. I I U.S. Certificated mechanic • . # 8 Archview Drive. I I Foreign Cen ditated Mechanic I • ' • ! 1 y Certificated Repair Station Cahokia, IL 62206 i • CRS R03R822L ' . - .-- . _ .. .. _ _.. • ... . . O I certify that the repair anctior alteration made to me unit(*) identified in item 4 above and described on the reverseor 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 . • - - . . . . _ • ..-January-•24 ; -•1993.: ."•-•-:- -- , :77.-.77 Signature f Authorized Individual " - - '..: .• Si.... - • ••••. •• • - • •• .. . T. Approval for Return To Service - ' • Pursuant to the authority given persons specified below, tne unit identified in item 4 was inspected in the manner prescnbed re the , 'i Administrator of the Federal Aviation Administration 'and is . EirAPPROVED O REJECTED ..._ "i FAA FltStandards I 4.--: ..__......___: _ -- • - 7 ' Manufacturer ,-----;.. k tpector . ... • .: ....1......-r..: ... -... - • .[Inspection Authorization . Other (Specify) -. - • - -- .• - ... • - - - - _ rt___ - - • ••• - - • • .. . FAA Designee ' 7 1 x - Repair Station Person Approved try Transport CanadiAinvonhoness Group . . '.. .,;.. . . . . Date al Approval or Fleteetipri •••••••: Certificate or , . Signature - of Authorized Individual . . . — - _ ..1 . ••- . -.•-t- • - - .• • ' --"?'. Designation No. .. . - - • ' 7..' - . - % • ::• •; .. • -- t1"--t : icitS R03R822L • %:... ..:•-•det.:1, il I .: • 1-24-91 • • • - ••-• • eP4Cei t i g 41 int* s,1,‘S;4' • • - . crt EFTA00278267

ee i 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 continues: •;:.:•`ormity with 'he applicable airworthiness requirements. • ..a.b...:: ' Ortserlption of Work Aoconfonthod (If more space is required, attach additional sheets. Identify will, afrcraft neonality and registration mark and date work completed.) Complied with' VertiCal Stabilizer COrrosion Inspection Special •InsPection Procedure No.- GSIP7RS71159.70001 and drawing and specifidations as fistedr •• • _ 1159CS .2p000 Tail Erection 1159CS' 20650 Front Beam Installation 7 Vertical Fin 115905 20051 Mid Beam Installation;- Vertical Fin - 115909 20052 Aft Beam Installation. _:=vertical Fin . 1159CS' 20074'Shear 'Deck Instillation .".;:115/CS•20154. Skin all ati On 7 Vertical :Fin Maintenance Manual - Flight Ccintror Ri:agino- Procedures .• SE 25400901 Standard Repair -Vertical Fin to Fuselage Attach Fitting . . • • . . • _ • - - • • • • EFTA00278268

r7 G V it. ..).:.C.1:2-ctd.••-•..:c.:••••:;1-1:;•- t.'404:::kval4T-rr: ••-'•-, • - FAA AIPCRAF CAMERA NO. -444O, .3j e us ck.,...tiner. of Trcnsporicrocn Federcd , • . ' 7 - . , - . . . . .. . • . ' — --- —'—'- ' MAJOR REPAIR AND ALTERATION - : (Airframe, Powerplant, Propeller, or Appliance) , Form Approved OMB No. 2120-0020 For FAA Use Only „ anon Actrrelstr Office Identification L52 5-(- ' 475;! 2C) INSTRUCTIONS: Print or type all entries. See FAIR 43.9, FAR 43 Appendix 8l end AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C.14211. Failure to report can result in a Civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act 01 1956)_ . -i • - ' - 1. Aircraft Make ' Culfe4tream Aerospace Model ' .G1159B Serial No. 151 ' Nationality and Registration Mark N979RA . 2. Owner Name (As shown on registration certificate) r Ogden Management Services, Inc. Address (As shown on registration certificate) Westchester County Airport, Hgr D-3 White Plains, New York 10604 3. For FAA Use Only • - . 1' 4. Unit Identification 5. Type Unit Make . Model Serial No. Repair Alteration AIRFRAME _ ..• .., - ..(As described in If= f above) ' - • X '......,. • POWERPLANT _.: • • • , . .. • rij I- - fr 77. -; 1 N hlt•I -1.2.Lt: ...: .. PROPELLER • . - •- . - 1A i ; ',3 T.:-., i i APPLIANCE Type , . • ' • . SR Fr:: n r las ••••• \e oser i / , ...1•• Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Midcoast Aviation, Inc. • #H8 Archview Drive St. Louis Downtown Parks Airport • U.S. Certificated Mechanic • CRS RO3R8221, X Foreign Certificated Mechanic • Certificated Repair Station ' Manufacturer . D. I certify that the repair and/or alteration made to the un't(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the US. Federal Aviation Regulations and that the information . _ furnished herein is true and correct to the best of my knowledge. Date •1 ., • • i — / A -ci 0 Signature of Authorized Individual • .......___ c . - 7. Approval for IR n To Service Pu Administrator BY suant to the authority given persons specified below, the unit iden died in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is jX. APPROVED 0 REJECTED FAA Fl t. Standards Inspector Manufacturer . inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport Canada Ainvoithiness Group Oate of Approval or Rejection A / ‘ — 7 c Certificate or Designation No. CRS R0311822L Signature of Authorized Individual " r 7 c - •Oe,i/i--"e2, FAA Form 337 it.ari • ... ,.... . . .. • • • ..-. • :: :‘..- • • --... -.ease - "..: , .. •4-1: . • ,a : . • ,. . .. • • . , . • .• (0 111'? 3?..ei i9 1.. .Z ee :AP 4112 .,..; irgt : ' ..."-iic .5;.;:rg..„ ;:a. :ci....„_.-2_,...,_-z,_:_;;;LI..;!..11:.......a.....z..,......_ _______ • • - .• te Sat EFTA00278269

•• . . 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. NOTICE B. Description A Wcsk ACCompllsped • (if more space is 70c:directs attach additional sheets. Wordily with aircraltnajimmilly and nrclstration mark and date work completed.) • . • . . , . _ 1.) Amend STC SA250BCE to activate the V Nay function of ,the Collins . EFIS-86C (14) System for operation at 18,000 feet and below. The amendment was in accordance with Midcoast Aviation, Inc. certification dcawing.list # AD890009 Rev. .C, and with' the following wiring diagram design change notices; No. 1159-06000-151=C1 'EFIS-86C (14) No. 1159-34010-151-B1 & 82 "MidcoastSwitching_Unitu Structural drawingno...0000087_1itev-...,11.!!§AUbelErISAnStallation", conduCted a fl I ght .test accordance. with'MideoaSt Aviation, Inc. Report Na. ASS90038. dated November. 27,' The above data was D.E.R. approved on FAA FOrm'S 8110-3 dated 27 • November' 1989 and 9-JanUary 1990, MidcOadt Aviation, Inc. file no. MC890114, MC890116 and MC900003. FAA approved Airplane Flight Manual Supplement dated 1-12-90 Rev. A is require0 when a Collins.EFIS-86C. (14) Electronic Flight Instrument System is initalled.' - 2.) Updated the No. 1 and .No. 2 flight.Directors in accordance with wiring diagram design-change notices n6.-1159—040107151A1 "No.1 Flight Dirdttor Mod" and no. 1159=04011-151-A1 "No. 2 Flight Director Mod". The .data was D.E.R. ' approved on FAA Form 8110-3 dated 27 November 1989, Midcoast Aviation, Inc. file no. MC890115. . No equipment changes were made, 'weight and ',Mance change was negligible. Additional Shecils Are'Attactied ' - ye • ' . . -: • r".-14:tri zt e . 4 - 5,4% ; p. • .;Liefaiep:. ...axe; •• • . • _ 741,4 , 4; j i • , • i • sr . , t- • • EFTA00278270

••• • .,_. . MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-0020 -For .usonani.,,,8 . Powerplant, Propeller, Appliance) FAA Use Only or troneaorsomin (Airframe, or -. ico.rvmarmnampri Arannwmeari • • Office Identification ,57, • Igien INSTRUCTIONS: Print or 'type all entries. See FAF143.9. FAR 43 Appendix El, andAC 43.9-1 (or s-uaseq,:ent revision thereof) for instructions and disposition of this form. This report Is required bylaw (49U.S.C. 1421). Failure to report can result in a civil penally not to exceed $1,000 for each such violation (Section. 901 Federal Aviation Act of 1958), • • 1. Aircraft Make • • . Gulfstream Aerospace ; Model ' • G-1159B Serial No. 151 • Nationality and Registration Mark N979RA . 2_ Owner Name (As shown on :hilts -what certificate; • . . . . .. -. . • • - ---- • • Ogden Management Services Inc. . - ,.. Address (As shown on registration certificate) • ' ' • • • Westchester County Airport, Hgr. D-3 White Plains,.New York 10604 ' 1. For FAA Use Only • • . • - . . . 4. Unit Identification • S. Type Unit Make . Model Serial No. Repair Alteration AIRFRAME e (As deftribed in Item 1 above) X POWERPLANT • • . , . . ' - PROPELLER _ APPLIANCE Type - Manufacturer 6. Conformity Statement A. Agency's Name and Address I B. Kind of Agency C. Certificate No. Midcoast Aviati.m, Inc. . • " u.s Cenificated Mechanic t4 a Archview Drive . . • • Fctreigil Certificated Mechanic I .8t. Loris Dbwntown Parks Airport ' X Certificated Repair Si111041 CRS-RO3R822L Cahokia, IT, 62206 ManufacEiner , D. I certify that the repair and/or alteration made to the un't(s) have been made in accordance with the requirements furnished herein is true and correct to the best of my identified in item 4 above and described on the reverse or attachmentshereto of Part 43 of the U.S. Federal Aviation Regulations and that the information c knowledge. Date . • 0" 1-16-90 Sionature of Authorized Indiyidual - 7. Approval fur lc ;turn To Service Pu suant to the authority given persons specified below. Administrator of the Federal Aviation Administration and the wit identified in item 4 was inspected in the manner prescribed by the is 0 APPROVED 0 REJECTED FAA Flit Standards Inspector Manufacturer Inspection Authorization Other (Speedy) BY FAA Designee x Repair Station Person App by Transport Canada Airworthiness Group • Date of Approval or Rejection x 1-16-90 Certificate or Designation No. CRS -RO3R822L Signature of Authorized Individual - t- - • _., •C/172-/v//1-6C, a .- re (--......e.--f-•-•,•-' FAA Form 337 (4-an r a k . ..• EFTA00278271

' • tr; • " NOTICE • We/gin: and balance or operating limitation chingei shell be entered inthe'apprOpiiate aircraft record. An alleratiortmust be compatible with all previous alterations to assurevontinued conformity with the applicable airworthiness requirements. ; • • DW Olin of Work Accomplished . • more space is required, attach additional insets. Identify alai airontli nationality and registration mark and date wore. completed.) • thardiedithcllual- Universal Navigation UNS-1A Multi-Sensor avigation•Systems V Nay to the Flight -Virectors and Autb Pilot Systein I . l: in accordance -With- wiring 'diagram- design. change notices # 1159-030S0- . - -.. : 151-1Ai "No: 1 Fl ight "Management System (ONS-1A). " • and # , 1159-03081-151- Al "No.... 2 Flight Mahagement System •(UNS1A1"..:-. The. data •was D.E.R. apprOved ant FAA Form 8110-3 .dated .27 November. ,89, • Midcoast Aviation, - Inc. ire no. 'MCS90115: •-' - -- . . . 7- ."- .. .---: --- • • • Opei-ation ' stir-1g' 6+. the system was performed-and, all functions- tested . normal: • .. . - . . , . -Pending FAA approval of the Fright Manual' Supplethent Report AM02589• -the aircraft-is pkacarded,t."Use -tf "the V•:Nav:-it prohibited below 18,000 •• feet PA - 3. i eiwipment was chiriged, weight and balance; chahtje is negligible. EFTA00278272

. . ea, . . . . . ' • . MAJOR REPAIR AND ALTERATION us Decarterien • isi soniciormon • .(Airirarrpe, Powerplant,Propeller,, Appilartce) rooms Ammon saivernvenen • : - . .. • .• Form Approve° •OMB No. 2120-0020 For FAA Use Only Office loentification .i3.5 745, c; _ . _ INSTRUCT IONS:Print or type ell entries-See FAR 43.g. FARO„" Apvenche a. sad AC 43.9.1 and disposition of thi s'l arm. This report is repaired by law (49 US:C. 1420. Failure to report " for earth such violation (Section 901 Federal Aviation Act of 1958). for subseouent revision thereof) for Instructions can result in e civil penalty not to exceed 51.000, 1. Alreraft Maze • . ' - Gulfstream Aeroscare - Model C-11.5211. Serial No. ' . • . 151 Nationality and Registration Mere . • 41979RA • 2. Owner Name (As sinner( on roussustson cartikale) Ogden Management Service, Inc.' , Adonis . . • ... NestchesterCounty White (As mown an antsualson cartillssio) Airport, Hgr D3 Plains, New York 10604 v . 3. For FAA Use Only ' . ' . - - ..--•.-- - - ... .. .. , ... -- • • • • • - • . . . • . • • . • • - • . -: Y. Unit Ideottrication . • S. Type • • Unit 'stake • • - • - . Model ' '. . ' Serial No. • Repair Alteration AIRFRAME • . . . described in Henri • . (As abovi • POWERPLANT • I • ,..,--r—,t . ..., `..:'‘ ..• . • ' PROPELLER . --- --rc c. ,. ..4.; , 1(t.,s... -5 t •::.-.;... t. .1999 . h — • • • . • • • APPLIANCE . Type . e- ...,. • 0. ,e.. • . .. - ••• 4•1?-•-• . ...,,AN.c., . -stri-7, . " • n..ger 1 t•ti, - . • Manutacturer - . - • - 6. Conlormity Statement ' ' ' . A. Aciency's Narrie and Address • '. - ' I e. Kind of AettnCY • I C. Certificate No. Midcoast Aviation, Inc. • It t ' 8 Archview Drive • St. Louis DowntoWn Parks.Ariport Cahokia. IL 67706 . I U.S. Centlioned Metnanie • . I CRS RO3R1322L I Felton Crime:wed mechanic x I Celli jested Repair Staten 1 manutschner • • D. t certify that the repairindior alteration matte to Ina unit(s) is:lentil ieci in item 4 above have been mace in accoroance with the reoutrements of Part 43 at the .US. Fecntrat furnished herein is true and correct to the oesibl my knowledge. end described on the reverse or attachments hereto Aviation Regulations end Gnat the information 1 " ' __,... ___. Date ' 0 Signature of Aulhonzed Individ 12-1-89 . I. . .2.44A-09 0 • • “,,-,--,;.---- - ' T. Approval for Return To Service -Pursuant Aominatrator SY to the auttiority'0,ven persons specified below. the unit ide.nlilied in item of the Federal Aviation Administration and is g APPROVED 0 REJECTED 4 was inspected in the manner prescribed by the FAA FR. Standards I 'mentor I Inspection Authorization • Other (Spicily) • I FAA Designee . I X RAtan:irlacI stati urer on I Person Approved by TranspOrt Canada Airworthiness Group Date of Approval or Refection. Certificate or Signature of Authorized Individual Designation No. ..:. .- . /) —7 — 9 ' . CRS Ft03882.2.L ..e...-mtin-ea, • emc- tv-r . - ' • • :, ...-.--....: . .: - ... . - --4... ... ..:1,...- -: -.4- •- - .. ,..- --. ..,:....sa - 4. . N 1 _....... ....; ..-% ..T...1. 1 .., ...r..-en . ••4.............. .r.4.;:....:-2:7?,asi..1.7i:Z .s{.ia...." .• • .. . dia.r iteeni C.::C • EFTA00278273

:1 fr • • i rfl, 1.: r'r; Si IiT :!;. rt t. r; ,-J 4 .. • r • FAA AIPCRAF REGI ST/a n CA) ERA NO. DATE: 446 NOTICE Weigh( and balance or pperatinq limitatidn changes shall oa entered in the appropriate aircraft teased. An alteration must be compatible with all previons alterations to assure continued conforinity with the applicable airworthiness requirements. . 8. Descnption of Work Acconiplistmet.. . lit more spactlie -required; altneh kediti0nal sheens. Idontily with aircraft itainthallt anOrigistration mar* and date work completed.) . . . • Instalied landing gear ncirn silence switches in the pilot's & co- pilot'S - control wheel! in accordance. WittiMidcoast Fliation, Inc. • --1)..E;.ki.+-a0proved wiring diagram # 1159,L20001-151 "Gear...fiorn Mgr. .The data".tie414Pproved on FAA Form 811'G-3 dated 11-27-89 Midcoast Aviation,. . , • • • .... _.- \ 2.) Updated SA2507CE Hones*ell: YC7-18778217 Laser..Reference System. • • - ReMbve.d a Collins Battery FVhisIT2th978--001 :and indtalledia Litton N Battery . - FIN 28002-001 and 100 Watt resistor..: in accordance with •\ . •Mi dEbast- Atiati ons- . ap Proved Wiring _diagram it .1.15970040-151 DUO it 441:.qtated 11-70-89 "IRS (_asor Re-f ) and striktural drawing 41 0000086- R.evision 93"-dated 11-27-89. The data .Was.. D.E.R. approved FAA Form B1103 dated 11-30189 Midcoast Aviatiohi •InC. File No, MC890118 ind- Plo890119. ....N. • • ; *-1b•O• • • . EFTA00278274

• • • e, . . ALTERATION • • Form Approved • OMB No. 2120-0920 . MAJOR REPAIR AND ate - For FAA Use Only (Airframe, Powerplant, Propeller, or Appliance) eiwww awns ' . Aiwnwinereeri • . Mos trientilicaticm-aTh T. 6Lz.s4. • .. • INSTRUCTIONS: Print or type sit entries-See FAR 43.9. PAR C Apre...rWits B. end AC43.94 itneubsettuent revision thereof) for Instructions and disposition of ibis tont. The: report is recurred try tow (49 US.C. I421). Failure to repon nit result Uncivil penally not to exceed 21.090 • for each such violation (Section 901 Peoeral Aviation Act of 1950). • . Mace Moire! • • Gulfstream AAerospace r--1 1 SqR --.... 1. Altera Serial Na Nobonality end Regtsuation Mont . \ • - 151' tslciliaPA • 2. Owner . Name (As :mown on repatralron cortibale '. Ogden Management 'Service, Inc. • • r .. • ACtansa (Aswan"? On rewsitairCin carliiscals) - . Westcheiter County Airport, Ngr D3 'White Plains, New York 10604 . . • - • • . 3. For FAA WM Only .4 ' . _ . ". • • • • . . -- . • • • • • • . .• . - . • - . i • • • • - 4: Unit Identification • S. Type • ' . Unit 14ake - — . M - • . . . Serial No. Repair Alteration • AIRFRAME ' -1As . - • described in nein 1 above/ • , . .. r-t • • . • ' POWERPLANT .i . ' .. - • .1 • • - .;.- 4-C, ' • • - -4" ...-.7. --2 7.'fil I SC... . ‘Er:-.L . . PROPELLER • 1° 89 •''' --i r -r. 6 • v H • 4 - 6' ../ - • "'''I • ...a. •'.'-_: c:r -NO a..4 . . . • I .. • APPLIANCE Type ••• \ felt -• 1 62. '74,--,.. ' * Manusasturv- . • 1, IM"---"-- - . ' 6. Conlormity Statement . . • - A. Apency's Narita and Address • . I B. Kind of Acenty I C. Certi irate No. Midcoast Aviation, Inc. . • I I us. Cerellicated Mecnanic : •• # 8 Archiyew Drive - I I Femme Certificated Meenanic • - St. Louis Downtwon Parke Arinort X I Ceralicand Renoir Station • . CRS R03R822L Cahokia r IL 62206 • • . I Manufacturer • D. I dertilv that the repair and/or itineration mace to tfte unitts) toentitied in item 4 above and described on the reverse or attaChments hereto have been mace in aCcorCianCe with the reouirements of Part 43 of the L'.S. Federal Aviation Regulations and that the information furnished herein is true and cisirectits tne pest tit my knowledge. Date • . ... 12-1—89 Signature of Authorized Instrvioual . . s _4:„...../.4.4., •o azr,...... ) . T. Approval for Return To Service • Pursuant to the authority liven persons soecilied below, the unil identified in item 4 was inspected in the manner prescribed by the Aominseator of the Federal Aviation Aomirustra hors and is • CC APPROVED 0 REJECTED _ ..._ ..... I FAA Flt.Stanovas , • ' . inspector Manufacturer inspecifors Authorization BY ___ I FAA Designee I (Repair Station Person Armored by tnoW, . ' x . • • • - !Caftan AsnvcrnluneSS &Otto Other (Specify) • Date of Approval or Refection . 7.'7Z - 7 - A f ,. CRS Certificate Or. Signature of Authorized Individual • • . , Designation, Na • . R03R822L ..-e-:-"7-7L..4-,--e a— t. A -.: .‘ r..... - We • : ...*:".",:TA4gt;C4 'AirtritC)1.24.Ci€kr‘;j4 EFTA00278275

• • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft recrad. 4n alteration must be compatible with all Previous alterations to assure continued conformity with the applicable airworthiness requirements. DescreRtion of work Acccrelisffird— 1 1 - - (llmorespace alb* additionoliheatildintily withairaalinatonalgii*id ilaistration mark and date work comPlennt) • .. • 1.) (iptlyttg:STC # SA25DBCE dated76.H69:Collin'S S Tube- EFIS-86C (14) System tp. indorridiaier Verti,atal and lateral approach modes :from the UNS-1A Flight. Mandgement:.Systemito the" existing auto pilot and Fight . DireMtort. inaccordante with-MidoeSt Aviation,- Inc. D.E.R. approved prawing.Change7'MpticesT(DCWS)Itb7the folloWing. Witing diagrams, No. 1159"6:6000-151JRevision ."EYbdNALC-1 dated:117*TO "EFIS-86C (14) ", NO::Igt036804151'ReVision-"N/t"-DCN LA71,:date64:17-22-89 "No. 1 Flight managithenir cy-steM -(0NS-1)"*No61159:-'03081t.-151- ROVision "N/C" DCN 4 dated.:11*22A9J:"No,;7?2 Flight Manageinent'Syqtenr -CONS—lre s No.1159- 0010J15i keViiacin -aN/C"-DCW4- A-1.dated-112:7-891°No.1 Flight Director Abd" . NO.61.1596401±-1=4 ne%44fte."N/d".DCN-#- A-1 dated 11-22-89 "No. 2 Flight Pirect0c Mod" and No-Alt9.-7734010Mti-Revision.:"A" DCN # B-1 dated 11-22-89 "Midcoast.B-vadirni7Uhit" andiSti'uctural-D6E.R6'approved drawing 41 0000087 RWIiibh-n5wThated'fri-27±89 "5-Tube EFIS Installa— tiOn".....;Aflight, test of the System.was cOn-ducted'in accordance with MidCoast Aviation, inC.-Flight Testa A9890039. --t--. • • The abbve'clAtaHws D.E.R. -approved -On FAATobes 8110-3 dated 11-27-89 „Midcoast'Aviation.r Ine6%File'No. MC89011‘.:MC890115 and MC890116. . • 26) Pending aPprOVil of thehfghtliariiiar'Sdpiiiement the aircrraft is . placarded to'i-ead "'Use 04 the c/..NaV approan from:the UNST1A Flight ManageMentLSystem is not Approved": -3.) No eiaiiiMent'Ohahges%werEteade tthe weight change•is negligible. ..ettriirzawac;:-, - • A EFTA00278276

•• • • . .... .. - -- • • . • ' ' • I • • ' . - • • _ . . ._ ; '• • I' ' ' • - MAJOR REPAIR AND ALTERATION . . . us ueoarmeni.v ;,.ta,7;aiy, . !•,, -a , . ,.4-•,.:t., att:11411.1% a itrepartvoct•,z••.•.y.. (Airframe, Powerplant, Propeller, or Appliance) t‘tt,,,,-...ri:11/21, Ad rsir l ik = Ir. -,;1•:=4:it:.., .. .:y.:..:!: ....t. i•.;•:,:1:7.:40.-rzz.-:.:- r 1..7 7. :77. - t.`:!7" --;":? ...;;. ::1": ': r,.* s'kj.: Approved ''.•-•7 Form • * . . OMB No. 21200020 ,1!:.:L 3 • For FAA Use Only::' ,--4 Office Identification. • - -' — • - ...Sri .../e2et..: t:t.C.:.:.:. s INSTRUCTIONS:Print ditties ell entries. See PAR 43.9, FAR 43 ApPendlx B,'Iind AC 43.91 (oesubiaquent retslon thereob kir inetrualon's and disposition of this form. This report is requiredby4w (49 U.S.C:1421). Failure to report can rest:illIn ik civil penalty not to &tailed S1,000 . for each such violation (Section 901 Federal Aviation Act of 1953). 7 .. *: •• • - • • . . . • I 1 Aircraft , :.':• Make . . : . i GULFSTREAM AEROSPACE; *, ••.•• : 41 . 0. 1 Model ' . -. :if f *N -G7 11 B 1fli lVTh 7.-• • '. :9.is4:-9,1 Serial No: •• ' ., I .: -i7 i w - -. • , - • • 1.51.L.: €'. .: f, : Mationali and. Registration Mark Lail j ,.., . !, ,j ...1 979RA • . , 2. Owner,' I * . 11 i: . .. Name (As shown on registration Cartificetb) .! r[i.::!3::•, . :,. 3 • . _...._. • . . . . .. ' . • .:. jr•; • :.:• :1,1 Pit% ., III c:4‘). Lz: Ogden Matitietheil.fiSeticce,..-ttiC-P,) - Address (A.Isbowrrpn regiltratiarcertificate) , f. . - • •14-WeicliceSiii4 County.. ,lAirp'cirt t. 'Hgr. D3 ' •141Iird'illains, NY 10604 ' • • t •'-' :i ! i.,. . ' t 1. • i. • -; _.",,?1 f • :1 3.; For FAA Use °Myr. • I.; ? -• • ;;..-;'4 in : ti;: t • , ; g• I ; • 1 . . . ': ; ; • • r c ' I, '. ;'• •1• €' ' n b b O i ' • OW II ..-:-Jii i . anl :it :,.t :a 4....!...:44.11 ,:titu ii..:1; 3 I. ta:t. - s t ni. !.: n ;;:,611,1 ±11161155.vi ci, jr- MVI. Ilif.',.•6:.-thshiga.)E ;if. b:fi ct3 plied !:.i. f . %III; igi,ss. j •1.. : •,. (:: ,E:23.2S: .S:-,1•11:••ritur 5:h:info:Act:. ',ix :3:: ,"--.; i•-sa!;‘,1 0:-; is as -sub:J..O"H :sell' I . . •I• • • : -c,.• • t t •'; r:*re• He: 4 t•:-..rti • :: ••; : •1 ii:c trrtre.itn . . ITT tilt .; . ;I ' . •: : ".7::"A • , ; . r ' .• . 4. Will Identification-: i" I • ! . A I IA . •• : S. •Type :•5i i • ' • i; . . Unit ... _ _ • Make c • Model Serial No. Repair _ Alteration , AIRFRAME : : . . : (AS 'described in Item I above)' • i• _ • — • - X • I • . . • POWERPLANT , • -• 0 . V..9:- ii-l; •>, ..... ...•:., cc." • .,•9• z---_1. _sr ••-••• PROPELLER s APPLIANCE. . , • • ......)- • 1 r •,:••• ) • ‘,.-- • • t ._/- i AUG 23:1989 C— I —s ..,_ is . • • - - Type . .! - ..~ ' Af.' • . . :9 Manufacturer ' I I i • , . . ,.,--- EL Conformity Statement A. Agency's Name and Address -. • B. Kind of Agency C. Certificate No. , Midcoast Aviation, Inc. 8 Archview Drive Cahokia, IL 62206 • U.S. Certificated Mechanic - CRS R03R822L , Foreign Cereficated Mechanic X Certificated Repair Station Manufacturer 1 D. I Certify that the repair andkr 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 knowledge. Date ,' July 10, 1989 • '.. h Signature of Authorized Individu - • e, . , 7. Approval for Return To Service Pu Administrator BY suant to the authority given persons speCilied below; the unit identified in item 4 was inspected in the manner prescribed by the of the Federal AViation Administration and is (i5 APPROVED ' 0 REJECTED FAA Ell. Standards Inspector Manufacturer Inspection Authorization Other (Specify) - FAA Detignee L . . . Repair Station . • Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection . . • i ' • July 10,• 1989 Certificate or .• Designation No.: ' R03R822L •:: Signature of Authorized Individual r - . - EFTA00278277

• 0:.t:i'. • I Jr• NOTICE • : :.••• Weight and balance OrOperiting limitation changes shall be entered in the appropriate iiireratt record. An alteration must be compatible Witkallprevious alterations to assure continued conformity with the* applicable airworthiness requirements. S. Dosaiptlen of Wort Accomplished . . . . (If more spaoe Is required, attach additional enders. . Identify with aircraft national ty and registrittiOn mark and date work completed.) .•"' • - • -• - • • • , ••• Assembled and installed Cabin Seat Cushions for flame blocking 'per the.: et•••:;.114. following Midcoast Aviation, Inc. drawings. - : •• • • • • , . . • • .._ 1.) -0000115 2:) , 0000116 -• 3.) 01100117 __if.) 0080118 .E.) 0000119 Prdcluction •;Production“Seai*- Cabin Sirigles-". ‘: " ‘34' 5'1 • • i• , • Production,Seat - Cabin Singles ProduCtiont Seit - Cushion TW641ace , Divan . ; • ; :litr: Prodnction Seat_ 7.Cashion Three-Place Divan _ L .2 Test cushions, Midcoast Aviation, Inc.. part number 0000120; 0000121, and 0090122 were tested in accordanCe with FAktapproved Flame Blocking Teat Frpcedurei and -found to tie in compliance with 0./tiR. 25.853(c), • • ; , -• APPendix F, part.ii. Tests were conducted by Designated. Engineering. Representative, _Alien • b A`z-wroaszt--- Lzil ".---12.1."../1.* • 3/4. VC. . • 4 • - . e -•• 'Pet I e?t • : • • ;,•-••Ai • ar-4_ 1•••. ,I•Lt . " 3,15 7-.Y .:r3"‹ .:' •11.12 • €.11.:} Z•iia'rrak .g..S.Ri‘S..:47.5.71.4.1;1:. • • ; : “1. 6.1-.. • • • • . • r!'s • ••••• . • : I. . 7. . • :I. ' . • 4 1 • , 'nom' . . -"-- • •- ..• ••• • ••••••• •• ••• •••••••• A etZt •rri•Ir• rt ni!!: :: •!. • •{ah1ri 'a - nt i)• • - '04 r VI) 'OS? Ztri: •;1 1...°/tt ^ r'7; t':. t 5.11 • •:: CPO ---0;; • ; " i ; • -•• ;• . . . 411, 1-•:.;• •.• • ••••• i ••• • • .4. • ‘.4". 'Mies • stc.rs! • a •cie. EFTA00278278

f . • • • • - . , it it 4. . - . . UN:TED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE • 2 MANUFACTURER AND MOOEL L • AUTHORITY AND EPS S FOR ISSUANCE . ' This arwonhiness cent/Kate is issued pursuant to Mt FederalAvietco Act of 1993 andcendies that. as of the datebt *nature. the ' aircraft to which issued has been insisected and found to conform to the type ciptificebe therefor. to bean condition for sate operation. and has been shown to meet the reouiremems of the aPpiveable comprehensive and detailed eirworterness code as provided by Annex 8 to the Convention on Internabonei Civil Aviation excePt es noted Main . Exceptions TERMS AND CONDITIONS ' . , • • . Unless sooner surrendered. suspended. revolted. Of a terroonatiOn date is Olherwtte atatenaile by Pie' Administrator. Inn airworthiness certiricate is erreCwe as Ionia as the rownfenarce preventative maintenance:and StleratiOrtS are Performer/ in accordancewith Parts21. 43, and 91 of the FederstA • Request amwopnate. and Itienrcratt is registered in theUnited States. Any alteration, re2roduct.on. or misoso.ot ths Certificate may be punishable by a fine not exceeding St.CK10. or impasonment not eitteeding 3 years or both. M THIS CERTIFICATE UST BE 'DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAI, AVIATION REGULATIONS . ' • . • ,• . • . • . 3” ;7 j ..-S:71 .74' *el ' tirialliasa theitk..• Av- •- . ..2•6•37tv • •v• • • 1 v.:vb.:. .•." EFTA00278279

-FAA A 1 R DEAF REGI STET CAXERA DATE: • ....." ,emia7:4 • ••• • " i•al: P . • ". • • • • 4 :7.21.' .2 : 2.V: r 2CJ.S:212— elmja.m, •Z a.::•6;SL • • • • •• • EFTA00278280

• • . . :. - . . .... • • . . . - 1 • . • - • .. • • ---.. - • • -- MAJOR REPAIR AND.ALTERATION.: .. . : US Davanewre -. . . e s erA • et tomoomman • • - • • ippnranie, PTA/' erpIant, Propeller, or Ayptlarece) . t Peckseal seacien I • • ' Alanweernmen ' — - - - Form Approved , 0MB No. 2120-0020 • • For FAA the Only Owen Identification • • • . iii7) - FS" a INSTRUCTIONS:PrintOr type SI entnes.See FAR 43_9. FAA 43 Appendix S. and AC 4319-1 (or subsequent nvirislon thereof) for Instructions and disposition of Mil foam this report Ismouired by law (49 U.S.C. 14t21). Failure to report can result In-a civil penalty not to exceed 31.000 for each such violation (SeCtiOn 901 Fading' Aviation Act of 1958). - 1. Afrcra It Make . ' Guffstreamlsrosnace Model . - • -•G-1159B Serial No. . ' 151 - Nationality and Registration Mark i - N979R4 • .. 2- Owner • Name (As shown an registration certificate) - - - - - - - Ogden Management Service, inc.. _ . Address (As shown an registration send insta)' - - Westchester County. Airport, Hgr D3 White Plains, Niro York 10604 • . .•: -. • .. I. For FAA Use Only • . • . • . .. . . • . t.s. • _. . ' • — ..-. _. • - .: i• - . --- - --- .--- . . :, • ... • - e. Unlit Identification _ 3. Type - Unit __ .. - Make • • -- Model nil Serial No. ' • Repair Alteration . AIRFRAME • _. .. • (AS ._.c• . L- -_; _. . described In Item 1 above) __t 7 el . .V........•:: .- . ---- - • .-... • • . • X - • POWERPLANT • ' • .. • • . - -. ,- • . . -- ... -- - - - .. f.- -`<er:\ • - • PR0PFI t PR . - . - - • ;.' - • • .,- , .- • .. • ::-:•-•••:-etii:21j.-3.sa: es; : ..- I -1.- 261951 izki -:-. - - • . APPLIANCE . . . :•.i .4,1 , • : .sc3/44. ) - .. •4•... 32 .--:-..-_--t s- . ........ -"-Yrrg.59) . • -. . • •• Manufacturer I Conformity Statement • • A. Agency's Name and Address • B. Kind of Agency ' C. Certificate No. ' Midcoast Aviation, Inc. # 8 Archview Drive:". . • Cahokia, IL 62206 useettacated wocname _ • CRS R03R822L . Torsion Certincated Mechanic cardocowd Rwizir Stilton . Mantritacturer , O. 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 knowledge. . . - - _ . Date • , `"c- • 0, • -71/4/5) • 4. Signature of Authorized Indivi ....teh ztte, • • 7. Approval for Return To Service . Pursuant Administratorof • BY to the authority given persons specified below. the unit identified in item 4 was inspected in the manner prescribed by the the Federal Aviation Administrat;on and is . et APPROVED O REJECTED • FAA Ft Striindards Inspector Manufacturers , Other (Spectiy) Inspection Authorization ' - • • .. • FAA Designee - Repair Station X . Person Canada Transport Grcruo App u by Airvrarthiness Date of Approval or Reiection 4;77 Certificate or Designation No. CRS R03R822L Signature of Authorized Individual • • . - ..- • - / 7 ,---•4-- -- _,(- -- ---47 ••• • • _.•-e-liti'irz-92/1 . a .7 /f . , . • • . ' EFTA00278281

•. NOTICE' Weight and baleliceoropei*Ing antilidOn Changes Shall beenteied In the appiiprilite aircraft record. n alteration mt;st be compatible with all prgvious alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Oinception of Wont Aer.orne!Ished . . . _ . • . mars space is mmdriii.-ittsen additional idtatdvidentitturith.aircrail natkineety„spd registration mark and date work completed.) . . • . • INSTALLED A HONEYWd•L'YG17:82D LASER R&V.ENOE aysmm IN ACCORDANCE WITH.. -• f . STC #8A2507CE DATa - 7-6789e. THE SYSTEM CONSIST ;8F- THE FOLLOWING ;.• : 77.7-.:EclUIPPIENT; 7.17 -7%; • INERTIAL RE:001:S UNIT I . . • C.) IRS BATTERY 7- • _. - • P/N :1101.0:17!Ip04-••• • • S/N 499 . ........ P/N• 70089782-101 7 S/N KE5718' P/N 792-4978001. S/N 195 • ._ D. ) MODE SELECT UNIT - 7 rP/N• CBI:04241803 S/N 711 ., E. ) INERTIAL SYSTEM DISPLAY UNI : `P/N CG1:230AC10 S/N'.107' F. ) SWITCHING UNIT i59.#.;4o10 -1151 —.-S/N 151 PERFORMED A. FUNCTIONAL TEST (GROUND .& FLIGHT) OF THE SYSTEM AND ALL OPERATION OPERATED NORMAL* APPROVE? 0-161-677-fiAki.JAL- SUPPLEMENT -DATED 7-6-89, -'IS REQUIP.ED WHEN A • - • ..1::A-klONEYWP-.4.. LASERE= INERTIAL REFERENCE -SYSTEM IS INSTALLED - • ••• • . INSTALLED-A COLLINS 5 TUBE EF1S=§6C (arSYSTEM IN ACCORDANCE WITH STC # SA2508CE DATED 7-6-89 THE SYSTEM CONSIST OF THE FOLLOWING EQUIPMENT. $ • A.) DISPLAY CC NTROL PAWEL 622-9P65-002 -- SIN 115 & I32 -- (DCP-B5H) 2 EACH ) E=-ECTRONIG F1,-IGEIT DISPLAY P/N 62.2-6:42-024 . -- S/N -2078,2079, - . ' (E-D-86) .4 EACH ' •• 2101, 2102 , . . . - ) DISPLAY PROCESSOR UNIT.. . • IDPU-86R) 2 EACH • -' • D. ) MULTI .FUNCTION _PROCESSOR ?•.= • -- UNIT • F. ) SWITCHING UNIT 6. ) COURSE. HEADING PANEL - 2 EACH - •• r•-1O114.::071:.- • •J.0 ,1;; • • 1.1 .H. ) MULTI F4-NCTION-.DIFPLAX. . •• I.) LATE.RAL.AC OMSTER. ••• • (LAC-80) •• - • - 'L : J. ) Fgti 6 EALI-f • • ' *.•. _ . • .- . K. FIIME.1: Er EAt.. • . . L. S ROGRA,17.ER (RDP4300) - H0107511304-- S/N 499 •-• P/N 70080782-101 7 S/N KE.5718' •• P/N 792•4478001. SIN 195 *rP/N• CGi042ABOE • -;-1 S/N 711 CE1E30Ad10 S/N.107' `i7."0.1N-:115.934610-151 —.-S/N 151 ND.& FLIGHT)0F;THE SYSTEM AND ALL HEW -DATED 7-b-89,71S'REQUIRED WHEN A • -• SYSTEI IS INSTALLED' - • . . 6C '(143 SYSTEM IN ACCORDANCE WITH STC # CONSIST . OF THE FOLLOWING .EQUIPMENT; P/N 62Z-91'65-002 7-7 --SIN 115 & -132 • • F. * • ) . •• • • . .0 • . •••• =•.-••• - - _ - )CII=IFI'Ter, • . . •• • - j. _ _ - K. . . • .„ , L./ . . :-.•P/N H0107511304-- ,S/N 499 P/N• 700841762-101 7 S/N KE571E -'.P/N :792-6478001. SIN 195 !P/N• CG1:042ABO3* • •--1 S/N 711 .P/N C3.1230Ad10 S/N.107' •701N-115§t34610-151 —.-S/N 151 FLIGHT) OF; THE SYSTEM AND ALL • . • . . -DATED 7-6-89,"IS •REQUIP.ED WHEN A ct. -SYSTEM IS INSTALLED. . . • • C. '(143 SYSTE:`7 IN ACCORDANCE WITH STC # • i--- NSIST • OF THE FOLLOWING EQUIPMENT; • P/N 6ZZ-91%5-002 7-7- SiN 115 & -132 . • • u A .. P/N 6224342-024 7- S/N 2078,2079, -' , : 2101, 2102 . • • • . P/N 622-6342-024 7- S/N 2078,2079, - • : 2101, 2102 . • EFTA00278282

.Ogden Carp. .N979RA SIN 'SI PAGE 2 cf 2 2.) PERFrAMGD.A.FUNCTICNAL TEST (GROUND ANA LIG T CP:THE:SYSTEM, AN11 ALL OPERATION-OPERATED:NOGNiFIL. FAA APPROVED FLIGHT MANUAL SUPPLEMENT DATED 76-SC, IS'REMUIRED EFTS-86 (14) ELECTRONIC FLIGHT 'INSTRUMENT SYSTEN':E INSTALLED Z.) PRECISE FLIGHT, INC. SA2622NM, INSTALLED A PRECISE AiLSELITE' CONTRCL UNIT IN THE LANDING/TAXI LIGHT SYSTffM IN ACCORDANCE WITH PRECISE FLIGHT INGTALLAT:ON INSTRUCTIONS NC. PPRI-1000 REVIGtON it 7 DATA 2-15-ES .AND D.E.R. APPROVED. WIRING DIAGRAM 115.9:-08010-:51-40ULSE LIGHT SYSTEM". , PULSE LIGHTAONTRICL UNIT P/N 2400-25-4-4 S/R K00147. - 4.) THE AIRCRAFT WAS WEIGHED AND A NEW WEIGHT AND BALANCE WAS COMPUTED. THE EDUIPMENT LIST WAS SUPPLEMENTED, AND. AN APPROPRIATE ENTRY WAS MADE IN THE AIRCRAFT RECORDS. .. • EFTA00278283

%Agar: ::••••••••••=m• ; 4 . • • r. 4. e V:4 44. • • • .4.-gailk . . . • • • , . r:•••••: • ' EFTA00278284

- FAA AlFCFAft,REGiSTEY CAMERA NO. ,CD DATE: - • APPLICATION FOR • 0 r , es of atibOrtMon ' • • al • • • AIRWORTHINESS 0 AttnIristredlon . PedarciArlaffon CERTIFICATE . -. . ,. INSTRUCTIONS — Print or type. Do not write in shaded areas: these are for FAA . . use Only.. SubMit original only to an authorized FAA Representative. If aDditiOna I space 'IS required: use an attachment For special flight permiti complete sections II and VI or VII as applicable. ' • 1.1LEGISTRATION FAAR/t...,. . N9791A: . . 2AIRCAAFT BUILDERS NAME Wake, - - . .Gulfstream.- 3. AIRCRAFT MODEL DESIGNATION G-1159/3- • - ' 4. YIVIAFR 1974 FAA CODING 3960//0 1 I AIRCGI DESCRIP1 S. AIRCRAFT SERIAL NO ' 151 -: 6. ENGINE BUILDERS NAME r/Anei • Rolls4telyce Spey.. :.•• 7, ENGINE MODEL DESIGNATION ,. .:, RB511-8 • • • . 5Y5.22 3 & NUMBER OF ENGINES . 9. PROPELLER BUILDER'S NAME Wake I .-- 10. PROPELLER DESIGNATION II. AIRCRAFT IS I Check it aDPliCable 1 Two (2'•) .N/A . .: .. 1 IMPORT .. • II. CERTIFICATION REQUESTED APPLICATION IS HEREBY MADE FOR: (OW eta/shame dams) .. . - , ..._ . A 1 X STANDARD AIRWORTHINESS CERTIFICATE (Indicate category) I 'NORMAL I • I UTILITY I I ACROBATIC I X I TRANSPORT I 1 GLIDER I I BALLOON B t SPECIAL PIPWORTHINESS CERTIFICATE (ChesprarOPnate itemal . . C .. .... • 2 LIM:Tcr• • • . - " . • • - •• 1 CASS i 5 • • PROVISIONAL (ind•cela • • :Ansi .- 2. CLASSh • 1 AGRICULTURE . AND PEST CONTROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISING 3 RESTRICTED (IfidiCete be conducted) operahOreS) to -. a FOREST tWilable CenServabOni S PATROLLING 6 WEATHER CONTROL' • '7 CARRIAGE OF CARGO • 0 OTHER alsecifr) • . , 1 RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT 3 EXHIBITION ' EXPEFIIMENTAL;Mrstateo to be Condo:riot getatiari • - 4 RACING 6 CREW TRAINING ' MKT SURVEY ... 0 TO SHOW COMPLIANCE FAR - . 1 FERRY FLIGHT FOR REPAIRS. ALTERATIONS, MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT (Indicate 2 EVACUATE FROM AREA OF IMPENDING DANGER • B operation to ors conducted. Section VI then. • - - . or Was' "' -- - - • " '- 3 OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKE-OFF WEIGHT complete applicable on /erase:4er 4 DELIVERING OR EXPORT 1 51 1 PRODUCTION FLIGHT TESTING t . 6 CUSTOMER DEMONSTRATION FLIGHTS • C I_6 _I — MULTIP E AIRWORTHINESS CERTIFICATE (Check ABOVE -Restricted Operation-am( "Standard' or trintea. a applicable, ' A. REGISTERED OWNER (As shown on certificate of aircraft registration) ' IF DEALER. CHECK HERE I • III. OWNERS CERTIFICATION NAME OGDEN • MANAGEMENT SERILICESi INC. ADDRESS Westchester City Arpt., Hgr. D3 White Plains_ NY 106044. -- B. AIRCRAFT CERTIFICATION BASIS (Check appticable blocks and comp4le items as stelae ad) X AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE and Revision No.) AI2EA, Rev. DATA SHEET (Gore No - No. 17 X AIRWORTHINESS DIRECTIVES ,Check if all appticab:e AD's cerraneo with and give ..rear AO Nut 89-05-05 • AIRCRAFT LISTING (One page nun:balsa •1\ - ': X SUPPLEMENTAL TYPE CER; IF !CATE i List number of each S TC giros/30.4Na) See Attached List C. AIRCRAFT OPERATION ANC MAINTENANCE RECORDS' • ' . ...—. . . X CHECK IF RECORDS IN Fgantr 34CE WITH . TOTAL AIRFRAME HOURS : • -5684:33 •.- • 3 EXPERIMENTAL ONLY /Ellies bows flown since last co/hi:care issued Or renewed) • 15:20 • - D. CERTIFICATION — I hereby unify that I m the mg:stereo owner (or his agent) of um aircraft Administration in accordance with Section 50 of the Federal Aviation Ad of 1958.-and applicable airworthy and elrgible for the airworthiness cer iliaile retKiested:" • ' • " ' described above. that the aiic Federal Aviation Regulation . and all is regesteicd with the Federal Anal or that the social, has been .nspected and is v • DATE OF APPLICATION July 6, 1989 NAME AND TITLE (Punt or typo . . .. • . - . .. Agent- Carl E, Jones — - SIGNATUR 9 IV. INSPECTION AGENCY VERIFICATION A. THE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Complete ttr. , 011 only it FAR 2: Won applies! 2 FAR PART 121 OR 127 curruncgg joupEfit9snit Certificate No.) . 3 . CERTIFICATED Certificate/4i MECHANIC (Give • • 6 X CERTIFICATED REPAIR STATION (Give Cot:ace', , N" R03R822L 5 AIRCRAFT MANUFACTURER (Gus name of Mal . ... . . . __ - . ' DATE • E E• • • - • - July 6, 1989 ,Chief Inspector SIGNATURE 1-. - • - I V. FAA REPRESENTATIVE CERTIFICATION (Check ALL applicable blocks in items A and Bs ' fr efifE CERTIFICATE REQUESTED .A:1 find that the aircraft described in Section I or VII meets requirements for 4 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE B. Inspeclion fora special Marc penny under Section VII • - FAA INSPECTOR FAA DESIGNEE was cored sled by: . . . . . : . CERTIFICATE HOLDER UNDER. FAR 65 I I FAR 121. 127 or 1351 . 1 FAR 145 DATE 7 64 / DISTRICTOTHCE •:. • • grl--/TP() • 4 DESIGNEES SIGNATURE AND NO . . . .., • ' , . • 1 - - - . • -- FAA INSPE OR ... SIGNAT \ - A \4 , - 1/1 ...11 FAA FOND 81304 I11-881 SUPERSEDES PREVIOUS EDITION a.. • .•••• ..aral• ••••••••••••••••a.mm. ay • it EFTA00278285

• FAA AI. Cf.AY . NO, DATE: e. W O z Z p 2: I e.. 23 11h A. MANUFACTURER. 4 • NAME . 4 ' o• - . ' , . B. I. Pc 1DUCTION BASIS (Check apphcatsle arm) PRODUCTION CERTIFICATE (Gin driadUchlwr cettilicatt nu-stew) . TYPE CERTIFICATE ONLY APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTISRATES REQUIRED FOR OPERATING NEEDS DATE OF AFFIXATION - . . NAME AND TI (LE faint a cyan -- . SIGNATURE' 6- . - • . r . .. • I . s• • VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER MAN PRODUCTION FLIGHT TEST . . . / . . A. DESCRIPTION OF AIRCRAFT:: .- - - • B. RE3ISTEREO OWNER . • . - • ., . ....._ BUILDER (Make/ . • • .............. ... - . WIODEL • SERIAL DESCRIPTION NUMBER • - ... - .. . . „ • • - - :. _ ...... - REGISTRATION MARK_ . . . . OF FLIGHT - . CUSTOMER DEMONSTRATION FLIGHTS CI (Check it apatreata • si • FROM, - - , .. TO . ' ".. . . VIA • . • . :. . DEPARTURE DATE DURATION C. CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT . I PILOT I I CO-PILOT 1. • I NAVIGATOR 1 I OTHER apeeitis D. THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS cottows...- • .. .. . • .. . . , - - ... ., . . . ... _ .... . . . . • • r..- . . . .. , .. . . . • .. .. . - . . . . • . • -. . - - - : ' r::::"" "- tt5:.. • • . . - . .. . . - . _ .. . .... . . . .- . . . . .. . ." • - • • - . ... . _ . .. . s• , _. .. . .-. • - • • E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY FOR SAFE OPFAAT IOI./ Use attachment if necessary, - . . . .... . ., • • - . — . • . • 2 1 . •• • , . . _- : • • ' ..• - - • , _ ... - -• - .. .. . . .. .• . .. , . . . . . F. CERTIFICATION — I hereby caddy that I am Me registered aineitor hisagain of Me antra Oescribetiatiove: Mat the aircraft isiegistered wan the federal Aviation Adam:pd.-on in accordance NMI Sec-bon 501 of the f ears, Aviation Act of 1958. and avocet* Fears! Avtatiolit pegolitioni: andlhai the airCralltias been inspected and is airworthy to, ire night ascribe& .. .... . • .„. _ . .. . . .... , ... . . • DATE NA/AE ANC? TITLE /Print a type( . ' .. . - SIGNATURE , . VIII. AIRWORTHINESS DOCUMENTATION (FAA use only) A. Operating Limitations and Markings in Compliance miff FAR- • . . • . . 9131 as Applicable • . . . - - G. Statement of Conformity. FAA Form 9130-9 (Attach when required) H. Foram AM./ontoids Certification for hived Aircraft ; (Anted) ;heti iequired) • • " B. Current Operating Limitations Attached i t" . r 7 . -... ' - Data. Drawings. Photographs. etc. (Attach when requintd):_,••• i_ . .... - I. Previous Ainumhiless Certificate Issued in Accordance ith ' FAR . git I CI( CAR (Original Attached) . Current Weight and Balance Information Available in Aircraft . . . / E. Major Repair and Alteration- FAA Forin 337 (Attach Whin required) -.I. Current Airworthiness C.tertificate Issued in Accordance will • "FAsi 2 . 1 ' /51 3 (Copy attached) F. This Inspection Recorded in Aircraft Records -.... .• : . :. _ , , . 91: • • - . . . . . • • • : . . •••••••••aj•ito.t.74:-;" • , • • . . • • - . - • . - • ................... . ..... ..w..—.......... ............... .........................................—....—...................—...—........... .—...... .........s.........—..............1........,.... EFTA00278286

• ........••••••••••• FAA A1PCEAF CA!'ERA NO. SA2622NM SA2907SW SA722EA• SA1193SW SA1057SW . .SA1087SW SA1553SW SA1861SW . SA999SW • SA1918SW SA951SW SA2512WE SA1613SW - SA2507CE SA2508CE • . 7aL:a.•••4•4.2.. .;;.;• wad - ea. :.ra';‘Chi • . a c _ Tale S.C.D $465ft r : . • • • • EFTA00278287

1; C. .~ • I FAA A1FCFAF RE GI SIRE CAMERA NO. DATE: -711•1174 =74'er4+2'e • ••• • . .I; • . - - EFTA00278288

:EXPERIMENTAL AIRCRAFT OPERATING:LIMITATIOkS. • . , :iteieirch & Development, ShOWing:CoMpliance Withi .,.Regulations, Crew Training, Market Surveys REGISTRATION NO.:. Aicy ‘Ichtc)„,40 1. No person may operate this.pircraft'for other than the purpose(s) of .c.1,04,,yrD6 Ar.7-44'wefueg' (FAR 21.191), to accomplish tests outlined in the applicant's program letter dated g5,—.;1?-1V, describing compliance with FAR' 21.193(d). Additionally, this aircraft shall be operated in accordance With applicable air traffic and general operating rules of FAR 91, and.ell additional limitations herein prescribed under the provisions.of FAR - 2. All flights shall he conducted within the geographidal area described as follows: coistrbi g)r.,44., -2/4./rah .S7;47, . • 3. No operations, including takeoffs and landings, shall be conducted over densely populated areas. or. in'oongested-airwaysr.except those takeoffs and landings authorized as follows: A4.4 ACTIVE' ,4/A2.49,600e0175 "we ;e‘/.1)./z),4t 4.° Unless appropriately equipped for night and/or instrument flight in , 'accordance with FAR 91.33, this aircraft must be operated Day VFR only. •7.• 5. No perSon may be carried -in' the aircraft during flight unless that person is required for the pOrpose:of the flight, • 6. No person may operate-this' aircraft' for..Orrying persons or property for compensation or hire. ' 7. This aircraft shall contain the- Flight' Manual, markings and placards required by FAR 91.31. • 8. This aircraft is prohibited from aerobatic flight; that is, an intentional maneuver involVing am-abrUpt change in the aircraft's attitude, an abnormal 'attitude, or abnormal acceleration not necessary for normal flight. 9. The cognizant FAA Flight Standards District Offide must be notified and their response received'in'uriting prior to flying this'aircraft after incorporating a major thange:*defined by FAR Part 43, Appendix A. Post-IrbmndfaxtmnsmMalmemo7671 OofPagesi• -- IbMi ti 0Anc7L-46//arn: F 41C,Allar,......., Cr-elel ZDTMIA-S. ae/VAtAr;..— Dept y4014,7 c%/.:P--,?..5-—/vss--7 FaX 9Ya- 79 /y EFTA00278289

Page 2 of 2 10. The pilcitin.4cOmnand aircraft- ust,as aPplicable,hold'an appropriate tategory/clasS rating, have aneircraft type rating, have a flight instructor's lop43qo ndOrtement.or possess a "Letter of Authorization" issued by an FAA Fli Standards'DiStrict-Office or Air Carrier ()Orations Inspector: , ::•• 11. This aircraft shill's* be flown unless it is maintained and operated in accordance with apprOpriate military technical publiCatiOns, manufacturer's instructions, orTAkOpprove0 maintenance. program-for this aircraft. 12. If aircraft', engineor prOpeiler:OperetiOn.lImiXationi are exceeded, an appropriate entry will. b4umdeln the histOritai records. (Applicable only to Research and DevOziptient and ShoWing.COmgiance with Regulations.) . . . _ . 13. This aircraft-shall not be opeeated:for glider towing or parachute jumping operations.,.: 14. The aircraft shall bear the-Word "Experimental" near each entrance to the cabin or cockpit in accordance with FAR 45.23, . 15. Additional Operating Limitatiobt Wer/vi57 thci-M -SI 6- -LiAckOrti • . 6 — ,;.?—.F9 . - A"' C"--- ‘1 6, Date of Issue - Represent ive Designation/Office No. EFTA00278290

fa US of Ircrsoce federal Adahlr•hrrarlon ... . • • • - • , -.MAJOR REPAIR AND ALTERATION . . • . (Airframe, Powerplant, Propeller, or Appliance)-. - • Form Approved OMB No. 21213-0020 , For FAA Use Only Dti,‘_, hiut.4 Nation ?Marlon Office Identification 57/ "r5 006 ' . 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 of thilform. This report is required by law (49 U.S.C. 1421). Failure to report can result terra-civil penalty not to exceed $1.000 for each such violation (Section 901 Federal Aviation Act of 1958). - . . 1. Aircraft Make - Gulf stream Aerospace Model - G-1159B Serial No. ' 151 Nationality and Registration Mark N979RA • 2. Owner Name (As shown on registrelbifn outificale) , • - • - Ogden Management Service, Inc.. Address (As shown on registration certificate) Westchester County. Airport, Hgr D3 White Plains, New York 10604 • ' 3. For FAA Use Only " - • . - • : • - . • . . • . • . • • - ' 4. Unit IdentitIcation 5. Type Unit ' Make •I • . Model Serial No. _ .. Repair Alteration ' AIRFRAME • . (As _ described in Item 1 above) • - . . X • POWERPLANT • . • 14: ; . PROPELLER - ' . ' ' {.- RED1'1.1Ln ‘C.,S- • JUL 12 j939 p- rz-; - APPLIANCE Type • L 851- r s•J 7- e. I: 62 ' " 4 • Manufacturer - 6. Conformity statement - . A. Agency's Name and Address • . B. Kind of Aiency C. Certificate No. ' Midcoast Aviation, Inc. # 8 Archview Drive Cahokia, IL 62206 — U.S. Certificated Mechanic 5 CRS R03R822L Foreign Certilicatexl Mechanic X Certificated Repatr Station . Manufacturer D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirementi 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. nate • 7447 . Signature 61 Authorized Indivi .., 7. Approval Approval for Return To Service ; Pu Administratorof • BY auant to the authority given persons specified below. the unit identified in item 4 was inspected in the manner prescribed by the the Fecle.al Aviation Adminielration and is - 1:2 APPROVED 0 REJECTED FAA FIL Standards Inspector Manufacturer; • Inspection Authorization Other (Specify) • FAA Designee X Repair Station . Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 1;7, Certificate or Designation No. CRS RO3R822L Signature of Authorized Individual ' - ..-- --ediurt-ez ' 'C c.ecze..---47 • . • • •-• ••—••• 7.7-1••-..—;•• ••— • •••• •• . • . ' • . • • • • •--‘1` ...'..(3.1‘••••; Oa • ;St • Or EFTA00278291

• . • NOTICE -: • • . . . , . Weight and balance or operating limitation changes Shan be entered inthe appropriate aircraft record. An alteration must be compatible with all previoits alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work AccomPastsod . - . '(It more space is required. attach additional shaets.tdendly with.aircrali mamma* and registration mark and date work completed.) , . . . --. • . 1; ).-.• INSTALLED. A HONEYWELL.:yGiaze LASER' REFERENCE 1SYSTEt1 IN' ACCORDANCE WITH,: •' STC #SA2507CE DATED .7-6-89. nig SYSTEM CONSIST OF THE FOLLOWING EQUIPMENT D.) E.) F.) MODE SELECT UNIT -INERTIAL SYSTEM DISPLAY UNI SWITCHING UNIT' • P/N 'H61075A804. 7 S/N 499 P/N 70089782101 S/N KE5718 P/N 7926978001 S/N 195 P/N cp1042ABO I S/N 711 P/N:C4-1-B30C10 S/N:107 il5§7:340i0 1.51 • S/N 151' PERFORMED A FUNCTIONAI, TEST (GROUND. & FLIGHT). OF THE SYSTEM AND ALL OPERATION OPERATED NORMAL. FAA APPROVED FLIGHTLi.i46AU 661 6.1gliT DATED 77.6r89, 'IS 'REQUIRED WHEN A •HONEYWELL LASEREF. INERTIAL! REFERENCE. SYSTEM IS • INSTALLED: INSTALLED A COLLINS 5 TUBE EFIS-'86C: (14) :SYSTEM IN ACCORDANCE WITH SIC # SA2508CE DATED .7=6.,-139 THE' SYSTEM CONSIST '0F THE FOLLOWING EQUIPMENT; A.) DISPLAY CONTROL PANEL (DCP-85H) 2 .EACH: B.) ELECTRONIC FLIGHT DISPLAY (EFD-86).4 EACH • *C.) DISPLAY PROCESSOR~UNIT aPU-86R) 2 EACH • ' • F.) SWITCHING UNIT G.) COURSE! HEADING PANEL- L (CHP-86c) 2-EACH ---..--;•- MULTI FUNCTION .D1S?LY. A . (MFD-85B) ' " I.) LATERAL ACCELEROMETER P/N 622-9165-002 • S/N 115 & 132. P/N 622-6342-024 S/N 2078,2079 , - 2101, 2102 P/N 622-9009-001 S/N 2687 & 3512 •-- P/N .622-9010001 • P/N .:1159=34010-151" :• P/N 622-7875,-002 -• • P/N 2277876'-002 , . . P/N' 229-03240-020 J.) FAN 6.EACH. PiN 0o9-1963-.0::;0 K. FM-6.7, 6 EACH. • P/N 6t2-71Z-74-002 S/N 2203 S/N 151 S/N 130 & 131 S/N f645 S/N 363 NONE L.I REMOTE 'RCGRAMMER (RDP-:,..00) P/N 622-5110-001 S'N 2081 EFTA00278292

• FAA A1RCPAF5REGISTRT CAMERA NO. DATE: t. . _ . ..„. Oaden Corp. N979RA SIN 151 7-6-89 - Pape 2 of 3 (Continued):. . 5.) The previously installed Dual ColIinsTDR-90 Transponder System control was changed froth a Gables to a Collins CTL-92 ATC control with A CAD-62 control-adapter. This control. head and adapter unit is an approved control device for the Dual Collins TDR-90 TransponderSysteM. No changes were made to the Transponder antenna's. The operatiOn of the Transponder system was.ground and flight checked and all operations were normal. Midcoast Aviation, Inc. D.E.R. approved wiring Aiagram 1159-11000-151 "Transponder Control (CTL-92T" reflects the aircraft.wiring. ' 6.) Removed a Bendix RDR-1200 Radar Systemr, radar indicator, RI' unit and radar antenna and installed a Collins Radar Antenna RT Unit and WXP-B50A & WXP-850BWeather Radar Panels. Operation of the syStem was ground and flight,checked.in.accordance with.manufacture.s.maintenance manual and. all operations-were found to be normal, completed in flight radar stabilization procedure. Midcoast Aviation, Inc. D.E.R. approved wiring diagram 1159-14010-'151 "Radar (TWR-850)" reflects the aircraft wiring and D.E.R. approved structural. drawing shows the installation of the antenna RT Unit, 0000088 "RTA-858 Antenna Ihitailation". 7.). Installed a Collins Air Data Computer ADC-80H‘DaDc, ADA-85 ADC adapter and TAI-80A TAS/TEMP indicator, using the existing temp probe. The computer is mounted•to a hat section pap with -flat plates and the hat section is mounted with AN bolts to radio rack.shelf using existing inserts. The hat section is manufactured from .063 2024T3 aluminum installation in accordance with AC 43.13-24 Chapter 2 paragraph 25, Midcoast Aviation, Inc. D.E.R. approved wiring diagram 1159-04040-151 "No; 3 Air Data computer" reflects the aircraft wiring. Operational • testing of the system was performed and.all function testing normal. 8.) Installed a cabin audio/video/stereo/airshow system. Cabin depressurization protection is provided for by a 10,000 foot pneumatic disconnect switch. The system is installed as a non-required system and . has been tested to assure no EMI with required avionic systems,. Midcoast Aviation, Inc. D.E.R. approved wiring diagram 1159-21010-151 "Cabin Entertainment" 1159-21011-151 Airshow reflects the aircraft wiring, and. D.E.R. approved structural drawings 0000133 "5 inch pop-up TV installation" 0000134 "TV and VCR" installation 0000135 "SFS 3068 inverter and M10600 audio amp installation" and AC 43-13-2A reflects the structural installation. 9.) The galley was rewUrked to add a microwave oven, inverter, and coffee - maker. These items were testVfor EMI and proper operation and found to be normal. Midcoast AViation, Inc. 1LE.R. approved wiring diagrams 1159-:- 30001-151 "Microwave OVen", 1159-30010-151 ,"Galley" and AEC 151-2 "Coffee Maker" and D.E.R. approved structural drawings 0000132 "microwave oven installation", 0000136 "SPH 1606E-3" inverter installation - R/H galley. ""••--'w."` - EFTA00278293

• (Gontinued)1/2 Ooden Corp. N979RA S/N151 7-6-89 Page 3 of 3 10,) •Instaliad -a IRS'/TRU gel ct annunciator sWitch This was an existing 4Sature- that•was molt+ .to use another navigation souree. The switches" installed on the pilot'. rand co-pilot's switch panel. IRS/TRU selact . , gives a magnetic headi when deselected or a true heading when selected..In the selacted position the annunciator is lit (IRS Mode).. Installed a ATT/ADG-select annunciator switch on the pilots and co— pilots switch panel. The pilots switch when not lighted is in the INS source tprimaryle and when lighted comes-from the AS 1 VG and # 1 DG .source, (Secondary); The co—pilot switch when not lighted comes from the #,2 VG and # 2 .DG scarce (primary), •and when lighted comes from the INS source (secondary). The operation of the switches were ground and flight tested and +dung to operate normali:Midcoatt Aviation, Inc. D.E.S. apprOved wiring diagrams, 1159-20007.151 "Instrument Panel & Annunciator Mod", 1159,-3260o-151 "CompasS Transfer Mod" and 1159-35000-151 "Altitude Transfer Mod" reflects the aircra:ft Wiring. • 11.) Installed.a. cabin 60 HZ AC Syste0 Inverter P/N SPS 1307 S/N 440 in accordance with Midcoast Aviation; inc: D.E.R. approved wiring AED 151,4 and mounting in accordance with AC't1L-1.32A.; Installed a B&D Instrument'Air Data Computer (# 4 ADC) P/N 2800A-041 S/N A01023 and Rosemount Probe P/N 129H S/N 74498.. to interface with the UNS- 1 Flight Management System, IRS (Laser Ref),•pilat's ALTM & ALT Data System, ALT Select-& Alert System: Operational testing of the system was performed (ground and flight testing) and all function tested normal. .Midcoast Aviation, Int.'D.E.R.7approved wiring diagram # 1159-04041-151 "No. 4 Air Data Computer" reflectS the. aircraft wiring. Ii,stallation of the Air Data Computer installed in the forward radio rack in accordance with AC 43.13-2A. The aircraft was weighed and a new weight and balance was computed. The equipment list was supplemented. and an appropriate entry was rude in the aircraft records. -----END - EFTA00278294

fr: f-d-1 • ' . . ,• -FAA A1PCRAT REGISTRY CAmERA ND. DATE: . .. e • . - . . • . ••• ...." MAJOR REPAIR AND.ALTERATION • - • : • • - in Deco-al-erg ., of kcersoomarron • 1 (Airframe, Powerplant, Propeller, or Appliance) . . .. Federal A..Union Adrrinl oration . • - Form Approved OMB No. 2129-0020 • For FAA Use Only Office Identification Sri - - ,S.60 ... 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 !arm. This report Is required by law (49U.S.O.1421). Failure to report can result irra civil penalty not to exceed 11,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1 Aircraft . Make . Gulf stream Aerospace Model C-1159H Serial No. -- - 151 • Nationality and Registration Mark N979RA 2. Owner • Name (As shown on registration certificate) Ogden Management Service, Inc. Address (As shown on registration ConiliCa(0)• .• ' - Westchester County Airport, Hgr D3 White Plains, New York 10604 • 3. For FAA Use Only • - . . • . • • ' a. Unit Identification 5. Type Unit Make • ' Model Serial No. Repair Alteration AIRFRAME . (As described in Item 1 above) I - .... POWERPLANT - . \., 1 WI / . . ,,,---., .. :., .42 . , :•.-;:, •'..7., .___ s? . • . PROPELLER t t•-• S—I '.;:-• "IQ 12 798 n 9 r_ SILL E;300 •.-7.7,r APPUANCE - Type . Kr - 62 -..._ I . - Manufacturer - 6. Conformity Statement A. Agency's Name and Address . B. Kind of Agency • C. Certificate No. Midcoast Aviation, Inc. • ≥f 6 Archview Drive Cahokia, IL 62206 _ U.S. Certificated Mechanic CRS .R03R822L Foreign Certificated Mechanic X Certirrcatee Reaair Station manufacture D. I certify that the repair and/or alteration made to the un't(s) identified in item 4 above and described on the . have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations furnished herein is true and correct to the best of my knowledge. reverse or attachments hereto and that the information Date •... ... 71 47 if 49 - Signature dl Authorized Individu .2-Cita/L-e- - Lie,./k/frr-cre --- . 7. Approval for Return To Service Pursuant Administratorof • BY to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the the Federal Aviation Administration and is . "KAPPROVED O REJECTED • FAA FIL Standards Inspector Manufacturer! • Inspection Authorization Other (Specify) - FAA Designee X . Repair Station . Person Approved try Transport Canada Airworthiness Group Date of Approval 7/o/677 or Rejection . • Certificate or Designation No. CRS R03R822L Signal of Authorized Individual vvirLiet : a: C.- INtesfidarrarefeett. EFTA00278295

. . NOTICE Weight and balance or operating limitation changes shall be entered inettle appropriate aircraft record. An alteration mus▪ t be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Aceomplished • . . more space is required. attach additional sheets. Identity svith aircralt nationality and registration mark and date work completed.) • .:. 1.) The Dual Collins VHF-20B System was removed and replaced with Dual • -/- Collins VHF 22A System, The•VHFi22A radios are'TSO'D replacement for the VHF-20's. Form, fit and fUnctAblieremain the same. New control heads .displaying diagnostibefunctions'are installed with new radios. Weight, power consumption, performance, iand reliability are improved with the VHF 22A. The antenna was not.changed therefore,ftight testing of the system is not required: Operatiohal -testing. Of the syttem was performed and all functions tested norMaL_Midcoast Aviation,- Inc. D:E.R. approved wiring: diagrams 1159-fd010-15l_No.. 1 VHF CommuhiCatitii (VHF-22B) and 1159- . 10.011-151, No. 2 VHF Communicatiom (VHF-22B) reflects the aircraft wiring. . , 2.) Updated- the Dual Collins-VIR-30A'S to' Collins VIR-,32's. The VIR-32 radios -are physically and -functionally interchangeable. The -weight, power • consumption, and,reliability of the navigatkon.system has not been • degraded. No. antenna changes were Made.thereforeAlight testing of the' installed antenna -radiation patterns were not -necessary. The control • • .heads for the'navigation system were changed from Gables control heads to Collins CTL-32.Contred-heads. System operation was ground and flight • checked and all operations were normal. Midcoast Aviation, Inc. D.E.R. . Approved wiring diagrams 1159-03610-151TNo. 1 Navigation System (VIR-32) and 1159-03011-151, No. 2 Navigation System (VIR-32) reflects the aircraft wiring. 3,..) Updated the Dual'Collins DME-40's to Collins DME-42's. The DME-42 radios . are.physicatly and functionally interchangeable: The weight, power • consumption and reliability of-the DME radio System had not been degraded. No antenna changes were made and therefore flight testing -of the installed antenna radiation patterns were not necessary. The control heads for the DME System are the control heads of the VHF navigation - System. Operation was ground and flight checked all bperations were normal. Midcoait'Aviation, Inc;D:E.R. approved wiring diagrams 1159- L3000-151 No. 1 DME (DME-42) and 1159-13001-1511 No. 2 DME (DME-42) reflects the aircraft- wiring. . . 40. RemovedaGablea-ADF:cOhtrol head, 4 each•ADF receiyers and 2 each ADF . antennas and ceplaced with,a Collins CTL-62 control head, 2 each CAD-62 control adapter. units..ind. 1 each Dual .ANT608 ADF antenna. This control - head adapter ilia aria antenna is an approved control' device for the Collins ADF-60 system. The operation. of, the ADF system was ground and - flight checked and all operations were normal. Midcoast Aviation, inc. D.E.R. approved wiring diagram 1159-'12000-151 Dual ADF (ADF-60) reflects the aircraft wiring. The -Dual 4DF antenna was installed in the existing: mounting of removed antenna. , . • • . I EFTA00278296

Ogden Corp. N979RA . S/N*151 .• PAGE 2 of 2 (Continued)2 , _ PERFORMED A FUNCTIONAL TEST (GROUND AND FLIGHT) OF,THE SYSTEM. AND - ALL OPERATION OPERATED NORMAL. FAA APPROVED. FLIGHT MANUAL SUPPLEMENT DATED 7-6-B4, IS REQUIRED WHEN .A EFIS-86 (l4)' ELECTRONIC FLIGHT INSTRUMENT SYSTEM'IS •INSTALLED. ' - PRECISE FLIGHT, INC. STC # SA2622NM, INSTALLED A PRECISE PULSELITE CONTROL UNIT IN THE 6ANDING/TAXI LIGHT SYSTEMIN- ACCORDANCE WITH PRECISE FLIGHT INSTALLATION INSTRUCTIONS NO. PPRI-1000 REVISION it 7 DATED 2-15-BB AND G.E.R. APPROVED WIRING DIAGRAM 11.59-0800715t "PULSE LIGHT SYSTEM" PULSE LIGHT CONTROL UNIT P/N.2400-25-4-4 S7NK00147. THE AIRCRAFT WAS` WEIGHED AND ANEW WEIGHT AND BALANCE WAS COMPUTED..- THE EQUIPMENT LIST WAS SUPPLEMENTED,:AND•AN APPROPRIATE ENTRY _WAS MADE IN THE AIRCRAFT RECORDS. . - • - ^ . • . . . . • t '•-•••••' .• • .. •• • ' EFTA00278297

- -"I • 71 • sf•-r :. . • -• " e n ! • , ;-...4:'• .g • 'OM Y314.13 AVIS i1311 IV:13dIV YY3 - yi EFTA00278298

e - • -.-: .:: .i. - .. : - REPAIR ANDALTERATION ' ' -.... .:; : :: - MAJOR US Dem:men -. - 3 - . ix konsponoion (Airframe, Powerplant, Prcpeller, or Appliance) ; . - Federal Aviation ' • Actinktfrarkin . • ' .. • - • Form Approved OMB No. 2120-0020 • • For FAA Use .Only Office Identification " 571-frice :' • INSTRUCTIONS: F4in iser type all entries. See FAR 43.9;FAR 43 AppendixO, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of thii form. This report lsreqUired by law (49 U.S.C. 1421). Failure to report Can result !ma civil penalty not to exceed $1,000 for each such violation (Sectibp 901 Federal Aviation Act of 1958).. . • . 1: Aircraft Make . ,. GULFSTREAM SPACE Model ' • . . G713.59B " Serial- No. '• • ., . 153; . . Nationality and Registration Mark N979RA , 2. Owner . Name (As shown on registration certilkate) , Ogden Management Service,••InC.--• • . Address (As shown on registration certilicate)• Westchester County Airport, Hgr 1D3 ' ' White Plains, New _York 10604 • . P "-.'i"..3 silerAfinn irishrifed hero n “ les Inflic•W Cke-efslY••••: • • •. • . , -:n:.:tric-f co ax:iy,oritiiness requirements and is approved:for tircraft, sub;ect to conformity inspection ic!.FAR Part 43, Section 43.7." ..sari.- Fsbo 77-iff ".• the above. cif):...:::@—• by a person autliazi..,:). . gi.bf 8 ,4a , . • / 445MaA vr 704/ / 5 • CO/HP.947R be tVirli Pii6Nr— MAIL/tent- 5 &few-to-sr: PAA• • . 6,4 roverte.v4 A t. nte..b. , ... . (Wit°. Dato InspectiO 17M- 4. Unit IdenlIfIcallan S. Type • Unit • Make ..• • • Model • 2.i• - • • Serial No. Repair' Alteration ' AIRFRAME . •• • - (As described in Item 1 abovd) . . • . . ' POWERPLANT' • ' " . . . 1 • ' • • . • ' ' - ' _.• PROPELLER . ' • . . • • •• . • ' . • . . APPLIANCE Type . • . . ,7-• • • • Manufacturer e: Conformly Statement A. Agency's Name and Address . . B. Kind cl Agency C. Certificate No. Midcoast Aviation, Inc. • #8 Archviebi- Drive St. LoUis Downtown-Parks Airport Cahokia. IL 62206 .. U.S. Certificated Mechanic - • . . CRS R03R822L Foreign Certificated Mechanic .t•-• X CerillicalTed RePeir Station . .. Masiulacturer . D. I certify that the repair and/or alteration made to the un t(s) denti lied in item 4 above and described on the ieverse or attachmedi hereto 'have been made in accordanCe with the requinimenti of Part 43 of the U.S. Federal Aviation Regulations end that the information furnished herein is true and correct to the best of my knowledge: Date . .: June. 30, 1989 • • Signe tuft 61 Authorized Individual ' )d.Z440-a a „142,„. __ . I .. T. Apploval for Helium To Service • • . Pu Administratortl • BY • . . ,i • avant to the authority given persons specified below.; !ha unit identified in item 4 was inspected in the manner prescribed by the ' the Federal Aviation Adminiitrition and i3 . a APPROVED 0 REJECTED • FAA Fit. Standards Inspector Manufacturer! • ., insCection Authorization Other (Specify) • • - • ‘ • • • ' * ' , • FAA Designee X Repair Station ; Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection . ' . June 30, 1989 Certificate or Designation No. R03R822L Signature of Authorized Individual • • ' • ' . . . _ ' •••,• ft-p- ;• "- . . . . • •- „...r• • -; . knarei 4itle ; f•-•, ' EFTA00278299

P. - FAA .AIRCF.AFLREGISTET CAMERA 140. DATE: rt 3 . . *NOTICE . . .Weight and balance' or bpereling limitatiorpthanges shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conforenity, with the applicable airworthiness requirements. a. Description of Work Accomplished more space is required, attach additional sheets. Identity with aircraft nationality and reels:ration mark and date work completed.) . . :Installed a Dual .Univarsal givigatimn UNS-1A•Mufti-Sensor Navigation System. The system was installpd and approved. in atcordance with AC- • '20L130 dated- 9-1"-es, & Ac.:43-12-2A- for the mounting of the equipment. See Midcoast AviatiOnt _Inc. Ccimpliance•Report: AC890006, dated 6-30-89. Operation testing of thee system was perfornied and :all functions tested normal. • 7 • FAA approved Flight Manual. Supplement dated 7-&-g9 is a UNS-1 MultiLSenior Navigation System is. installed: The equipment list was supplemented and the aircraft was weighed and a new weight ,and- balance was - coinputed s .-an appropriate entry was made in the aircraft records: - • The Flight Kanuai. cOmOatijile with aircraft. -eft' n- • t .;., a itei• • EFTA00278300

ti• • '1 •11. 'co • • t : . r -• • ' Milliattraft • . . _ I ' ' • • . ' — • • , -. . ' •• • • • MAJOR REPAIR AND.ALTERATION ' • ' •.; • k u:oeoormw+ .. • oftnycnomn (Airframe, Powerplanli Propeller; or Appliance) ..:. Federal /Marlon ' . Adrninktrarion .- .. . . .. _ ' " Form Approved OMB No. 2120-0020 • . • For FAA Use Only Office Identification Cil : fi Stin • • INSTRUCTIONS .Printor type all entrles.Sed FAR 43.9, FAR 43Appendix El. and AC 43.9-1 (or subsequent revision thereof) foe InstructIons and disposition of this form. This report is required by law (49 U.S.C.14292.Failiare to report can result bra civil penalty notto exceed $1.000 for each such violation (Section 901 Federal Aviation Act of 1958). ; ' ' • 1. Aircraft Make ' - -• . -GOLFSTREAM AEROSPACE - Model ' .• • • il, ' . G-1159B Serial No.• - ' .1. 1 • • :. Nationality and Registration Mark . - N979RA . 2. Owner • • Name (As shown on registration certificate) • , . • . Ogden Management Service, Inc. Address (As shown on registration certilicate)• .Westchegter County Airport, Hgr D3 White Plains, New -York 10604 - • . • . 3. For OAA Use Only • • • . . • • .- . • • . - - • • . . . • • ' i .. • " • • ; 1 . • • - • 4. Unit IdenUfloatIon • S. Type • Unit Make - -. - Model • ;:: Serial No. Repair Alteration ,.. - AIRFRAME - - • ' • ' . ' • (As described .- ' in Item 1 above) : • • - • . :;.„ • . ' PoWEFIPLANT . - • - . • . . • 4 . Ite• Q ta • . bb• 4 <13' firclifill --:-. • • • • PROPELLER • • - ' . • 12 1989 c- MOO' • `Hi ITI‘ APPLIANCE Type . • • .\ . . 62: • . • i ' . , • ' • • Manufacturer . . ll Conformity Statement A. Agency's Name and Address • . B. Kind of Agency ' C. Certificate No. • Midcoast Aviation, Inc.. • #8 Achview Drive St. Louis Downtown-Parks. Airport Cahokia. IL 62206 ....- U.S. Certificated Mechanic • CRS R03R822L Foreign Cenificaled Mechanic X Cerilfirsaied Fleriair Station . ' Manulacturer . . D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date . . . • Juhe 30, 1989. .. Signatu e of AuthorizedIndividu - • • . -tact/t4 :• 0 "..e12,104 --- • •. ... • . , T. Ap • royal for Return To Service . • i Pursuant Adminiatratorof • BY .. • to the authority given persons specified below. the unit identified in item 4 was inspected In the manner prescribed by. the. ' the Federal Aviation Administration and is . tit APPROVED O REJECTED • FAA Flt. Standards Inspector Manufacturer. • • Inspection Authorization Other (Specify) ' . , _ • - . ' • . • FAA Designee x. Repair Station . Person Approved by Transport Canada Airworthiness Group .. Date of Approval or Rejection . • " June 30 , 1989 Certificate or Designation No. RO3R822L . ' Signature of Authorized or. Individual . . • .. / pm ,Z, ..„4.• .-•: 4; 7 i fi r LI . /....4.57f.eirtel../ • •i.- ' • • - • _ • ; • - • • • • • — t -`-'21%. • • EFTA00278301

-FAA AIPCRAISRFCTSTILT CAXERA NO. DATE: - --A-fraste . 4 .. . . NOTICE Weight and balancebr 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 file applicable airworthiness requirements. • B. Description of Work Accomplished '(!f more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) • -•• il 4t4:40.:‘,..., • ' •,- . • -4br•-**-7 • .. • • • • . • . . • • . • ft.) Installed a Dual-Universal Navigation UNS-1A:Multi-Sensor Navigation . •Sistem. The systeeWas initarted -and*Approved'inaCcordance with AC- ' 20-136 dated.9,42-68, 4 ACA,3-12-2A for theMounting.of the equipment. See MidcOast AviatiOn;:InC.-.-COMplipnce Report-AC840006, dated 6-30-89. • - . Operation teating,of.,theisyttem was performed:and-all functions tested normal. 2..) • Pending FAA approval of the Flight.ManUal.Supplemento-NavigatiOn shall • not be predicated upon the Use 64 the Univertal Navigation UNS-1A • .• Flight Management System. Aircraft has been placarded._ 3.) The equipment.11St was_suppIemented and the aircraft was weighed and a new weight and balance was cOMpUtad,jan appropriate entry was made in the aircraft records. ••• • • . END • • • . . . • . , • . • J . • %a ...;;;I‘rrAtt.;;44jHz?.;_...tti i rr .. t"4; -6; I .4 EFTA00278302

:7; pr 74. •:; F'! r." ?. .• . ; • •••...a sch.1 W . APPLICATION FOR U3 Leartor AIRWORTHINESS . Or ITIIIOnFal . fiadorat moan — CERTIFICATE Admilstralfen • , DiSTRUCTIONS - Ptint or type. Do not write in shaded areas: these are for FAA use oaly. Submit original only to an authorized FAA Representative. If additional • spuieis ;squire& use anattachment. For special flight permits complete Sections • II and VI or VII as applicable . 1.REGISTRATION MARK l• • a N979RA 2.MRCIa an in HUMPS NAME (Make( GULFSTREAM 3. AIRCRAFT MODEL III2SIGNATION _ 'Gt1159a• IL YR. MFR. '1974 FM COOING• t-eS CIS cl \ \C-. • I. AIRCIld TESCRIP1 5. AIRCRAn SF PIAL NO. • 151 .-- S. ENGINF BUILDERS NAME (Make) Rolls-Royce Spey - . 7. ENGINE MODEL DESIGNATION RB511-8 • - . ---- - 4 55 3 S. NUMBER OF ENGINF4 „ I. PROPEArgi BUILD RS NAME (Mate) 10. PROPELLER WOK DESIGNATION 11. AIRCRAFT IS (Check if applicable) 'Two(2) ._._., N/A I N/A - I IMPORT II. CERTIFICATION, REQUESTED APPLICATION IS HEREBY MADE FOR: (Check appidebb gems) A 1 STANDARD AIRWORTHINESS CERTIFICATE (Indicate Cals907) I 1N0fUSIAL 1 I UTILITY I I ACROBATIC' 1 TRANSPORT 1 I GLIDER _ r.. I BALLOON B X SPECIAL AIRWORTHINESS CERTIFICATE (Chock appeal:dam der* 2 LIMITED S • . I CLASS I ' . S PROVISIONAL (Wale asst . 2 CLASS II • 1 AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISING 3 RESTRICTED Unchcara be concise operation(s) to 4 • FOREST (Weds consenatton) _ S PATROLLING 6 WEATHER CONTROL -red) . . . 7 CDIAIAGE OF CARGO . a ' OTHER (Simon I RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT • 3 EXHIBITION 4 x ENTAtfintleat• tExbepERDA. ed o / opitiat.on(s) 4 RACING S CREW TRAINING MKT. SURVEY • 0 X TO SHOW COMPLIANCE WITH FAR . • . - 1 FERRY FLIGHT FOR REPAIRS. ALTERATIONS. MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT . (WIWI 2 EVACUATE FROM AREA OF IMPENDING DANGER r I operation to be conducted. Section VI Men • VII • 3- OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEIGHT - r .--- complete applicable on reverse Of as stool 4 DELIVERING OR EXPORT.. a $ PRODUCTION ;LIGHT TESTING . • • CUSTOMER DEMONSTRATION FLIGHTS . 2 C I 1 I MULTIPLE AIRWORTHINESS CERTIFICATE 'Once ABOVE 'Rostra red Operation" and -Slardard- or-Limited.- as applicable-1 _ .........• III. OWNER'S CERTIFICATION A. REGISTERED OWNER (As shown on certificate of Sweep IVIVISIftlIOO) IF DEALER. CHECK HERE I NAME • OGDEN MANAGEMENT SERVICES, INC. ADDRESS Westchester White Plains, City Arpt., HGR D3 NY 10604 B. AIRCRAFT CERTIFICATION BASIS (Check applscabee blocks are complete ;rens as inccaled) X AIRCRAFT SPECIFICATION OR 1 iPE CERTIFICATE end Revision No.) . Al2EA, Rev. DATA SHEET (Gres No. No. 17 X AIRWORTHINESS DIRECTIVES latest AD No ) 89-05-05' (Check if ad amicable ADC complied wan and give AIRCRAFT LISTING Kin. Pan number(-.) . . SUPPLEMENTAL TYISE CERTIFICATE (Lat number of each S TC incorporated) C. AIRCRAFT OPERATION AND MAINTENANCE s RECORDS - X CHECK IF RECORDS IN COMPLIAN 1.173CE WITH • TOTAL AIRFRAME HOURS 5669.13 3 EXPERIMENTAL ONLY (Enter hours florin since last combust issued Or mowed) mowed) mowed) FAR D. CERTIFICATION — I hereby certify that I Aornenishaoon in accordance with Section 50 airworthy and Ogitife lot the ainvontimess certificate am the registered owner (or bus *gent) of the Limit described above. Ihal Me aircraft of the Federal Aviation Act of Irak and applicable Federal Anshan Regulations/ and unveiled Is registered with the Federal Aviation that the aircraft has been inspected Ind is . DATE OF APPLICATION June 28, 1989 NAME AND TITLE term! Or type) • ..Carl E. Jones - Agent SIGN RE c ...7 . C-- - . ' IV. INSPECTION I • • AGENCY VERIFICATION A. THE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY. (Complete this section only it MR 21 62td (applies) 2 FAR PART 121 OR 127 CERTIFICATE HOLDER (Give Cerblicate No.) 3 CERTIFICATED MECHANIC (Give Certificate No .7 ' 4 CERTIFICATED REPAIR STATION i Gabe CitlidiCale No) • • ' ' ' S . AIRCRAFT MANUFACTURER (Give name of Ewen) e • - . _ . I . 7 • . DATE I , • • TITLE • _ . SIGNATURE . _ . .. i . • (Check ALL applicable (Necks on items A and 13J X a THE CERTIFICATE REQUESTED • &Imo that the aircraft described m Seaman I or VII meets recturremersts kic 4 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE id ai. Z 0 B. Inspechon for a metal fight Devine under Section VII FAA INSPECTOR FAA DESIGNEE <r 4 4 < Z u ass conduCte0 by - • . CERTIFICATE HOLDER UNDER: 11 FAR 65 1 . 1 FAR 121. 127 or 1351 1 FAR 5 tr. .., — . .., IS Y a ci. Iso DATE a DISTRICT OFFICE • • • - DESIGNEE'S SIGNATURE AND NO FAA INSPECTOR'S SIGNATURe • f „......- • . • . . . . • EFTA00278303

, 1. e • 1 A. MANUFACTURER • NAME t r.., . . ADDRESS - -, . • • ... B. PRODUCTION 13ASISIChick apptcatAattami WC' IT T PRODUCTION CERTIFICATE (Gni c004act•Oh cedar-ate number) . - TYPE CERTIFICATE ONLY APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE ouAtenn OF CERTIFICATES REOUIRED FOR OPERATING NEEDS DATE OF APPLICATION . . • . NAME AND TITLE Min 00 IOW) - • . SIGNATURE . . . . f • - - . VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION FLIGHT TEST A. DESCRIPTION OF AIRCRAFT I . • REGISTERED OWNER • • - .• ADDRESS A BUILDER (Ma/re) - 9 . _ MODEL - : r. - % a\ SERIAL NUMBER 11* REGISTRATION MARK I 8. DESCRIPTION OF FLIGHT . CUSTOMER DEMONSTRATION FLIGHTS 0 (Chen 4 appAcabir) FROM • TO . • VIA • • - DEPARTURE DATE DURATION. C. CREW REOUIRED TO OPERATE THE AIRCRAFT AHD ITS EOUIPMENT , I PILOT I • I CO-PILOT f , JNAVIGATOR - I . I OTHER apecoly7. - D. THE AIRCRAFT DOES NOT MEET THE APPIJCABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS: ` - - t. • • •. . • . • • ... . - • E. THE FOLLOWING RESTRICTIONS ARE c.orissoutEo NECESSARY FOR SAFE OPERATION (Aa attactmett si ninarstagy) . • ' • . - • '... - . .. • .- • . . . . .. . ' • , • • • • F. CERTIFICATION— thereby ctrlity lhat 1 enitheiegislerecl owner (or h4 agent) ot the aircraft described Mame: that at encratIoregistereiS with the Federal Aviation Administration in accordance wills Sechon 501 of the Faders, Aviation Ad of 18613. end applicable Fodivid Aviilion Regastions: and Mat Me aircraft has been enspecled and is airworthy for the Ilighi ' described. • • ' • • - • • • - — • - : ". • ' • . . • . . • • DATE f4A/AE AND TITLE (Pheifiar train - _ SIGNATURE VIII. AIRWORTHINESS DOCUMENTATION (FAA us. only) . •••• . Operatav Lorritatorts•rd Mirlungs tratcrrolarr-it wit• FAR Pr G. SCIANAWA of Conformity. FAA Form 8130-9 (Attach when Nature) X A ' 91 31 as'Applicable • " • . • N. Fair /unworthiness Cendication lot Import Aircraft ) 1/4/ EL Current Operitmc Lirritat errs Attached -. . (Attach than manned) • , C. Data. Drawings. Photogiaphs. etc. (Attich whin inuated) . L Pretoria Asnionniness Ce iticate n (wired in Accordance men Current Balance Info/mats, Astable Liman FAR, /. s83 C4%) CAR (cgromai miaow") X D. Weight and in . E. Maim Repair and Alteration. FAA Form 337Mdean when rahuirect) J. COMM Airworthiness Cersiticate Issued in Accordance with • X F. Trois Inspection Recorded m Aircraft R•soids ' FAR A). iqi a) • (copy attached) •. . . • •• •• • • ••44.1P+ .• • . • ••• . L. 0. • : ••• '" • • • • - . . EFTA00278304

• FAA? AUCPAFT RiC ISTET _CA..EFA h p1 DATE: sji - ors U umITED STATES OF AMERICA • „ . DEPARTMENT OF TRANSPORTATION - FEDERALAWATION ADMINISTRATION ' SPECIAL AIRWORTHINESStERTIFICATE A CATEGORY/DESIGNATION . EXPERIMENTAL .- . PURPOSE SHOWING' COMPLIANCE WITH'REGOLATIONS- pt. 1' MANU- FACTURER NAME - N/A , . , . ADDRESS N/A . C FLIGHT F FROM N/A .> To - :N/A D 979 R: N._ . SERIAL NO. • 151 - - BUILDER GULFSTREAM AU D?ACE MODEL C -1159A E DATE OF ISSUANCE 6-2$-89 EXPIRY 6 -28 -90 OPERATING LIMITATIONS DATED ' 6-28-89 ' ' AREA PART OF THIS CERTIFICATE: TYRE Of FAA RW A . .-./ . . JAMES E. JA SON ' -: DESIGNATION OR OFFICE NO. : .. . CE 45• Any attention. reproduction. or misuse 01 MIS bertittate may be punishable by a fine not exceeding 51.000 or 'imprisonment not exceeding 3 years. or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA FORM MSS? MOM ROC OFVFOSF SIDE ..":".Wir, taw • -• .: 'h.\ • • am, EFTA00278305

A ^ T4iS'airworafiness certificate is issued under the authority:rtzraiavig„lip Acopf 1958 and the Federal Aviation Regulations (FAR). . . B This airworthiness certificate authorizes the manufacturer named on the reverte side to candugt production flight tests. and only production flight tests, of aircraft registered in his name. No person may conduct production flight tests under this certificate:. (1) Carrying persons of ' property for compensation or hire; and/or (2) Carrying persons not essential to the purpose of . the flight . • a C . . . This airworthiness certificate authorizes the flight specified on the reverse side for the purpose `-' shown in Block A. n — • • .- . . . This airworthiness certificate certifies thatasof the date of isEuanCe, the aircraft to which issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable cornpretbensiwiand detailed airworthiness code as provided by Annex 8 to the Convention On International Civil Aviation. No person may operate . the aircraftdescribed on the reverse side: (1) except in accordance withthe appliCable FAR End in accordance with conditions and limitations which may be prescribed by the Actin inistratora:s part of this certificate: (2) over any foreign country without the special permission of that country.' • • L. E . - ..• • • sooner surrendered. suspended. or revoked. this airworthiness certificatais effective for the duration and under the conditions prescribed in FAR Part 21. Section 21.181 or 21217. • Nttrc . . 7: 4 •I t 4 • EFTA00278306

t ‘ EXPERIMENTAL AIRCRAFT OPERATING LIMITATIONS Research & Development, Showing Compliance With Regulations, Crew Training, Market Surveys: (Over 8O0'HP. 12,500 Dm) CGOLit-57ZN5Afin AaeosPasia) MAKE: Geatri ir7.41t) SERIAL NO.: /5/ MODE-:6:1-/iF5-77eXiscen7 6;-1/5" REGISTRATION NO.: Apg7959/9 1. No person may operate this aircraft for other-than the purpose(s) of S-1/72ze.m.2'1 (7,0,77,01.1.4/tn- Aolni AlE614I4-4177,-,.45C (FAR 21.191), to accomplish tests outlined in the applicant's program letter dated 6 - _2? -2W, describing compliancewith FAR 21.193(d). Additionally, this aircraft snail be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). - - 2. All flights shall be conducted within the geographical area described as follows: COATI IDF/V7-24A-, !7"1/17"6/9 S7 9r 3. No operations, including takeoffs and landings, shall be conducted over __ --densely populated areas or in congested airways; except those takeoffs and landings authorized as follows: ALL Al(7:7-ifttaF Al/Apick)A?)75 /We Ez/i.V1/1.4-c1C- 4. Unless appropriately equipped for night and/or instrument flight in accordance with FAR 91.33, this aircraft must be operated Day VFRonly. 5. No person may be carried in the aircraft during flight unless that person is required for the purpose of the flight. 6. No person may operate this aircraft for carrying persons or property for compensation or hire. 7. This aircraft shall contain the Flight Manual, markings and placards required by FAR 91.31. 8. This aircraft is prohibited from aerobatco_flight; that is, an intentional- maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude, or apnormal acceleration not necessary for normal flight. 9. The cogniiant FAA Flight Standards District Office must be notified and their response received in writing prior to flying this aircraft after incorporating a major change as defined by FAR Part 43, Appendix A. (Continued an Reverse) , EFTA00278307

. .Page 2 cf 2 10. The pilot-in..commard of this aircraft must,•as applicable, hold an' . Appropriate category/class rating, have an aircraft type rating,'have a flight .instructor's log-book endorsement or possess a 7Letter.Of Authorization" 4ssued .by an FAA Flight Standardi Distridt Office or. Air Carrier Operations. Inspector. 11. This aircraft shall-not -be-flown unlesSitii maintained and operated in accordance with approprigte military tedhniCal pUblicatiOnS, manufacturer's instruCtions, or FAA approved maintenance program ft:sr this aircraft. . . , 12. If aircraft, engine or propeller operatiOn limitations are exceeded, an appropriate entry will-be—made in--the historical records. (Applicable only to Research and Development and Showing COmpliande with Regulations.) 13. This aircraft shall-not- be` operated for glider towing or parachute jumping operations. 114 - The-aircraft shall bear the word "Experimental" near each entrance to the cabin or cockpit -in accordance with FAR 45.23. 6 - 4.5? -8P9 Date of Issue Representative Designation/Office No. EFTA00278308

FAA_ U.S. DEPARTMENT OF TRANSPORTATION Form Antlered . . • FEDERAL AVIATION ADMINISTRATION Baer Bonn No. 04-R060.I FOR FAA L'SE ONLY ". MAJOR REPAIR AND ALTERATION oFFINOSoatfola111) (Airframe, Powerplant, Propeller, or Appliance) . 7-0-67 • INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendie 8. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. 1. AIRCRAFT MAKE GULFSTREAM MODEL • G1159 I SERIAL hat 101 ' !NATIONALITY AND REGISTRATION MARK I • U.S.A. . N979RA NAME (4.5 shown on registration certificsde) ..., ADDRESS (As shown on registration certificate) 2. OWNER 1 HANGAR D-3 - WESTCHESTER COUNTY OGDEN AMERICAN.CORPORATION A WHITE PLAINS, NY 10604 3. FOR FAA USE ONLY • .. .- . .. . 4. UNIT IDENTIFICATION S. TYPE • Witt Mal . MODEL i an rat NO. • WAR AMA- AMON AIRFRAME neeneene••••••••••• (As described in item I above) •••••••neenermeneee PSI 177 .POWERPLANT ₹ . • ,i-r.7. FP „rep!? JAM 1 4_ . .: : 4 I ;‘ !, 11 PROPELLER LI I lircu. -.) ... i ! s , ....... ).__:,_- , .. !.:.',..).3(1':i.r : _ b . , Li , _, ..___ ..:t • APPLIANCE TYPE R/H ELEV. ASSY. 1159C520002-1 ‘-rt rare , r• S/N 151- . .• • .X MANIJIACTiall . • GULFSTREAM • • • 6. CONFORMITY STATEMENT • A. AGENCY'S NAME AND ADDRESS • B. KIND OF AGENCY C. CERTIFICATE NO. u.s. cteroncArEo MECHANIC GULFSTREAM AEROSPACE CORPORATION toseinN Mt/IMAM MECHANIC P.O. 80X. 2206— TRAVIS FIELD • x CEETIPICATED MANI STATION 701-10 SAVANNAH,GA. 31402 ssassuractuara D. I.certify that the repair and/or alteration made to attachments hereto have been made in accordance with ' end that the information furnished herein is true and the unit(s) identified in item 4-above and described on the reverse or the requirements of Part 43 of the U.S. -Federal Aviation Regulation, correct to the best of my knowledge. DATE 1-8-87. SIGNATURE OF AUTHORIZED INDIVIDUAL PATRICKAL LYNCH e best orS . cm.m....€4....., 7. APPROVAL FOR RETURN TO SERVICE Pursuan 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 go APPROVED OREJELC ...„--...., BY PIA FM STANDARDS INVICTOI . fitanura.cruin INSPECTION AUTTIOIJZATION . ONES 'In ; ) . FAA DESIONEE X REPAIR STATION CANADIAN DEPARTMENT Of TRANSPORT IMPECTOS Of Ammar DATE OF APPROVAL OR REJECTION • 1-487 . CERTIFICATE OR DESIGNATION NO. . 701-10 - SIGNATURE OP AUTHORIZED INDIvIrWAL az,24, ,_.- PATRICK 'J. LYNCH . e FAA Fenn 337 (7-67) (8320) EFTA00278309

P4()1rICEi, 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.) . REF: GULFSTREAM AEROSPACE CORPORATION WORK ORDER NO. CO2B-0151-087-2654 REPAIRED L/H ELEVATOR ASSY. P/N 1159CS20002-1 S/N 151 PER GULFSTREAM AEROSPACE CORPORATION DWG. NO. 1159CS20431•MASS BALANCE CHECK PER GULFSTREAM AEROSPACE CORPORATI CUSTOMER BULLETIN 264 HOW TO MEASURE CONTROL SURFACE STATIC BALANCE. (REPLACED DAMAGED TIP AREA SKIN WITH NEWHPART-PANITED SAME) K ADDITIONAL SHl±IS ARE ATTACHED C FAA AC 72-4908 EFTA00278310

it I . r. DEPAPIMENT OR TRANSPORTATION . FEDERAL AVIATION ADMINUSTaATION - MAJOR REPAIR AND ALTERATION (Aiiitatne.,Powerplant, Propeller; or Appliance) Foto: Approved • Budget Bureau No. 04-R060. t FOR FAA USE ONLY; p • OFFICE 41 N -,,: IFIr it uent INSTRUCTIONS: Print of:type all entries.-• See FAR 143..9,• PAR 43.Apii,n44.B, and AC 43.9-1 (or subsequent revision thereof) for instructions. arid diSposition of this fbrm. • ' . • . • - . ' ' • • • . . • 1. AIRCRAFT MAKE G1112912111111 mopia 0.1159B . . SERIN. NO: 181 . 7 NATIONALITY. AND REGISTRATION MARK 219799,9 2. OWNER NAME (As shown on registration certificate) 09912/ AMER/CAN MIL' ADDRESS (As shown on registration certificate) 277 PARK AVENUE N.Y., A.Y. 10017 3. FOR FAA USE ONLY , . ... . . . . . . 4. UNIT IDENTIFICATION 5. TYPE UNIT MODEL SERIAL NO. ItElMit " . ALTER- .ATIoti AIRFRAME ne.reemenommen (M destrind in item ; above)(men•npnewswem POWERPLANT PROPELLER - - - - • • TYPE • • • : w:.,... • • .• • • ' - ' - - APPLIANCE MANUFACTURER . . ... - . • • • • • - 1 • 6. CONFORMITY S1ATEMENT • • • A. AGENCY'S NAME AND ADDRESS, ! • B. KIND. (IF AGENCY C. CERTIFICATE NO. MIDWAY AVION/CS-CORPORAT/ON U.S. CERTIFKi.TED•MECHANIC BLDG. 15 FOREIGN .cuifFIC.ATI0 MECHANIC .. • . WESTaignim COUNTY AIRPORT . lac CERTIFICATED. Remit STATION • 111-92 n-,Erp 4iNs, NEw YORK .10604 - MANUFACTURER--. , D. 1 certify that the repair and/or alteration lade to attachments hereto -have•teea.made in accordance with and that the infortgatiod furniihed hereiniktrue•ind-correct the unit(s) identified in item 4 above and described 'on the reverse or the reqiiitements.cf Part 43 of the U.S. Federal Aviation Regulations to the best. sf my knowledge. . DATE • ..... -. -,„..-.-•,. . 5 , • • • 12--30-85 • - .. . 4IGikii.:frit:ok AUTHORIZED I DIVIDUAI • 4 • V. iiht THOMAS V. MCGRATH ' 7: APPROVAL FOR RETURN TO. SERVICE • Pursuant the BY Adininistragor to the authority of the Federal FAA at StAtiPAPS INSPECTOR given '- s persons speCified below Aviation Administration • OTHER FA.F.NUF*Aatiiiii.: the unit identified in item 4 was iicipetie.d in the manner prescribed by and is APPROVED • REJECTED (Specify) • • INSPECTIONAuitieitthArtori • . . . • • FAA DESIGNEE lInt FEEIAIR• STATION • CANADIAN DEPARTMENT .... OF TRANSPORT. INI.PEaCit : - ' OF AIRCRAFT • i ,- • • DATE OF A112Q130-(85 REJECTION 12-30-85 CERTIFICATE .OR • DEtIGNAntirciiti 111s93. :•.1 • 'MMU$ TORE OP LITHORIMe XI IVIDUAL ergo . iThe . • - 18862428 • (832I:” EFTA00278311

?;. - TAA ATPCP.AFT_J:EGISTFLI‘ r CAMERA NO. DATE: • , • • 4.1-e-. . - • figenAe..4;fr A • -I. V " NOTICE .. • , . Weight and balance or operating limitation changeshall be'entered in the aircraft record. An alteration must co_ mpatible with all previous.aberalions to assure continued conformity with'the applicable airworthiness requirements. \- • 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. craft nationalitrond'registration mark and date work completed.) . • TEE,INSTALLATION_WAS ACCOMPLISHED III ACCORDANCE WITH MULFSBER0 .INSTALLATION/OPERATORS MANUAL. P/N. A.04/119-00 REV. El SECT. II. , THE DRITEI WIRE INSTALLEDAND INSPECTED IN ACCORDANCE WITH FAA AC 43.13-1A, CHAPTERS 11 am 1SJ and FAA AC 419.1S-EA, CHAPTER 10. EMI AND RPI CHECKS WERE PERFORMED, AS WELL AS, SYSTEMS, OPKRATIONAL TENT. NO ADVERSE EFFECTS WERE NOTED AND SYSTEM OPERATIONAL CHECKS WERE GOOD. THE SYSTEM HAS A NEOTIO/BLE EFFECT ON THE TOTAL ELECTRICAL LOAD OF THE AIRCRAFT. THE AIRCRAFT EODIPMENT LIST AND WEIGHT AND BALANCE WERE UPDATED TO REFLECT. THE CHANGES. • Itru.s Govastascr PRINTING OFFICE: 1977-711-02O200 • • EFTA00278312

, DEPARTMENT Of TRANSPORTATION • FEDERAL AVIATION ADMINISTRATION Forte Approved Budget Bureau No. 04-R060.i MAJOR REPAIR AND ALTERATION - • FOR FAA USE oNLy7.4+7C, (Airframe, Powerplant, Propeller, or Appliance) OFFICE IDENTIFICATION r AZ 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 instruction's and disposition of this form. c... GULFSTREAM . . MODEL ' • G-11598 1. AIRCRAFT SERIAL NO. - 151 NATIONALITY AND REGISTRATION MARK N 979RA 2. OWNER • NAME (As shown on registration certificate) OGDEN :AMERICAN CARP. ..-- - ADDRESS (As shown on mgistralion certificate) •277 PARK AVENUE NEW YORK, N.Y. 10017 3. FOR FAA USE ONLY • _ . , . .. . .- . 4.- UNIT IDENTIFICATION S. TYPE • ' UNIT MARE MODEL i SERIAL NO. REPAIR . ALTER- ATION AIRFRAME • . nomenneenniens (As described in item 1 abore)••••••*4••••••••••••• . XX . POWERPLANT 0 .... . . PROPELLER .. - • - ••• - • ' • . . .... .... - -,- • • ' . . APPLIANCE . MANUFACTURER ' ' . - • 6.- CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS B. KIND OF AGENCY C. CERTIFICATE NO. THOMAS V. Mc-GRATH X U.S: CERTIFICATED MECHANIC • 731 Hungry Harbor. Rd. FOREIGN CERTIFICATED MECHANIC - No. Woodmere, N.Y. 11581 CERTIFICATED REPAIR STATION ---• 1886228 . . MANUFACTURER. . . T- • D. I certify that the repair and/or alteration made to attachments hereto have been. made. in accordance.with and that the information furnished herein ,is' true and the tiiiii.(s) identified in item 4 aboye and described on the reverse or the requirements of Part 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. DATE g - 1- sc. ... ,.. SIGNATURE OF AUTHORIZED INDIVIDUAL • Thomas V. McGrath Plar Y Al Clas2Se • • • - .• 7. APPROVAL FOR .RETURN TO SERVICE - - Pursuan to the authority given persons specified below the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Petrel Aviation Administration' and i-: O APPROVED O REJECTED FAA RT. STANDARDS ,. INSPECTOR MANUfACTURER X INSPECTION AUTHORIZATION OTHER (Spocifr) . . . .. . BY • FAA DESIGNEE ' REPAIR STATION CANADIAN 'DEPARTMENT' '' OF TRANSPORT INSPECTOR OF AIRCRAFT y • .• DATE OF APPROVAL OR REJECTION ,. ' . 8 - -2- - g C CERTIFICATE OR DESIGNATION NO. IA 1886228 SIGNATURE OF AUTHORIZED INDIVIDUAL' • Thomas V. 'McGrath 01/4t1-0 V. cjt(440f---- . . .47 r • / . • - . _ . • • • - - - • • • . • • . EFTA00278313

- • 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 ACCCIMPLISNED.(If more space is required, attach additional sheett:--- Identify with air- craft nationality and: registration mark and date work completed.) • A Sunstrand Dititontrol Ground Proximity Warning .Systeni, tomputer P/N 965 13411 -010,-wes'installed on:the aircraft..' :The installation was performed in ao nrdance With' the instructions of,STC.SA36NW. The units-Were installed and inspected -in accordance with Chapters 11 & 15 ;of' FAA AC'43;13-1A. andr.CfiaPter10. OfFAA:AC4'.:037A.,;;ESI:and RFI tests were performed. An electricalfiloackanalysis;vas-perfoimed with the -results being negligible. - • 'A flight teet-VIS .8eindilated-in:StCapitante...WitiOlonUfadturer's pacument Number 060-0?78-007. The:syptem-perfotmed;vitliin::011:iolerenites. An FAA' Approved- night Manual Supplement :v9aS ;incorporated into Flight Manual. The aircraft-Weight -and-Bilante:Report dated 6-71-84 was updated with a .including a revised EquipMent:LiSt.-_ ' • ADDITIONAL SHEETS ARE ATTACHED. ik US. GOVERNMENT PRINTING OFFICE: 1977-771-071 ngo • . EFTA00278314

i • t': • : it A UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION•-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I. NATIONALITY AhO REGISTRATION MARKS 2. MANUFACTURER 14,5...rMODEL If. . , ' •••• • —• GULFSTREAM G-1159B •5. AUTHORITY AND BASIS FOR ISSUANCE ) ..:&:-.t -T-.. This airworthiness certificate: is itsUed pursuant•to:elet.. 958 and certifies that/at of the date of Issuance, the aircraft tot hick issudd'hers'berc conform to the him RATI;6034 therefor, to be in condition for safe operotiOn,:and: requirements of the applicable comprehensive and detailed airetwthinessloid• Or Convention on International Civil Aviation, except as noted. herein. --.....; \ A ... Eroeptions: 4. 7±e—..—_—_ L.( ' • ! • 'NONE 7/ 1, A. TERMS AND CONDITIONS " y ' . CI Unless sooner surrendered, , revoked, at a tirinincrliondate is atlstameho established by the Administrator, 'this airworthiness certifies • it effective as long os-the , 44 snaintenance, and alterations ate • perionnod in accordance th Parts 21, OS and 91 oft Aura' ,yriladOrrThen. MI appropriate, and the aircraft is registered in the United. States. I . DATE OF ISSUANCE DMIGNARtirrigl Al 6/4/84 SAV-MIS0 Any alteration, reproduction, or misuse of this aertiAcate by a not exceeding $1,000, or ins. prisonmeni not exceeding 3 yews, or bath. THIS CURING T MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORD• ANCE WITH APPLICABLE FEDERAL AVIATION REGULATIO FM Form 8100-2n-671 FORMERLY FAA FORM 1362 • • - -,c1. - - • Yl Cimae• Pam. COMO ••••=.•=. EFTA00278315

Irt E' t . • : -T. - • - ' . - • ' ••••-- • . EFTA00278316

No cStificlitemey bli issued unless a completed ...Station • loan has bleat received (14 C.F.R...21) DEPARTMENT OF TRANSP9RTATION ' FEDERAL AVIATION ADMINISTRATIRN * APPLICATION FOR AIRWORTHINESS CERTIFICATE II.OTRUCIIONS — Pionebs.type: Do not write in shaded areas; these after FAA use only. Submit original only to an authorised MA Representative II addiiional space is required. use an attachment. For special flight permits. complete Sections II and VI or irpa5 applicable. . , I. AIRCRAFT DESCRIPTION 1. REGISTRATION MARK 2. AIRCRAFT BUILDER'S NAME Woo N979RA • GULFSTREAM . (.AIRCRAFT MODEL DESIGNATION 6-11598 4.YR. MFG. ' 1974 FAACODING . • g 9 gii //, 5. AIRCRAFT SERIAL NO. 151 1/4 • B. ENGINE BUILDER'S NAME Wake; ' ROLLS ROYCE,: 7.ENGINE MODEL DESIGNATION • .SPEY MK 511-8 - 5-0.5.2-3 ' • . S. NUMBER OF ENGINES 9. PROPELLER BUILDER'S NAME IMAM IO.PROPELLER MODEL DESIGNATION i 1 LAIRCRAFT IS. • TWO • N/A • N/A *HOMO ORX X X IMPORT. , . . 'ION REQUESTED APPLICATION IS HEREBY MADE FOR: (Check seplkable items) A IS, X STANDARD AIRWORTHINESS CERTIFICATE twicartesreSionf I IffORMALI ' 1 UTILITy. ' ACROBATIC X 'TRANSPORT I I GLIDER ' BALLOON B 1.. ..e SPECIAL AIRWORTHINESS CERTIFICATE (Check satliroonnt tint) LIMITED - I': CLASS( - 5M • PROVISIONAL fIncleitit demi CLASS II n..' AGRICULTUREPADPEST CONTROL AERIAL SURVEYING 3 I :Otilt lriitiING inn. RESTRICTED (Indians i anntion to - be conducted, • • - FOREST Ulan Coneentnnl PATROLLING 5 I WEATHER CONTROL -.. OTHER iSiieWO oils RESEARCH ANTICIEVELOPMENT AMATEUR BUILT 3 EXHIBITION l',.#1 4 EXPERIMENhl (IndOleoperationgs/ - .... to be conducted) . RACING CREW TRAINING 5 I I SURVEY ,- c•-• . _ ' TO SHOW COMPLIANCE WITH FAR • . Adel . • _ FERRY FUGHT FOR REPAIRS, ALTERATIONS, MAINTENANCE OR STORAGE C45 L*4 SPECIAL FLIGHT PERMIT (Indicate iA operation to tie conducted. the. - EVACUATE FROM AREA OF IMPENDING DANGER . complete Section nor Vitas . • aoolicaln on reverse sal . .. OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEIGHT ' • DELIVERING OR EXPORT . 5 I PRODUCTION FLIGHT TESTING C 5 MULTIPLE AIRWORTHINESS CERTIFICATE !Check ABOVE -RestriCtedOpenrion"and "Standard" or "Lennin.- as exec-salsa III. OWNER'S CERTIFICATION A. REGISTERED OWNER Ms shown on ceilificate of aircraft registration/ IF DEALER. Ci4ECK•HERE I - NAME ADDRESS • OGDEN -AM ER I CAM CORP. • , WESTCHESTER COUNTY AIRPORT WHITE PLAINS. NY B.AIRCRAFT CERTIFICATION BASIS (Check applicable blocks and complete iteeWezt indicated) X AIRCRAFT SPECIFICATION OR TYPE CERTIFICATION DATA SHEET (Gaelic. and IrritA REV . • 15 X AIRWORTHINESS DIRECTIVES (Check if all notice:3e AD's compaed wan and give inn""`" 82-11-02 AIRCRAFT LISTING Mire page numeerlsil • N/A.. X SUPPLEMENTAL TYPE CERTIFICATE (Lest nano.. r of each STC intonate:ern . SEE ATTACHED LIST C. AIRCRAFT OPERATION.AND MAINTENANCE RECORDS • • . X D. Administration been CHECK IF RECORDS IN RL.tair7IICE WITH . CERTIFICATION — I hereby certify in acccordance wi :nspected and is airworthy and TOTAL AIRFRAME HOURS (Entter kr used incraft only1 EXPERIMENTAL ONLY tenter:nuts flown 'glee last cartilicste issues 3593.7 HRS. "'in' 7.3 HRS . .. that I am the owner for his agent) of the fl ash described above; that the aircraft is registered with the Federal Aviation It Section 501 of the Federal Aviation Act of 1958, and applicable Federal Aviation Regulations; and that the aircraft has eligible for the airworthiness certificate mutated. DATE OF APPL•CATiON 6/1/84 NAME AND TITLE !Print Or NON -. • PATRICK J. LYNCH SIGNATURE ea.c..ix b' IV. INSPECTION AGENCY VERIFICATION A. THE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (COMO:Ste this section Only if FAR 21.183 id) apples) 2 *tit FAR PART 121 OR 127 CERTIFICATE HOLDER (Gin Certificate No.1 CERTIFICATED MECHANIC /give . . Cilrleate No. i X CERTIFICATED REPAIR STATION (Give Ceinficete N 1' • 701-10 li aiaa AIRCRAFT MANUFACTURER (Ginner* of firml GULFSTREAM AEROSPACE CORPORATION \ DA E 6/1/84 TITLE QUALITY `CONTROL MANAGER SIGNATURE . ?ara.A Si V:FAA REPRESENTATIVE CERTIFICATION (Check ALL applicable eiocksinitems A end 81 fl THE CERTIFICATEREOUESTED • A. I find that the aircraft described in Section I or yr meets requirements for: . AMENDMENT OR MODIFICAT ON OF CURRENT AIRWORTHINESS CERTIFICATE , . B. Inspection for a special flight permit under section VII • FAA INSPECTOR was conducted by• CERTIFICATE HOLDER UNDER: . F A 65 I F 210R 127 I FAR 145 DATE DISTRICT OFFICE . DESIGNEE'S SIGNATURE ANON°. . FAA I C 'ATURE 6/4/84 t ACE-181A-1 t 6/4er.- : SAV-MISO . .. .. - . • EFTA00278317

I • r -VI. PRODUCTION I FLIGHT TESTING A.MANUFACTURER .. • • • N . - NAME. • • - . :. — ' • ADDRESS 't • B.PRODUCTION BASIS (Check eseltable awn) • PRODUCTION CERTIFICATE (Gin pi-admits, estficste number/ . TYPE CERTIFICATE ONLY APPROVED PRODUCTION INSPECTION SYSTEM C.GIVE QUANTITY OF CERTIFICATES REQUIRED FOR OPERATING NEEDS —....-,- —.10. , . • DATE OF APPLICATION NAME AND TITLE JAHN wisp& , . . SIGNATURE A.DESCRIPTIQN Of AIRCRAFT _ - FIEGISTERED OWNER • ADDRESS . , . . .". .• BUILDER (Mete - •: ' MOOD. SERIAL NUMBER • REGISTRATIONAAARK • . .. B.DESCRIPTION OF FLIGHT . , ' FROM . - TO - ' . . . . • . VIA • DEPARTURE DATE . DURATION C.CREW REQUIRED TO OPER ATI THE AIRCRAFT AND ITS EQUIPMENT —I- PILOT I CO-PILOT 1 1 NAVIGATOR I • • - OTHER doeeork.-• - • . VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PROD' t D.THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS: .1 • .... • - .. • ( . . • .., ‘... r • -0., : . . - '• ' - • ..• '"" . .. . _ E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY FOR SAFE OPERATION (Useartachmont if necessary) ea ' .. .-. - • • • • • - - - -- . .. . .... . . . —. . • . : . ---- _ . . -. ... — • .. ei - • .. - . - a ' ,.. >.. • . • • e F. CERTIFICATION — thereby certify that I am tits rtgistared owner la he agent) of the tweraft described above; that the aircraft is registered with the Federal Aviation Administration in accordance with Section 501 of the Cadged Aviation Act of 1958. and applicable Federal Aviation Regulations; and that the aircraft has been inspect4andis airworthy for the flight deserted. DATE r NAME AND TITLE AweWine I SIGNATURE •... i .I V,II.AIRWORTHINESS DOCUMENTATION (FAA use only) A. Operating Limitations and Milricingairi Compliance trth FAR. Y 0. Statement of Conformity, FAA Form 8130-9 (Attach when required; X 91.31 as Applicable : H. Foreign Ainvonhiness Cenificatioi for Import Aircraft B . Current Operating Limitations Attached (Attach when required, .., • C. Data, Drawings, Photographs. etc. (Attach when required) I. Previous Airworthiness Certificate Issued in Accordance with X .. D. Current Weight and Balance InIormatkin Available in Aircraft X FAR21.191 (b) CAR (Original attached) X E. Major Repair and Alteration, FAA 337 (Attach WhIlf/ Mtlefadi J. Current Airtiorthiness Certificate Issued in Accordance with . X F: This Inspection Recorded in Aircraft Records . X • FAR 21.181 (d) /copy imachoth . :t•—• . . • --<"•---7--14"-e',.:s,17- - - . . . • :••••••re • . I • • • - EFTA00278318

I , . UNITED STATES OF AMERICA DEPARTMENT OFIRRNSPORTATIOI:s1) ' • - • . FEDERAL AVIAT1O-WADMINISTRATION \ 4C:. . A . STATBAENT OF CONFORMITY *IN .PART THERE OF 1 - SECTION I - AIRCRAFT / 1. MAKE GULFSTREAM - -G-11598 3. SERIAL NO. 151 4. REGISTRATION NO. N-979RA SECTION ,II ENGINE 1 • MAKE 2. MODEL • • 3. SERIAL NO. • SECTION III PROPELLER I. MAKE 2. NUB MODEL. 3. BLADE MODEL' _ I. Hue SERIAL. NO.. _ 5 BLADE SERIAL NOS =nom Iv - CERTIFICATION • I hereby certify that: . • . • • . . . . . El A. I have complied with Section 21.33(a).' - 0 21 Subpart FL conforms to its type certificate, the type design therefor. F), conforms to its type pitch propeller was subjected Fl (G.A.C. A.S.C. •s B. The aircraft described above, produced under type certificate only (FAR is in a condition for safe operation and was flight cher:lied on • • 0 C. The engine or propeller described above, presented \'' • (1) oft) . C. herewith for type certification, conforms to • under type certificate only (FAR 21 Subpart The engine or, if applicable, the variable on D. The engine or propeller described above produced certificate end is in a condition for safe operation. by the manufacturer to a final operational check GULFSTREAM AEROSPACE CORPORATION. NO. 300 "GIIB WING MODIFICATION") Deviations: . NONE , - • . • . • . . - . • . . • - • Mara/ • DWG. NO. 1159-2500 REV. NO-DEO ..., • . . . • e---, • . • • \ . - . . • . .. . SIG/4Af itiisivagat r PATRICK J. LYN TITLE -‘,. \ MANAGER QUALITY CONTROL ORGANIZATION • GULfSTREAM AEROSPACE CORPORATION pr' DATE 6/1/84 ' EFTA00278319

- This IQ* sboutd be latsnitted to • .teprostritative pram Aldaikstuttir ander the following circumstances: . . • . . • L. By the applicant for o type certificate. ca • suppleseatel type certificate at the time be presents c aircraft or parts tinfoil to the FAA for Loa By the applicant fin • type certBintt• at a sopplarantal type certificate for each engine or prepeller submitted for type certificatican- _ — . By the type certificate holder or licensee msmnfaCtnring products under a type certificate only, upon the initial transfer by him of the ownership of each product or upon application for the original issue of an aircraft airworthiness certificate:or en -Attworthiness Approval Tag (FAA Form 8130-3k. This form should be completed as Lotion Section I. Aircraft. Complete the pertinent pest of only this Sidon volsa1 certification covers an aircraft or part thereof. Section lL Engine. Coriplete this section when ceirtifiarlionfloiliiiieitgine- _ .. . Section III. Novell er...:Caterplete this section when certifications carvers a propeller. • / Section IV. Certification. .. - been A. Check this block when an aircraft or partttierettcbt presented fir (Met or ground tests during type certification or supplemental type certification.. heat B. Check this block -when the bolder or licensee of a type certificate only, initially transfers the owner- ship of an aircraft manufactured under that type certificate, or applies for the original issuance of an air- worthiness certificate. • - Item C. Check this block when an engine or propeller is presented for type certification. Item D. Check this block when an engine or propeller islpitiented for anorthines's approval and insert the • date the product completed a final operational check. • • ' • • aa, ' S \rel.-sr-A:m. s t it , - ' EFTA00278320

Attachment for Application for Airworthiness Certificate for.G-IIB S/N 151 N-979RA SA 722 EA. W/FMS SA 1057 SW W/FMS SA 1553 SW W/FMS SA1861.SW W/FMS SA 1037 SW W/FMS SA 951 SW W/FMS. G -II B-82-001 G-II B-82-003 EFTA00278321

EFTA00278322

. : • FAA AIRCRAFT REGISTRY CAMERA NO. 3/V DATE : 3 7- Ea Attachment "8" Page 1 of 1 Date 6/1/84 Attachment for Application for Airworthiness Certificate for G-II8 S/N 151 N-979RA • Listing Of SupOleMental Type Certificate S.T.C. Subject 1. SA 722 EA Safe Flight SCAT System W/FMS 2. SA 1057 SW W/FMS IDC Sat/Tas Indicator with , Rose Mount Probe and Collins FD-109-Y Flight Director System and Provisions for Flight data Recorder 3. SA 1553 SW Collins INS - 61-B W/FMS. 4. SA 1861 SW Sperry ADC-200 Altitude Computer W/FMS and Alt Preselect System 5. SA 1037 SW Interior Emergency Lighting W/FMS 6. SA 951 SW (32 System, Long Range W/FMS 7. SA 1193 SW- Weather Radar RT Mounting 8. SA 999 SW (Provisions.For) Collins AUR-101 Cockpit Voice Recorder. 9. SA 1918 SW Jump Seat Installation 10. SA 2512 WE Relocate APU Speed Logic Control Unit 11. SA 1613 SW BKM Master Warning Interface 12. SE 994 EA 'Oil Tank Sight Gage Float EFTA00278323

• • . • • L. • :;" I, 9% c • .` -." . • . - -0,2' 'in '''.-sez••;"r -7.4%. . -‘ • • • EFTA00278324

'Attachment "C" Page 1 of 22. • Date 6/1/84. • Attathment for Application for Airworthiness,certificate-for T-111B S/NI151 N-979RA Subject Incorp ASC 216 Speed Brake Flap Alarm In conjunction With BKM Lighted S/B Handle (STC SA 2366 SW) 1. Infttllal BKM Pitot Heat Monitor Per 2. Modified Rudder Hinge Points For ASC 300 PER 1159CS25000 ' 3. Repaired enter And Upper Hinge Points on Rudder Per 1159CS20092, 1159CSM 30080 Aand 1159CS20080 Installed VLF/ADF Coupler For Coupling ADF Sense Ant To Existing VLF (TSO C-94) Repaired R/H Wing Structure Flap, and Gear Door Due to Tire Blow Out Per SC 1159CS806 t/W AD 74-17-05 Reactivate Ground Splr System Per ASC 180 And Installed Ground Splr Inspector Window Per 1159RDF260 C/W Safe Flight "Spded Control Auto' Throttle" Modification STC SA 722 EA Relocated Safe Flight Accelerometer Per 1159RDB343 Installed Dual Collins NCS-31 System Wiring Per EAS DWG 180601 Structural Attachment I/A/W AC 43-13-1 Chapt 11 Ibstallation of complete Avionics Package (Wiring And Sheetmetal) 8 Pages Installed Interior Emergency Lighting "System, Installed Page Gulfstream Jufflpseat STC 1918 SW Installed Cabin inSulation, Relocated APU Speed Logit Control Per STC SA 2512 WE Installed BKM Master Warn Interface Unit Per STC SA 1613 SW. Installed Oil Tank Sight ;Gage Flout Per STC SA 994 EA . . CoTplete Int9rjor Installation (10 pages) •W/ Eiec load analysis.`, EFTA00278325

FAA AIRCRAFT REG/STRY•• CAMERA NO. 3A/ DATE: 3 —42 7 — c7-5: • .:"; 45, - • 7e. • t•-eniVrtir :•• jet;t.as • .• • •'.4iv•at '..1Col: agt1:, ••: • • *- EFTA00278326

Attachment for Application for Airworthiness Certificate for,GIIB S/N 151 N-979RA EFTA00278327

.4 1 • • atrTte...C..• at i t • •." .41470., 7:.? ...:0-st. 4. • e: ▪ 'LL-etrallow- . • . - EFTA00278328

• DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION : . - APPLICATION FOR AIRWORTHINESS CERTIFICATE ..,. INSTRUCTIONS —, Prir.t or type. Dc not write in shaded areas; these are for F 4A use only Submit original crgy to an authorized FAA Representative. II additional space ts required, use an attachment. For 'special flight minus complete Sections ll and VI or vii as aPPliCable • ICRAFT1 SCR IPTION 1. REGISTRATION MARK N -979RA 5. AIRCRAFT SERIAL NU. 151 - 2 AIRCRAFT 'UILDER'S NAME Wend GULFSTREAM B. ENGIN9 BUILDER'S NAME Marl ROLLS-ROYCE 3. AIRCRAFT MODEL DESIGNATION le .YR. MFG. G-11596 1.1974 FAA CODING . - 7. ENGINE MODEL DESIGNATION SPEY MI: 511-8 10.PROPELLER MODELDESIGNATION 11.AIRCRAFT IS. 8:NUMBER OF ENGINES TWO I. PROPELLER BUILDER'S NAME Mahe "N/A . - ' N/A . KKKKXXXXXXI I IMPORT APPLICATION IS HEREBY MADE FOR: lava no:tat* items/ A fc STANDARD AIRWORTHINESS CERTIFICATE Proms cap:WI INORMAL 1 UTILITY ACROBATIC TRANSPORT I I GLIDER 1 I 3ALLOuN X SPECIAL AIRWORTHINESS CERTIFICATE (ClocUerretet • tonal • LIMITED C., us • ,. • • -' - CLASS I tu PROVISIONAL ithelicets duel nit. CLASS It 3 0 tu ,----7 G i A" RICULTLHTEANDPEST CONTROL 2 $114 : ' • AERIAL SURVEYING 3 i I tK IA LTISING 2 ST RE RICTED andicat mention to ..,, . be conducted/ ISM FOREST (Wedge conservation, 4 PATROLLING i I I WEATHER CONTROL 0 ... " • L".11 ,• OTHEn Mosey/ V IgrAll RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT 3 I EXHIBITION EXPERIMENTAL (lactate opeciNonis/ • to becondueral) t_'..,4 ---..:,- RACING I CICW TRAINING 4 MKT SURVEY TO SHOW COMPLIANCE WITH FAR .. " q r, L FERRY FLIGHT FOR REPAIRS. ALTERATIONS. MAINTENANCE OR STORAGE • 0 Sc'ECIAL FLIGHT PERMIT (indicate operand" robe conducted. then r. -r 6it EVACUATEFROM AREA 0F9.1PENDING DANGER ccfneNteSeirion Woe Wi Vadat* on Jenne sloe! n 2 OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEiGHT 4 I DELIVERING OR EXPORT 4 PRODUCTION FLIGHT TESTING C 1 I I MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE "RettfiCtOd °prawn" and "Standen:I- or "bmgeo." es ODDiCable ) V . FAA I IV. IANINZT 10 N REPRESENTATIVE III. OWNER'S CERTIFICATION CERTIFICATION • VERIFICATION A. REGISTERED OWNER fAs shown on certificate ot aircraft registration' • IF DEALER. CHECK HERE I NAME • OGDEN-AMERICAN CORP. ADDRESS WESTCHESTER tOUNTY AIRPORT WHITE PLAINS, NY. El .AIRCRAFT CERTIFICATION BASIS !Check applicable blocks and cornplete 'firsts indicated) . . AIRCRAFT SPECIFICATION OR TYPE CERTIFICATION DATA SHEET (Gin No.- and Revision Nod . N/A AIRWORTHINESS DIRECTIVES (fleck Attest AD Nod Na if arrappl-cao: e AD's compieo awn ono cve AIRCRAFT LISTING (Give page nomberf in - • SUPPLEMENTAL N/A TYPE CERTIFiCATE Iter N/A numoet ot taco S7.: axon:lowed) C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS • - - t, A HECK IF RECORDS IN AR 9i .i OMPLIANCE WITH 73 TOTAL AIRFRAME HOURS (Enter for used aircraft °Nei 3586.00 HR. b._ EXPERIMENTAL ONLY or---di ' di N/A 'Enter Frours lbws since Last Certibcare caved' / ' D. CERTIFICATION - I hereby certify that I am the owner (or his agent) of the aircraft described above; that the aircral: Administration in ecccordence with' Section 501 of the Federal Aviation Act of 1958, and applicable Federal Aviation been inspected and is ainvortiw and eligible for the airworthiness certificate requested. is registered with the Federal A;iialtof - Regulati,ms; and that the aircrati. has DATE OF APPLICATION 5/16/8.4 NAME ANDTITLE /Print or Time/ ROY CHRISTIANSEN - AGENT A. THE AIRCRAFt• DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Complete this rion only if FA .183 (di appbes) 2 FAR PART 121 OR 127 CERTIFICATE Corn:Kate No.I HOLDER (Give CERTIFICATED MECHANIC (Gat ' • . Cettikste No.! ..• CERTIFICATED REPAIR STATins IGin Certificate No .. • aml AIRCRAFT MANUFACTURER (GNI; monied finn1 DATE TITLE SIGNATURE . - (Check ALL topic** blocks in nen A and El . ... Vi„)( THE CERTIFICATE REQUESTED A.I find that the aircraft described in Section I or VII meets requirernentS for: is AMENDMENT OR MODIFICATION OF CURRENT AiRwORIHINESc CFR 1 FICATE B. Inspection for a special flight permit under section VIE FAA INSPECTOR • was conducted by CERTIFICATE • i HOLDER UNDER'. FAA 65 FAR 121 OR 127 I FAR 145 DATE DISTRICT OFFICE DESIGNEE'S SIGNATURE AND N . , ACE 181A-1 for.../KS-. DMIR 5/24/84 SAV -MISO PATRICK J. L CH ACE-1 FAA INSPECTOR'S SIGNATURE FAA Form 8130-6 14.801 SUPERSEDES PREVIOUS EDITION . , '• ••• n. • . • , .4-mun : 34 aliar. .. • eu:n2.:YM• 1.77,7:--S—• • - .411:714irast... • • • • air • EFTA00278329

A.MANUFACTURER • .. Fumed \ 3'. \ 3 I I — • .....: - ' ' ADDRESS • . • • VI. PRODUCTION FLIGHT TESTI? B.PRODUCTION BASIS (fleck spoficabb item/ . • • - . IPROc • '•N CERTIFICATE Win procksticm aninalts Humble ' TYPE CERTIFICATE ONLY • . . APPROVED PRODUCTION INSPECTION SYSTEM r ' • • C.GIVE QUANTITY OF CERTIFICATES REQUIRED FOR OPERATING NEEDS ti;--i"---a-So DATE OF APPLICATION • NAME AND TITLE (Prot et shift . . • , • • _ SIGNATURE • • • VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION FLIGHT TEST A.DESCRIPTION OF AIRCRAFT • REGISTERED OWNER • . • . ADDRESS • • BUILDER (Mats/ MODEL . . ...-. —.. o!'• ' • ' • ‘ i SERIALNUMBER • • rn" :• ... REGLSYBATON MARX • . l B.D ... l SCR IPTION OF FLIGHT N, FROM . . T .: • e , ..• VIA . . . •• - DEPARTURE DATE DURATION I C .CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT : - L PILOT CO-PILOT NAVIGATOR I OTHER afracifv/ ... • ' D.THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS: - • • . , .. S' . • • . . .-.. . . • ' • - •• ' . . .. . . - • f• - . . . " / • I • ' - .. .. • • .. . ' . • • i E. THE FOLLOWING RESTRICTIONS ARE CONSIDEREO NECESSARY FOR SAFE OPERATION IllsofittocAmont it necessary) . • • . . . : • • N. . • • ' . . F. CERTIFICATION — I hereby certify Mallon the regal for his agent/ of the aircraft described above; that the aircraft is registers, with the Federal Aviation Administration in accordance with Section 501 of this al Aviation Act of 1968, and applicable Federal Aviation Regulations; and that the airciaft has been inspected and is airworthy lot the flight dirtied. • DATE NAME AND 'NILE nhint or owe; . . SIGNATURE 2 top to— w A. Operating Limitations and Markings in Cornpliande with FAR 91.31 as Applicable G. Statement of Conformity, FAA Form 8130-9 (Attach when.requiredl H. Foreign Airworthiness Certification for Import Aircraft IA torch when requinxf 1 zw ot it 1-. X B ,Current Opeating Limitations Attached . . . I. Previous Airworthiness certificate Issued in Acmdanco with ' FAR 21.183 (d) CAR - !Original enschern t- It 0 et • 0... 2 ; C. Data, Drawings, Photographs. etc. (Amen soften required) X 3 4 et X D D. Current Weight end Balance Information Aviilable in Aircraft J . Current Airworthioass Certificate Issued in Accordance with -- FAR 21 191 (b) . so-Rye/ate& • 0 4 <Oil: E. Major Repair and Alteration. FAA 337 fIttsch when ',oz.:Trod) . ≥ X F. This Inspection Recorded in AircraftFtessords . . nY • .;:*: ,...kt tOrti llt.i lf>n r: ' '741;17.de , EFTA00278330

UNITED STATES OF AMERICA DEP4R•TMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD •AIRWO NESS CERTIFICATE 5. AUTHORit T AND BASIS FOR 1551JATICEJ -'1‘-----t- -=:" iTh \\\zi This airworthiness certik Ciel ohrtisfissued pursuen lie ire o) Aviation NO ok 958 and certifies that, os of the ' . dote of issuance. Ow oircrtift to."-rerhich issued hial-inirs•- • inipectvel and fogad cordage; to the type certificate therefor. to be in condition fed...sole opedstian,_dad.A6C-Isiers 'shown to Mak therequirements of the applicable reatatrhentivst and detailed oirworthines4 'code as-inracred by Alien i TO- TS Hors en Intermission& Civil Aviation, except as noted'herein. ' . .---..--7.: -/ Alai t Exceptions: TERMS AND CONDITIONS •  Unless sooner surrendered. 'statische). revolted, or a is m:notion this airworthiness certificate is Aective as long Or em KICH", performed in accordance with'Partyll.r 43, and 91 of the aircraft is registered in the Unitodekftes. Any olterotIon. roorodutlion. or misuse of this certificate prisonment not exceeding 3 years, or both. THIS CERTIFICATE ANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. . FAA Form 8100-2 (7 671 . PORMERLY FAA FORM 1362 EFTA00278331

1...try‘cr - . EFTA00278332

", • ..• .• r• v• ^-• DEPARTMENT 'UNITED STATES OF AFIERICIle OF TRANSPORTATION — FEDERAL AWATIONADMININTRATION SPECIAL AIRWORTHINESS CERTIFICATE: A CLASSIFICATION: EXPER . PURPOSE: gm 'S MANU- FACTURER ACTOR - - C FLIGHT CRON In ' TO D N— 97944.A S 7..4R NO. ibl. BUILDER a ii M liele11596 E DATE OF ISSUANCE rio 5 RY 6/24/84 OPERATING LIMITATIO Bil 5/ 4/4 11 /4 E A PART OF THIS CERTIFICATE SI PAIR E T a I"' ESIGNATION OR OFFICE NO. fli OPI1R ACE 1055 . Any &Imam. tvprcatortal. or mime of this oertacato may to potilhabie by n Enno con -- enthwg late tit not ninandlas 3 yawn, or beds. TIM WG ITHPICATE MUST BE DISPLAYED IN TEEL MR- CRAET EN ACCORDANCE IWITFI APPLICABLE; FEDERAL AVIATION REGITIATIONE. CRA B • tasatrt-IRROSir--t---- amTRI6•MerEltrolgati__LIRSIERF . ---311W r ed'..ertw•-• " EFTA00278333

. . • This airworthiness certificate' b head ttadat the authority of the Federal Aviation Ast a 1958 end the Federal Aviation Regulations (FoR). @ . • B This eh.. Linnets certificate authorise the coantrfacturer netted on the reverse side to conduct production flight tests, and only production flight tests, of Aircraft registered in his name. No person may conduct production flight tests order this certificate: (1) Carrying persons or property ter compensation or hiniu atallor (2) Coming persons not essential to the purpose of the flight. _ • . - . . c This sirworthinen certificate authorises the flight apecifisd ad the reverse side for the pur- pose shaven in Block A.. D .-.-4 E Tara airworthiness certificate certifies that. as of the date of issuance, the aircraft to which issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not ...neat the requirements nf the applicable comprehensive end detailed aft; worthiness code as provided by. Armes 8 to the Convention On International Civil Avis- - thin. No person may operate the aircraft described on the reverse side: (1) ercept in accord- ance with the applicable FAR and in accordance with creiclitions and limitations which run be prescribed by the Administrator a pan of this certificate; (2) over any foreign country • without the special permission of that country. Unless sooner nupentled, or revoked, this eirwortlxinets certificate is effective' for the duration and, under the conditions prescribed in FAR Part 21, Section 2L181 or 21217. . • - nen= `.." ---..'-' nff e .tr ....anIDAS•ITCASITTPTagniai ditei .... _ = .:• •7 C.% "n iCp . • ft- !.t•ir CilterwrazdarafiSr s7-.-Itera'SOF TWOI•nt• — — EFTA00278334