I. US Department

I. US Department of Transportation MAJOR REPAIR AND ALTERATION Federal Aviation (Airframe, Powerplant, Propeller, or Appliance) Administration , Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification/WA—P./06-U trg INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Gulfstream Aerospace Model G-IIB Serial No. 151 Nationality and Registration Mark N909JE 2. Owner Name (As shown on registration certificate) Hyperion Air, Inc. Address (As shown on registration certificate) 103 Foulk Road, Suite 202 Wilmington, DE 19803-3742 he alteration aircraft subject DATE identified herein complied to conformity inspection 2-1/4-4/ 2-6'D 7with applicable by a person FAA Inspector3. For FAA Use Only air-worthiness requirements and is approved authorized in FAR 43.7. only for the above described 4. Unit Identification 1 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. 1111111111111 U.S. Certified Mechanic 11JR439Y LIMITED AIRFRAME Foreign Certified Mechanic X Certified Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 2.---c//:, 7Signature of Authorized Individual Glenn Tietjen 7. Approval for Return to Service Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 was inspected in the manner prescribed by the APPROVED • REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of App oval or ejection 2.— e_c" a 7 Certificate or Designation No. I1JR439Y Signature of Authorized Individual Glenn Tieten _ FAA Form 337 (12-88) EFTA00278135 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.) Gulfstream Aerospace, G-IIB, SIN 151 I) Removed, refurbished and re-installed interior furnishings as outlined below: 2) Replaced the existing crew seat dress covers with Teddy & Arthur Edelman OLD-B3 Old Shrunken Buffalo Bull Leather, lot KA06FL and Aeristo Aerolamb Camel sheepskin, lot Y6M343. Attached Skandia, Inc. F.A.A./D.E.R. approved 8110-3, dated 01/24/07, work order 155311-07, document ID 74756, test ID 12NW-77971, DERY-405143-CE. Seatbelts were re-webbed by A.B.I. Attached SC-108B Certification / Packing list dated 01/19/07, to color coordinate. Each belt is tagged and identified as meeting FAA-TSO-C114, -C22F, or - C22G requirements. 3) Replaced the existing veneer on the entrance bulkheads with Carl F. Booth & Co. Elm Burl Veneer. Attached Skandia, Inc., F.A.A./D.E.R. approved 8110-3, dated 02/13/07, work order 156511-07, document ID 75004, test ID 60NW-6004, DERY-405020-CE. 4) Fireblocked and upholstered six (6) single cabin chairs, one (1) double seat, one (1) jumpseat, and potty seat with Teddy & Arthur Edelman OLD-B3 Old Shrunken Buffalo Bull Leather, lot KA06FL. Aircraft seat cushions have been fireblocked as per the requirements of 14 CFR, 25.853(c) Amendment 25 — 116 Appendix F Part II. Results of sample burn tests are documented on attached Skandia Inc. FAA/D.E.R. approved 8110-3, dated 02/09/07, work order 156074-07, document ID 74969, test plan 15724, DERY-410100-CE. Seatbelts were re- webbed by A.B.I. Attached SC-108B Certification / Packing list dated 01/19/07, to color coordinate. Each belt is tagged and identified as meeting FAA-TSO-C114, -C22F, or -C22G requirements. 5) Fireblocked and upholstered the UH aft divan assembly with Jeffrey Arnoff Dugally Beige Chenille Fabric. Aircraft seat cushions have been fireblocked as per the requirements of 14 CFR, 25.853(c) Amendment 25 — 116 Appendix F Part II. Results of sample burn tests are documented on attached Skandia Inc. FAA/D.E.R. approved 8110-3, dated 01/18/07, work order 153082-06, document ID 74710, test plan 15465. DERY-410100-CE. Seatbelts were re-webbed by A.B.I. Attached SC-108B Certification / Packing list dated 01/19/07, to color coordinate. Each belt is tagged and identified as meeting FAA-TSO-C114, -C22F, or -C22G requirements. 6) Replaced the existing carpet throughout the aircraft with Texstyle 58A, 58B, 58C custom wool carpet. Attached Skandia, Inc. F.A.A./D.E.R. approved 8110-3 dated 01/09/07, work order 154634-07, document ID 74508, test ID 12-19848, DERY-405143-CE. 7) Removed the existing cabin ALC fluorescent indirect lighting system and replaced with B/E Aerospace LVIII Elite LED Lighting System and replaced the galley and lavatory incandescent lights with B/E Aerospace 6800 LED Lighting as per International Jet Interiors wiring diagram, B/E Aerospace Cabin LED Lighting System Installation, JRW0706-WD. Attached Skandia, Inc. F.A.A./D.E.R. approved 8110-3, dated 02/14/07, DERT-830134-NE. 8) Modified the existing Cabin 14VDC Accessory Power Distribution System as per International Jet Interiors wiring drawing, JRW0707-WD, Rev I/R Cockpit 14VDC Power Receptacle Installation. Attached F.A.A. form 8110-3 dated 02/16/07 by F.A.A./D.E.R. DERT-636280-NM. 9) Replaced the footrest hydroloks on the six (6) cabin seats with P.L. Porter Controls Hydrolocks. Attached F.A.A. 8130-3, dated 01126/06, tracking number 536641, Authorization No. ODAR F601987NM. 10) All stitching is performed IAW International Jet Interiors Stitching Guide IJISG-1, rev. I/R. 11) All materials meet 14 CFR, 25.853 (a) Appendix F, Part I (a) (1) (ii). 12) Reference W.O. # 06264 on file at this agency for further information. 13) A logbook entry has been made reflecting this alteration. 14) A supplemental equipment list has been provided. 15) It has been determined that there is no significant weight change. 16) Passenger aisle width maintained per 14 CFR, 25.815. 17) The work described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. 18) No further entries. ❑ Additional Sheets Are Attached EFTA00278136 U.S. DEPARTMENT OF TRANSPORTATION . . . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 01/24/07 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream MODEL NO. • GlIB TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Skandia, Inc. International Jet Interiors LIST OF DATA IDENTIFICATION TITLE Work Order # 155311-07 Document ID 74756 Purchase 0rder _.# 2092 FLAMMABILITY TEST RESULTS REF:Skandia, Inc. Design Data # S155311 ..SPECIMEN .#1,Test specimens are 31N..12" compos4es consisting of Teddy & Arthur Edelman OLD-B3 Old Shrunken Buffalo Bull Leather Lot OKA06.FL sewn back to .bCk to Aeristo Aerolamb Camel Sheepskin Lot #Y6M343. Test specimens are representative of Crew Seat Dress Cover., REF TEST ID # 12NW-77971 "Flammability test witnessing only, does not constitute installation approval of the material." PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for S/N 151 APPLICABLE REQUIREMENTS (List specific sections) 14 CFR PART 25.853 (a) Amdt 25-116 Appendix F Part I (a)(1)(ii) CERTIFICATION -Under authority of appointment under Part 183 of have vested by direction of the Administrator and in accordance with conditions the Federal Aviation Regulations, data listed above and on attached sheets been examined in accordance with established procedures and found to comply Regulations. approval of these data these data and limitations numbered with applicable requirements of the Federal Aviation • ecommend 1 (We) Therefore Approve SIGNATURE(S) OF SI NATED ENGINEERING REPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) 0-j9' - DERY -405143-CE Structural Special Carin Demus FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION EFTA00278137 now • EFTA00278138 • U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 02/13/07 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream MODEL NO. GII TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT • Skandia, Inc. International Jet Interiors LIST OF DATA IDENTIFICATION TITLE Work Order # 156511-07 Document ID 75004 Purchase Order # 2139 FLAMMABILITY TEST RESULTS REF:Skandia, Inc. Design Data # S156511 SPECIMEN # I Test specimens are 3" x 12" composites consisting of AAR Composites 1/8" ATR-FP-12IF1 bonded to Carl F Booth & Co Elm Burl Veneer. Veneer is finished as per International Jet Interiors Process Specification #01IJINVIAB. Components are bonded together with Akzo Nobel 3M 8046 Top/Trim Adhesive. Test specimens are representative of Entrance Bulkheads., REF TEST ID # 60NW-6004 "FIammability test witnessing only, does not constitute installation approval of the material." PURPOSE OF DATA . Demonstration of compliance with material flammability requirements in support of Field Approval for S/N 151 APPLICABLE REQUIREMENTS (List specific sections) 14 CFR Part 25.853 (a) Amdt 25-116 Appendix F Part I (a)(1)(i) CERTIFICATION -Under authority of appointment under Part 183 have vested by direction of the Administrator and in accordance with conditions of the Federal Aviation Regulations, data listed above and on attached sheets been examined in accordance with established procedures and found to comply Regulations. approval of these data • these data and limitations numbered with applicable requirements of the Federal Aviation Recommend I (We) Therefore Approve SIGNATURE(S) OF D SI AT NGINEERING REPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) .nr----, DERY-405020-CE Structural Special Judy ns • FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION EFTA00278139 S EFTA00278140 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 02/09/07 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE GULFSTREAM MODEL NO. G-1159B TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Skandia, Inc. International Jet Interiors LIST OF DATA IDENTIFICATION TITLE Work Order # 156074-07 Document ID 74969 Purchase Order # 2126 FIREBLOCKING FLAMMABILITY TEST RESULTS REF: Skandia, Inc. Test Plan #15724 Rev IR Dated: 02/06/07 For PN's 15724-1, 15724-2, 15724-3 & 15724-4 Edelman Leather, OLD-B3 Old Shrunken Buffalo Bull, Dye Lot KA06FL Skandia, Inc. F/R Canvas Natural Skandia, Inc. DAX Graphite/Poly 26 ILD Skandia, Inc. Ethafoam 4101 PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Field Approval for S/N 151 APPLICABLE REQUIREMENTS (List specific sections) 14 CFR Part 25.853 (c) Amendment 25-116 Appendix F Part II 14 CFR Part 25.853 (a) Amdt 25-116 Appendix F Part I (a)(1)(ii) CERTIFICATION -Under authority of appointment under Part 183 have vested by direction of the Administrator and in accordance with conditions of the Federal Aviation Regulations, data listed above and on attached sheets been examined in accordance with established procedures and found to comply Regulations. approval of these data these data and limitations numbered with applicable requirements of the Federal Aviation •• Recommend I (We) Therefore Approve SIGNAT E(S) OF SIGNATED E N ERING EPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) •/ DERY-410100-CE Structural Special Donna J. arri FAA Form 0-3 (11-70) SUPERSEDES PREVIOUS EDITION EFTA00278141 • S. EFTA00278142 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION ; - STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 01/18/07 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATJON MAKE • GULFSTREAM MODEL NO. G1159B TYPE (Airplane, Radio, Helicopter etc.) Airplane _ NAME OF APPLICANT Skandia, Inc. International Jet Interiors LIST OF DATAIDENTIFICATION TITLE Work Order # 153082-06 Document ID 74710 Purchase Order # 2074 FIREBLOCKING FLAMMABILITY TEST RESULTS REF: Skandia, Inc. Test Plan #15465 Rev IR Dated: 01/10/2007 For PNs: 15465-1 & 15465-2 SKANDIA, INC.: DAX GRAPITE/POLY 26 ILD JEFFREY ARNOFF: FABRIC, DUGALLY, BEIGE, TREATED AT SKANDIA, INC. REF. TREATMENT #SKFP 152676 "Flammability test witnessing only, does not constitute installation approval of the material." PURPOSE OF DATA • Demonstration of compliance with material flammability requirements in support of Field Approval for S/N 151 APPLICABLE REQUIREMENTS (List specific sections) 14 CFR PART 25.853 (c) Amendment 25-116 Appendix F Part II 14 CFR PART 25.853 (a) Amdt 25-116 Appendix F Part I (a)(1)(ii) CERTIFICATION -Under authority of appointment under Part 183 of have vested by direction of the Administrator and in accordance with conditions and limitations the Federal Aviation Regulations, data listed above and on attached sheets numbered been examined in accordance with established procedures and found to comply with applicable Regulations. approval of these data these data requirements of the Federal Aviation 0 Recommend I (We) Therefore Approve SIGN URE(S) OF DE'SIGNATED ENGINEERI EPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) DERY-410100-CE Structural Special Donna J. Parrish FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION EFTA00278143 EFTA00278144 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 01/09/07 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE GULFSTREAM MODEL NO. GlIB TYPE (Airplane, Radio, Helicopter etc.) Airplane NAME OF APPLICANT Skandia, Inc. International Jet Interiors LIST OF DATA IDENTIFICATION TITLE Work Order # 154634-07 Document ID 74508 Purchase Order # 2070 . FLAMMABILITY TEST RESULTS REF:Skandia, Inc. Design Data # V154634 SPECIMEN #1 TEXSTYLE: CARPET, 58A, 58B, 58C, CUSTOM WOOL TO BE . , • • . • . • INSTALLED UNBONDED IN. AIRCRAFT MAIN CABIN, GALLEY, COCKPIT AND.LAV _, FLOORS , REF TEST ID # 12-19848 "Flammability test witnessing only, does not constitute installation approval of the material." PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for S/1•1 151 APPLICABLE REQUIREMENTS (List specific sections) .,.,. 14 CFR PART 25.853(a) Amdt 25-116 App F Part I (a)(1)(ii) CERTIFICATION -Under authority of appointment under Part 183 of have vested by direction of the Administrator and in accordance with conditions the Federal Aviation Regulations, data listed above and on attached sheets been examined in accordance with established procedures and found to comply Regulations. approval of these data these data and limitations numbered with applicable requirements of the Federal Aviation • Recommend I (We) Therefore X: Approve SIGNATURE(S) OF DESIGIATED ENGINEERING REPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) de,.A.1/g../ 01-7,P0-----DERY-405143-CE Structural Special Carin Demus FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION EFTA00278145 _ • •, • EFTA00278146 L.:130 v • v • . vv A. U.S, DERAR7SAENT-Or . 1 RA N'S PORTATION • . : TEDERALAOATIONADMINiSTRATIDN . STATEMENT OF COMPLIANCE WITH.THEPEDERAk.: -AVIATION.REGULATIONS OATE February 14, 2007 AIRCRAFT.OR AIRCRAFT COMPONENT IDENTIFICATION: MAKE. . Gultstream.Aerospace Corporation. MOOELNO • ' . . 3 HS TYPE 1)Ii!Pienel 41.r.010. "encirki.'ef0 Airplane NAME OF A.OPLICA NT International Jet Interiors • .LIST OF DATA IOWILEISAWN T1711 B/E Aerospace Inc,. Report dated Feb, 14, 2007 Drawing No. JRW0706-WD, Rev.I/R Dated 2/8/07 LVIII "Elite" LED, fluorescent lighting system replaceMent on aircraft # 151 GLIB (see attached report -10 pages) • 8/E Aerospace Cabin LED. Lighting System Installation Reference Documents: 1- inverter AL-5114 Installation InStruction AL-11026M, 2- Master ControllerInstallatibn Manual AL-11630M; Initial Rel;Oated 1/23/2007 3- TR Module Installation Manual AL-11625M, Initial Rel. Dated V26/2.007 4- Drawings; N©.: 6825 Rev. B, dated 1/30/2007. LE lighting unit; No. 81529 Rev. B., dated:12/30/20QT COntrollet Module; No'. 81528 Rev. :B, dated 1/29/2007, TR Module 5- Envl0rtriental Test Report No. STR-07006-1 .6, EMI Test Report STR-07906-2 , . This approval is fOrtrigineering•design data only. It indicates the data listed above demonstrates compliance only with the regUlations SpeCified.by.paragraph and. subparagraph listed Pelow:as "Applicable. Requirements". This form does constitute FAA • approval of all the engineering data necessary for substantiation of compliance to neceSsarYrequireMents for the entire alteration. This approval is subject to satisfactory ground functional check and ground EMI/RFI checks to be conducted by International Jet Interiors. puroose OF:nATA To support a major alteration on /N 151 APPUCAEILg REQUIREMENTS (List specificsections) • FAR 25,853(a) Arndt 115; 25.869 (a)(4)Aindt.11.3; 25.1301(?),(b),(c),(d); 25.1307(c) Amdt.72; 25.1309(a),(b),(d),(g) Amdt,41;.2 .1351a)(1) Amdt.72; 25.1353(a) ;(d)(1),(2),(3)Arndt.113; 25.1357(a):-25.1431(a)(c) Amdt:113; 25:1529.Amdt:54. CERTIFICATION:- kinciet eUthority vortad 1).y direction of the. AdniInistielee'and!•in aCCoreatxt ,w1h. CooriditioS under. Pari 153 of the. Federal Avlatien.RetiulAtlenS. data Ilsted.aboveand on' ttaciled StrielS•nurnberral accordonee vOn e.oiilished procedures and found to corn* with apoilc.ablefeoulrements of the Federal 0 Recommend approver of the data I (We) Therefore i.Approve thooe data end firnlatione of aPpOinimertf 1 filru 10 ha r: /Irian eirlairia In Avration:Regulatfons SICNATUREfSj OF DESIGNATE° ENGINEERING REFRESENTATNE(S) OES:GNATION NLIMBERS{S} CLASSIHCATION(S) Vito A. PUlera ati'-"--.DERT-830134 ,NE Systems and Equipment- Electrical & Mechanical. • FAA Form 81104 (11-?o) SUPERSEDES PREVIOUS COITION ELECTRONIC FORMAT OM) EFTA00278147 EFTA00278148 FEB-16-2007 15:29 From:BALL f UDC, U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 16 Feb 2007 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Gulfstream MODEL NO. Gl1B TYPE (Airplane, Radio. Helicopter. ofc.) Airplane NAME OF APPLICANT International Jet Interiors LIST OF DATA IDENTIFICATION TITLE JRW0707-WD Rev IR 2 Sheets dated 08 Feb 2007 Cockpit 14VDC Power Receptacle Installation Notes: 1. This Statement of Compliance addresses only the electrical aspects of the engineering design data in the referenced drawing. 2. This document documents a finding of compliance only for the regulations listed below in the APPLICABLE REQUIREMENTS box. Compliance to additional regulations may be required. 3. This document does not provide full FAA approval of the equipment installation. Additional engineering data may be required for approval. 4. This approval is valid for Gulfstream Model GIIB aircraft , tail number N909JE (SN 151) only. PURPOSE OF DATA To demonstrate compliance with applicable FARs in support of an aircraft modification documented in FAA Form 337. APPLICABLE REQuIREmENTS (List specific 'tenons) FAR 25.1301(a), FAR 25.1357(a) CERTIFICATION - Under authority vested by direction of the Administrator Part 183 of the Federal Aviation Regulations, data listed above and on anacneo established procedures end found to comply with applicable requirements of ERecommend approval of these data I (We) Tnerefore CZ Approve these data sno In accordance with conditions sneets numbered -NA- and limitations of appointment under have been examined in accordance with the Federal Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REP SENTATIVE(S) DESIGNATION NUMBERS(S) CLASSIFICATIONLS1 Systems Karl M. Frantz 7(4,4i DE RT-636280-NM and Equipment orm /3110-3 (I t-70) SUPERSEDES PREVIOUS EDITION ELECTRONIC FORMAT (7.00) EFTA00278149 I.) EFTA00278150 1 . Approving National Aviation Authority/Country: FAA/UNITED STATES 2.3 • • . Form Tracking Number: AUTHORIZATION RELEASE CERTIFICATE FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG 536641 4. Organization Name and Address: DECRANE AIRCRAFT SEATING CO., 701 MAPLE ST., P.O. BOX-129, PESHTIGO, WI 54157, USA do P.L Porter Controls, Inc., 3000 Winona Ave., P.O.Box 7722, Burbank, CA 91510-7722.USA. TSO C39b; TSO C127a . 5. Work Order/Contract/Invoice Num: .. 7. 0 2005-527 • 6. Item: 7 - Description: 8. Part Number: 9 . Eligibility:` 10. Qty: ii- Serial/Batch Number112. Status/Work 1 - HYDROLOK • SL02300-28 TSO Article: N/A .,... •:•‘....- . •,4•::. ,..,:.., T.*. ..5tn•-; V.:All 1-IZe• . 14.9..4.• !,tt",'-.. 50 5 1 5 0 1 9 • New . 13. Remarks THE PART SHIPPED UNDER THIS APPROVAL IS A SUB COMPONENT OF A FAA-PMA HIGHER A.fi.S.EMBLY. DIRECT SHIP AUTHORIZATION II:..;. EER DECRANE AIRCRAFT SEATING CO., 701 MAPLE ST., P.O. BOX 129, PESHTIGO, WI 54157, USA do P.L Porter Controls, Inc., 3000 Winona Ave., P.O.Box 7722, Burbank, CA 91510-7722 USA • ISO C39b; TSO C127a ' .,::'.,:• 14. Certifies the items identified above were manufactured In conformity to: • . . ... :.14 cFR.43:9 Return toSerVi4.• • • - . . . .. ,. .. . . . . :.- Other regulation specified in Block.t3..:7:•:. .....: • • , • • ..:, dertifiesthat iiii.10s Otneiirjte:s00:Ci4d in.iiiii;013;fthe work identifie.ii irBlack.1 and • .. described inbiock.i was accomplished. in ootofdanee with. Title 14; Code of Feder's! ..,.- - ...,... f,feguletione,iikti4Otiii.in.fesj5ect to thSt work, the itemsSieapkOVedfoi return: to Service..:: • - ...- -";::-.- -, ... . X Approved design data and are in condition for safe operation .e-:.1;:”•:::. I I Non-approved design data specified In Block 13. 15. Authorized Signature: ,••-•.. „..s.. / tr:j L. L.X_____,_ k.),, •:----,-- 16. Approval/Authorization No.: ODAR F601987NM . . •: irij .Authorized.Signaiiire:r I- •••• `'...1. - .... .. . • ,.. - - - -' . . . .. . _ 21„:APproval/Certificate NO.;-- .... 18. Date(m/d/y): JAN/26/2006 0>:. ...1.•!..,/p0:(-f;psi, pr:0nTni • ... 4 Date(mi ' • -•• • •-• 17. Name (Typed or Printed): Eva Alarcon User/Installer Responsibilities At is important to understand that the existence of this document alone does not automatically constitute authority to Install the part/component/assembly. • t . . :'Where the user/installer performs work in accordance with the national regulations of an airworthiness authority differem •••.,.rthe airworthiness authority of the country specified in Block 1, it is essential that the user/ins' Vier ensures that • his/her airworthiness axepts parts/components/assemblies from the airworthiness authority of the country specified i-. ..1. ,,, . !'. Statements in B' ! i and 19 do not consitutue Installation certification. In all cases, aircraft mainenance records r : .intain an installation certification issued in accordance with the national regulations by the ut, .'!'er before the • - aircraftcaircraftmay be :• i -.., i .. . ••...: EFTA00278151 %.- EFTA00278152 Aircraft pelts Inc. P.O. Box 845 2000 Anders Lane Kemah Texas 77565 FAA R.S. #: YB1R632K Packing Slip: 208 Ship To: PO: 2073 Ship Date: 1/19/2007 AIRCRAFT BELTS, INC. TM t"t.nt Sold To: International Jet Interiors • Ship Via:FedEx PI SO: 73092 -IRLO.f.1W.1; . antipc1446.- Ai* 6410:01, _ • . ekz4 1 1.00 EA 1.00 0.00 r5ptrps Description: Reweb Pac Sci 4pt Assy w/Inertia Reel # 210 / #12 FOB: ORIGIN Sales Person: Terri Phillips Page: 1 t'Ot fssewsiq, IR 2 2.00 EA 2.00 0.00 r4ptfps Description: REWEB PAC SCI 4PT FIXED HARNES # 210/ #12 IR 3 4.00 EA 4.00 0.00 r3ptrabi IR • Description: Reweb ABI.3.PointAssy. ..w/Jpertiayeel #.12 . . • - , • 4 7.00 EA 7.00 0.00 rlaabi IR Description: Reweb ABI Lap Belt # 210 5 1.00 EA 1.00 0.00 rlaabi-p IR Description: Reweb Plated ABI Lap Belt # 210 1 2 3 5 CERTIFICATION This is to certify that the above components have been manufactured/repaired and inspected in accordance with current Federal Aviation Regulations: ISO C-22 and/or TSO C-114 and found airworthy for service unless otherwise noted. The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsability of those desiring to install either on or within a specific type of class of aircraft to determine that the aircraft installation conditions are within the ISO standards. If not within the TSO standards, the article may be installed only if further evaluation by the applicant documents an acceptable installation and is approved by the administrator. Details of this manufacture/repair are on file at this facility. EFTA00278153 tit EFTA00278154 MAJOR REPAIR AND ALTERATION usloepariment (Airframe, Powerplant, Propeller, or Appliance) of Transportation Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identificaticg ib4,—/ INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instr tions 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 Model GULFSTREAM AEROSPACE G1159B Serial No. Nationality and Registration Mark 151 U.S.A. N909JE 2. Owner Name (As shown on registration certificate) :. HYPERION AIR INC. I s : 2. # • ,#§ • s :.• . : •• # z • cats) 3. For FAA Use Only 4. Unit Identification - 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME described in 1 X (As Item above) 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 AIRFRAME 1,3. RADIO 1,2,3. LIMITED AIRFRAME, & P/P LIMITED INSTRUMENT 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 Signature of Authorized Individual . . . . . , _ . . ---------- 8/20/04 John K. Urso, Inspector. 7. Approval for Return to Servi Pursuant Administrator BY to the authority given of the Federal Aviation persons specified below, the unit Administration and is identified in item 4 w nspected in the manner prescribed by the ❑ REJECTED r APPROVED 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 8/20/04Certificate or Designation No. EYKR782D Signature of Authorized Individual John K. Urso, Inspector. /- ZIA-6"-- FAA Form 337 (12-88) EFTA00278155 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.) GULFSTREAM - II (G-1159), S/N 151, REG N909JE, W/O 20985 INSTALLED AN ARTEX 406 MEGAHERTZ EMERGENCY LOCATOR TRANSMITTER (ELT) SYSTEM (ISO C126), IAW ARTEX C406-N MHZ EMERGENCY LOCATOR TRANSMITTER OPERATION, INSTALLATION AND MAINTENANCE MANUAL, DOCUMENT NO. 570-5060, REV B, AND THE FOLLOWING JET AVIATION DRAWINGS: WIRING DRAWINGS: • G2B-20895-370, REV IR, DATED 8/10/04, TITLED - EMERGENCY LOCATOR TRANSMITTER SYSTEM. REFERENCE F.A.A. FORM 8110-3, DATED 8/16/04 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM STRUCTURAL DRAWINGS AND REPORTS: • G2B-20895-1370, REV IR, DATED 8/9/04, TITLED - ELT EQUIPMENT INSTALLATION. • G2B-20895-1371, REV IR, DATED 8/9/04, TITLED - ELT ANTENNA INSTALLATION. • ER01489, REV IR, DATED 8/9/04, TITLED SUBSTANTIATION REPORT, ELT & EGPWS INSTALLATION FOR GULFSTREAM G1159B, S/N 151 REFERENCE FAA FORM 8110-3 DATED 8/9/04 BY STRUCTURES DER NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER ARTEX 406 MHZ EMERGENCY LOCATOR TRANSMITTER OPERATION, INSTALLATION AND MAINTENANCE MANUAL, DOCUMENT NO. 570-5060, REV B, WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: G2B-20895-080 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. 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 UPDATE REPORT NO O2B-20895-040 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN JET AVIATION DOCUMENT G2B-20895-050, TITLED - INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR ARTEX C406-N MHZ EMERGENCY LOCATOR TRANSMITTER. THERE ARE NO COCKPIT PROCEDURAL CHANGES OR FLIGHT MANUAL SUPPLEMENT DUE TO THIS MODIFICATION -------- - END --------------- ------- D Additional Sheets Are Attached O U.S. G.P.O 1990-761-753 EFTA00278156 4111.1.11 ME eiKnoN GE4WITH -, ; ;cFED .'7,::;a:Nsi.k..acsewit}s1114 .11. aK,10'449 16. Ina leaCh 'ittlra:/:<09 .40.ttrAelektlaCti EFTA00278157 I • EFTA00278158 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE August 9, 2004 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION ' MAKE Gulfstream MODEL NO. G1159B TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates LIST OF DATA IDENTIFICATION TITLE G2B-20895-1370 G2B-20895-1371 G2B-20895-1450 ER01489 ELT Equipment Installation, Sht 1-4, Rev IR ELT Antenna Installation, Sht 1-3, Rev IR Minor Deviation to STC ST02789AT Mk VIII EGPWS Equipment Installation, Sht 1-7, Rev IR Substantiation Report Substantiation Report - ELT & EGPWS Installation for Gulfstream G1159B, s/n: 151 Note: 1. This approval is for structural aspects only. 2. This approval is based on analysis and drawing review. 3. After the repair or alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of an alteration to Gulfstream G1159B, s/n: 151, TCDS Al2EA APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305 25.307 25.321 25.561 25.601 25.603 25.605 25.609 25.611 25.613 25.625 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation In accordance with established procedures I (1)1 Therefore by direction of the Administrator and in accordance with conditions Regulations, data listed above and on attached sheets numbered and found to comply with applicable requirements of the Federal Recommend approval of these data. Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Structural David E. Haralson Po.‘Evet. licerze.,__ DERT-810028-NE , FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01489.doc EFTA00278159 I EFTA00278160 REVISION STATUS REV LTR REV BY DESCRIPTION APPROVAL DATE (No data herein shall be deemed to have been approved by any regulatory agency). v. . iates, Ltd. ‘I'l _SWF 11117177711A1 am eac n rport CRS-EYKR782D West Palm Beach, FL 33406 PROPRIETARY NOTICE: This document contains specifications and/or data, technical material, proprietary information that are the sole property of JET AVIATION ASSOCIATES, LTD, to be held and treated by its recipient on a confidential basis and is not to be shown or disclosed to any unauthorized organization or person without the written authorization of JET AVIATION ASSOCIATES, LTD. Woric Order No.: 20895 MODEL: TITLE: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR ARTEX C406-N EMERGENCY LOCATOR TRANSMITTER Gulfstream G-1159B NAME DATE Prepared By: T. CARR 08/10/04 Checked By: J. URSO 08/16/04 S/N: 151 Q/A: J. URSO 08/16/04 Engineer: N/A N/A DOCUMENT NO.: G2B-20895-050 REV: IR SCALE: NONE SHEET: 1 OF 9 Approved: N/A N/A EFTA00278161 I EFTA00278162 , 0 MAJOR REPAIR AND ALTERATION US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identificati INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instr i s 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 Model GULFSTREAM AEROSPACE G1159B Serial No. Nationality and Registration Mark 151 U.S.A. N909JE 2. Owner Name (As shown on registration certificate) Address As shown on r: .istration certificate HYPERION AIR INC. 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME • described X (As in Item 1 above) 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. U.S. Certified Mechanic CRS EYKR782D AIRFRAME 1,3. RADIO 1,2,3. LIMITED AIRFRAME, & P/P LIMITED INSTRUMENT Foreign Certified Mechanic .-......., x Certificated Repair Station Manufacturer D. I cert have furnished unit(s) identified in item 4 above and described on the reverse or attachments hereto Part 43 of the U.S. Federal Aviation Regulations and that the information been made in accordance with the requirements of herein is true and correct to the best of my knowledge. Date Signature of Authorized Indivi ual....., -Jo-tm K. Urso, Ins----ector. -- - - — it - -- 7. Approval for Return to Sery Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 inspected in the manner prescribed by the ❑ REJECTED 4 APPROVED 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 8/20/04 Certificate or Designation No. EYKR782D Signature of Authorized Individual John K. Urso, Inspector._ /(--• 66v-- FAA Form 337 (12-88) EFTA00278163 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.) GULFSTREAM - II (G-1159), S/N 151, REG N909JE, W/O 20985 ACCOMPLISHED AN UPGRADE TO THE EXISTING HONEYWELL MST-67A TRANSPONDERS FOR THE INCORPORATION OF FLIGHT ID. REMOVED TRANSPONDERS PIN 066-01143-0601 (TSO C112) AND INSTALLED TRANSPONDERS P/N 066-01143-2101 (TSO C112). REMOVED HONEYWELL TRANSPONDER CONTROL UNIT P/N 071-01507-3603 (TSO C112) AND INSTALLED TRANSPONDER CONTROL UNIT P/N 071-01618-0021 (TSO C112, C I 18, C119b). REFERENCE AC20-41A, SUBSTITUTE TECHNICAL STANDARD ORDER AIRCRAFT EQUIPMENT. NO WIRING OR STRUCTURAL ALTERATIONS WERE ACCOMPLISHED. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER HONEYWELL MST67A MODE S TRANSPONDER SYSTEM MANUAL 006-00681-0006 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: G2B-20895-080 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. 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 UPDATE REPORT NO G2B-20895-040 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS REQUIRED PER F.A.R. 25.1529 ARE CONTAINED IN JET AVIATION DOCUMENT G2B-20895-051. THERE ARE NO COCKPIT PROCEDURAL CHANGES OR FLIGHT MANUAL SUPPLEMENTS DUE TO THIS ALTERATION. -END ❑ Additional Sheets Are Attached O U.S. G. P.O 1990-761-753 EFTA00278164 REVISION STATUS REV LTR REV BY DESCRIPTION APPROVAL DATE (No data herein shall be deemed to have been approved by any regulatory agency). ATE!' RIAERFICIII . . ' s, Ltd. a m Bea n Airport West Palm Beach, FL 33406 CRS-EYKR782D This document contains specifications ASSOCIA TES, LTO. to be held and organization or PROPRIETARY NOTICE: the sole property of JET AVIATION or disclosed to any unauthorized LTD. and/or data, technical material, proprietary information that are treated by its recipient on a confidential basis and is not to be shown person without the written authorization of JET AVIATION ASSOCIATES, Work Order No.: 20895 MODEL: TITLE: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR THE INSTALLATION OF THE HONEYWELL PS-578A MODE S/TCAS CONTROL PANEL Gulfstream G-1159B NAME DATE Prepared By: T. CARR 08/10/04 Checked By: G. L. KARR 08/16/04 S/N: 151 Q/A: J. URSO 08/19/04 Engineer: N/A N/A DOCUMENT NO.: G2B-20895-051 REV: IR SCALE: NONE SHEET: 1 OF 5 Approved: N/A N/A EFTA00278165 • EFTA00278166 e MAJOR REPAIR AND ALTERATION US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office lc,ra_lioryt INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for structions 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 Model GULFSTREAM AEROSPACE G1159B Serial No. Nationality and Registration Mark 151 U.S.A. N909JE 2. Owner Name (As shown on registration certificate) A. :, ,, i•ir or :A.' . .IPI :IC . e) HYPERION AIR INC. 3. For FAA Use Only - 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME .. described in X (As Item 1 above) ----- -. 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. U.S. Certified Mechanic CRS EYKR782D AIRFRAME 1,3. RADIO 1,2,3. LIMITED AIRFRAME, & PIP LIMITED INSTRUMENT Foreign Certified Mechanic X r- Certificated Repair Station Manufacturer D. I certi o the unit(s) identified in item 4 above and described on the reverse or attachments hereto have ements 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 8/20/04 Signature of Authorized . Individual — ---. — / 1- - -------- - e---(A.--y^ John K. Urso, Inspector. 7. Approval for Return to Se e Pursuant Administrator BY to the authority given of the Federal Aviation persons specified below, the unit Administration and is identified in item as inspected in the manner prescribed by the ❑ REJECTED APPROV 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 8/20/04 Certificate or Designation No. EYKR782D Signature of Authorized Individual John K. Urso, Inspector. /('CiA FAA Form 337 (12-88) EFTA00278167 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.) GULFSTREAM - II (G-1159), S/N 151, REG N909,1E, W/O 20985 REMOVED THE EXISTING HONEYWELL MK I GROUND PROXIMITY WARNING SYSTEM AND INSTALLED A HONEYWELL MK VIII ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) IN ACCORDANCE WITH JET AVIATION ASSOCIATES, LTD. STC NO. ST02789AT PER JET AVIATION ASSOCIATES, LTD., MASTER DRAWING LIST, DOCUMENT NO. G1159-19760-010, REV A. DATED 01/30/04, TITLED - MASTER DRAWING LIST FOR THE INSTALLATION OF THE MK VIII ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) IN THE G-1159 SERIES AIRCRAFT. CONCURRENTLY ACCOMPLISHED RADIO ALTIMETER UPGRADE BY REMOVING THE # 1 AND # 2 COLLINS RADIO ALTIMETER ALT-50 AND INSTALLING COLLINS RADIO ALTIMETER ALT-55B IAW COLLINS ALT-50/55 RADIO ALTIMETER SYSTEM INSTALLATION MANUAL 523-0775918- 004118 DATED 4/11/97. DEVIATIONS TO THE STC ARE DOCUMENTED ON THE FOLLOWING JET AVIATION DRAWINGS. WIRING DRAWINGS: • G2B-20895-450, REV IR DATED 8/13/04, TITLED - MINOR DEVIATIONS TO STC ST02789AT MK VIII EGPWS SYSTEM WIRING DIAGRAM. • G2B-20895-506, REV IR, DATED 8/13/04, TITLED - MINOR DEVIATIONS TO STC ST02789AT AUXILIARY ANNUNCIATOR SYSTEM WIRING DIAGRAM. REFERENCE FAA FORM 8110-3 DATED 8/16/04 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM STRUCTURAL DRAWING AND REPORT: • G2B-20895-1450, REV IR DATED 8/5/04, TITLED - MINOR DEVIATIONS TO STC ST02789AT MK VIII EGPWS EQUIPMENT INSTALLATION. • ER01489, REV IR, DATED 8/9/04, TITLED SUBSTANTIATION REPORT, ELT & EGPWS INSTALLATION FOR GULFSTREAM G1159B, S/N 151. REFERENCE FAA FORM 8110-3 DATED 8/9/04 BY STRUCTURES DER NO. DERT-810028-NE. THE MK VIII EGPWS WAS FUNCTIONALLY TESTED PER JET AVIATION GROUND TEST PROCEDURE DOCUMENT NO. G1159-19760-060 REV. A DATED 01/30/04, TITLED - CERTIFICATION GROUND TEST PROCEDURE FOR THE MK VIII EGPWS, WITH NO DISCREPANCIES. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS REQUIRED PER F.A.R. 25.1529 IS CONTAINED IN JET AVIATION ASSOCIATES, LTD. DOCUMENT NO. G1159-19760-050, REV. IR, DATED 11/19/03. THE REQUIRED FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT DOCUMENT NUMBER G1159-19760-100, REV. IR, DATED FEB 09 2004 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END ❑ Additional Sheets Are Attached O U.S. G.P.O 1990-761-753 EFTA00278168 Anita, Atatts of jknuriat pepartment of Zranspartztlian gtbtral cikfliritiorc gaiministration Supplant/Ifni Type Terlifirate oeio4jecale essaedlotiVel,9216,e ST02789AT tes, Ltd. Palm Beach, FL 33406 _ceirleXe4.4ea4.64-aeanfe 1;s 44, *Aise Aujg"),e).• 44i4a,eorivywedaci-coae-44'471444144, -44-aisii-eillitiAWAt ccs .ysearXedievrws ',see& ezeiveoWdecizeos .v9a-eirmeysis elgirel 25 e/ Federal Aviation aiov:sa,g;od.e- .9;y7e Fe..4;4.74, Al2EA ,A6,718 Gulfstream Aerospace Corporation ../#20.41.• G-1159, G-1159A & G-1159B Series g"-1••04:91' e/Tf" "",""' Installation of a Honeywell Model MK VIII Enhanced Ground Proximity Warning System (EGPWS) in accordance with Jet Aviation Master Drawing List (MDL) G1159-19760-010, Rev. A, Dated January 30, 2004 or later FAA approved revision. ...Wthiezz.tievs4 ezepeinvu/44O,9 ".s... FAA Approved Flight Manual Supplement (AFMS) for Gulfstream Aerospace Corp. Models G-1159, G1159A & G-1159B Series Aircraft with Honeywell Model MK VIII EGPWS, Jet Aviation Document No. G1159-19760-100, Rev. IR, Dated February 9, 2004, is a required part of this STC. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. ces.-4/eoale czaatZ4 Jurpo"1.44, eaveic.42 a, ,0,.< Wale .3zuvinoelesm JeAyseved. ~Weider Iewmisalay, dale ss ode.~4se e,s4de.‘„i6. 46 ,AL/Z174/%3€4Z4710V. VW, le cy,gereo September 19, 2003 ros:isreed. 07.41 oi,s;ssuaekre February 9, 2004 grah, a'nevwfool. gri,..aetzejgae;TA5s, .Adme:44.V.sale ,990, c/46 6,1414. gffled;" (w-gnature) jot Melvin D. Taylor Manager Atlanta Aircraft Certification Office (Title) Any alteratico or this certificate is punishable by • fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. SPA Poem $110-1(10-6I) PA= 1 of 1 PAGIS This certificate ray be transferred in accordance with fAR 21.47. EFTA00278169 I . EFTA00278170 SET Rff711778111 SUPPLEMENTAL TYPE CERTIFICATE N°. ST02789AT BY USING THIS SUPPLEMENTAL TYPE CERTIFICATE, YOU AGREE TO THE FOLLOWING TERMS. IF YOU DO NOT AGREE TO THE TERMS OF THIS AGREEMENT, PROMPTLY RETURN THE SUPPLEMENTAL TYPE CERTIFICATE, MAINTENANCE INSTRUCTIONS, AND FLIGHT MANUAL SUPPLEMENT TO JET INCORPORATED FOR A FULL REFUND. Jet Aviation Associates, Ltd (JET) grants you (the "Licensee") the right to use the Supplemental Type Certificate ("STC") referenced above on the Gulfstream G-1159B aircraft Serial N°. 151 , (the "Aircraft"). You may not use the STC and related materials, including drawings, flight manual inserts, instructions or other materials for any other aircraft or for any other purpose. COPYRIGHT. The STC is owned by JET and is protected by United States copyright laws, other United States laws, and international treaty provisions. Therefore, you must treat the STC like any other copyrighted material. One (1) copy of the written materials accompanying the STC package may be made for each aircraft Serial Number listed above. CONFIDENTIALITY. Licensee will protect the STC Data Package, whether in storage or in use, with the same degree of care as the Licensee uses to protect its own confidential and proprietary material against public disclosure and unauthorized use, but in no case with any less degree than reasonable care. Licensee will keep the STC Data Package confidential and will not disclose it to anyone other than employees of the Licensee reasonably having a need to have access to it for the purposes specified above, and such disclosure to them shall be made only under conditions of strict confidentiality. LIMITED TRANSFER RIGHTS. You may not sell, rent or lease the STC, except that you may transfer your license to the STC to any purchaser of the Aircraft. INDEMNIFICATION AND LIMITATION OF LIABILITY. Licensee shall have no recourse against JET for, and hereby agrees to defend, indemnify and hold harmless JET, its shareholders, directors, officers, employees and agents, against any and all claims (whether in contract, tort, or otherwise, including negligence of any degree) for or in respect of any loss (including loss of use and/ or profit), expense, liability, property damage and/or bodily injury (including death) which may at any time be suffered or incurred (for any reason whatsoever) by Licensee and/or any third parties (including persons or any property being carried in the Aircraft in any capacity whatsoever), directly or indirectly ar