NOTICE Weight andtalance 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. Nk. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001, W.O. 16236, PAGE 2 OF 2. THE FOLLOWING REQUIRED ANNUNCIATORS WERE LOCATED ON THE EXISTING PILOT AND COPILOT'S INSTRUMENT PANEL ADJACENT TO THE EADI UNITS: FMS HDG THE FMS IS IN HEADING SUB-MODE. (COLOR: BLUE) GPS INTEG GPS INTEGRITY IS OUTSIDE OF THE ALLOWABLE LIMIT FOR A PHASE OF FLIGHT (2.0-NM EN ROUTE, 1.0-NM TERMINAL AND APPROACH TRANSITION, AND 0.3-NM FINAL APPROACH SEGMENT). SEE SECTION III, ABNORMAL PROCEDURES. (COLOR: AMBER). THE ADDED ANNUNCIATORS ARE DIMMED AND TESTED USING THE EXISTING PILOT AND COPILOT ANNUNCIATOR COUPLERS. THESE UNITS HAVE BEEN MODIFIED USING JET AVIATION MODIFICATION NO. 33-39-02-1, CAPT. AND F/O ANNUNCIATOR COUPLER MODIFICATION, DATED 04/12/01, REFERENCE FAA FORM 8110-3, DA IED 05/29/2001 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21, DATED 19 MARCH 2001 WITH NO DISCREPANCIES NOTED. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 1 OF 5, DATED 06/19/2001, WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. 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. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK, INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECIRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTAT J.FD IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLY WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.I3-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. 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 FOR CONTINUED AIRWORTHINESS AS REQUIRED BY FAR 25.1529 IS DETAILED IN THE UNIVERSAL AVIONICS CORP. UNS-1D FLIGHT MANAGEMENT SYSTEM TECHNICAL MANUAL NO. 34-60-09, DATED AUG 15/97. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333- CE. THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236-100, REV IR, SHEETS 1 THRU 9, DATED ne 2-1 i 20 0 I HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END K Additional Sheets Are Attached EFTA00277680

"fr .4 EFTA00277681

Oak Jet Aviation Associates Ltd. BIdg. 1515 Perimeter Rd. Palm Beach Int'l Airport West Palm Beach, FL 33406 FAA CRS EYKR782D Document No. B727-16236-100 AFM Supplement to The Boeing Company 727-31 Serial No. 20115 FAA Form 337 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N908JE SERIAL NO.: 20115 WITH DUAL UNIVERSAL AVIONICS FLIGHT MANAGEMENT SYSTEMS (UNS1-D) INSTALLED This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VOR/DME from the Collins No. 1 and No. 2 VORJDME systems in accordance with manufacture's Installation and Checkout Manual No. ?4-60-09, Rev. 2. dated August 15, 1997 or later approved revision and FAA Form 337, dated- 7/2/0/ 0 The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FAA Approved: Federal Aviation Administration Flight Standard District Office - 17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 JUN 2 1 2001 FAA Approved Date: Page 1 of 9 EFTA00277682

Os 1 EFTA00277683

May-29-01 01:59P N 3 Curt-an 352 243 1011 P _ 06 L DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05129/2001 -, AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane. Radio. Helicopter. etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-293, Initial Release, dated 04/16/01 B727-16236-410, Initial Release, dated 04/10101 B727-16236-411, Initial Release, dated 04/15/01 33-39-02-1, Initial Release, dated 04112/01 FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT NO. 1 FLIGHT MANAGEMENT SYSTEM NO. 2 FLIGHT MANAGEMENT SYSTEM CAPT AND F/O ANNUNCIATOR COUPLER MODIFICATION PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N90BJE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581 (a)(b)(d) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 25.1381 (a)(b) FAR 25.1322 (b)(c) FAR 25.1431 (a)1131(c) CERTIFICATION - Under authority vested by direction data listed above and on attached sheets 'mothered NONE of the Admiwistrator and in accordance laid. conditions and Ensiles-tows of appoinemeat ander Part I23 of the Federal Awl-mien IRegulatiosts, have been remained in accordance with establistard procedures sod fooad to comply with applicable requirements of the Federal Aviation these data & Equipment Aspetts, Design Approval Only. Does Not Constitute Installation Approral) Regulations. 0 Retommeoil approval of I (We) Therefore El Approve these data (Systems SIGNATURES F D LUG TE GLNEE RETRESENTATIVE(S) DESIGNATION NUMBERIS) CLASSIFICATTON(S) ,Q DERT-510087-NM Systems & Equipment No an J. an 01111 _ 110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME: SC-727-FMS.DOC EFTA00277684

a • EFTA00277685

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 1, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION • MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE • B727-16236-1261 B727-16236-1410 • • AT-855/RTA-880 Antenna Installations, Sht.1-7, Rev A • Dual FMS WI RTU Equipment Installations, Sht 1-6, Rev IR Note: - 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 . . . CERTIFICATION - Under authority vested by direction of the Administrator .and in accordance with conditions under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I ('Therefore Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) David E. Haralson .a.are. 14,-.1.-- DERT-810028-NE Structural FAA FOITTI 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01202.cloc EFTA00277686

a i EFTA00277687

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 18, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL B727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation LIST OF DATA IDENTIFICATION TITLE Jet Aviation Engineering Drawing No. B727-16236-1441, Dtd. 5/29/2001, Rev. A END END GPS Antenna Installation Beoing B727-31, N908JE, S/N 20115 END END END END END END END END Note: The certification evaluation of structure. Structural Repairs on Notes: basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 6/18/2002. aspects only of the above listed data are approved is valid for the aircraft model and serial number is based on structural analysis on file at DER Services office in Ft. Lauderdale, FL. No. B727-31 Serial No. 20115 1) The structural herein. 2) This approval listed below 3) This approval corporate Model PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LIST SPECIFIC SECTIONS) 25301, 25303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition appointment under Part 183 of 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 requirements of the Aviation Regulations. Recommend approval of these data I (We) Therefore P1 Approve these data and limitations of have Federal SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau DERT-510024-CE Structures FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITIO N DER SERVICES PROJECT NO. 2001-082 EFTA00277688

16 v i EFTA00277689

a 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 Ont Office Identification 5-0- FS`DO - i 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructi s 9 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 exc ed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type •- Manufacturer ,,, 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic X Certificated Repair Station Manufacturer AIF & 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 7/2/01 • Signature of Authorized Individual John K. Urso. Inspector. 16, U -V 7. Approval for Return to Service k 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 K REJECTED C4 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 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assuranc FAA Form 337 (12-88) EFTA00277690

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.) BOEING 727-31, SIN 20115, N908JE, W/O 16236. INSTALLED 2 EA NEW GARMIN GPS ANTENNAS P/N 011-00134-00 (TSO C129A). 1 EA AT FUSELAGE STATION 284.8, BL 0.0, AND 1 EA FUSELAGE STATION 934.3 RBL 4.56, PER JET AVIATION DRAWING B727-16236-1413, REV IR, DATED 6/5/01 TITLED - DUAL AUXILIARY GPS ANTENNAS INSTALLATION. REF F.A.A. FORM 8110-3 DATED 6/6/01 BY STRUCTURES D.E.R. NO. DERT-510394- CE. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-IB, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SF.I.FCTED AND INSTALLED LAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-IB, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. 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 LAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN ENGINEERING REPORT JMER-836, REV IR, DATED 6/10/01. REFERENCE FAA FORM 8110-3 DATED 6/11/01 BY STRUCTURES DER NO. DERT-510394-CE. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277691

••• yr 44t.c.c000v..)4 0 AgiA U ri't S • to 002 U.S. DEPARTMENT OF TRANSPORTATION PEDERAL AVIATION ADMINISTRATION STATEMENT OP COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Tune 6, 2001 • AIRCRAFT OR AIRCRAFT COMPONENT WENTIFICATION MAKE BOEING MODEL NO. 8727-3I TYPE (Airplane. Reif*, Helicopter, etc.) Airplaii NAME OP APPLICANT I ul, ...----A-kl../ViaaalLasicKjares ...., , LIST OP DATA IDENTIFICATION TITLE B727-16236-1413 IR Sheets 1— 3 (6/5/01) END DRAWING — DUAL AUXILIARY GPS ANTENNAS INSTALLATION NOTE: Approval for the structural aspects related to the above design data will be covered by a separate Form 8110-3 which will be issued for the Proof of Structure and will include required inspection items) to ensure Continued Airworthiness . . associated with this modification. END END PURPOSE OF DATA To provide a record of design approval of the above data applicable to B727-31, SIN 20115, Registration No. N90&1E. for manufacturing and confortnity. See NOTE above. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.6601 FAR 25.609 FAR 25.603 FAR 25.611 FAR 25.605 FAR 25.613 CERTIFICATION - Under authority vetted by direction of the Administrator arxi in 2,c,cordanee wick cordidons sad limitations of appointment under part 183 of az Pcderal Aviation Regulatiorn. ellta listed above and on attached slims numbered IVA have been examined in sem-dame with #=011101(4 procodures and found m comply with applicable requirements of !be Federal Aviation Regulations. I * Therefore 0 Recommend approval of these dota X Approve Mete data (Sec NOTE above) siGNATurtr.(s) OF DESIGNATED REPRESENTATIVE(S) DESIGNATION NUNIBMS) CLASSIFICATION(S) DERT - 510394 - CE STRUCTURES Kenneth W. Thompson - FAA 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION sheet 1 of 1 EFTA00277692

a %I EFTA00277693

• .. U.S. DEPARTMENT OF TRANSPORTATION. - FEDERAL.AVIATION ADMINISTRATION . , STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 11, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BDEilia /172L-31 EURELANE.---IgLAYialisnlAsurdatcda11_, MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT LIST OF DATA IDENTIFICATION TITLE JMER-836 IR Dated 06/10/01 • ENGINEERING REPORT — STRUCTURAL SUBSTANTIATION - DUAL AUXILIARY GPS ANTENNA INSTALLATION ON A BOEING B727-31 AIRCRAFT, S/N 20115 NOTE: The operator of B727-31 aircraft S/N 20115 modified by drawing B727-16236-1413 dated 6/5/01 issued at no revision, is required to incorporate in the Airworthiness Limitations Section of the Instructions for Continued Airworthiness applicable to the existing Maintenance Program, an inspection item at a frequency not to exceed 3700 flights to detect signs of distress (0.25 inch or smaller crack and/or working rivets) common to the GPS antenna installation as detailed in drawing B727-16236-1413. Refer to FAR PART 25 Appendix H and Report JMER-836 IR page 4.1 (CONCLUSIONS) for instructions. PURPOSE OF DATA To provide a record of design approval of the above data as applicable to B727-31 S/N 20115 and to show compliance to the following FAR's: . . APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 FAR 25.307 FAR 25.605 FAR 25.613 FAR 25.303 FAR 25.571 FAR 25.609 FAR 25.625 FAR 25.305 FAR 25.603 FAR 25.611 Chlt111-ICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered N/A have been examined in accordance with I (k) Therefore established . X procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data Approve these data (Structural aspects only) - . SIGNATURE(S) OF DESIGNATED REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 60- 7- DERT - 510394 - CE . STRUCTURES Kenneth W. Thompson .. • FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION sheet 1 of 1 EFTA00277694

.1. 11 EFTA00277695

O f ' MAJOR REPAIR AND ALTERATION OS Deoartrraant 0 Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office identification 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 BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item 1 above) X POWERPLANT PROPELLER APPLIANCE Type • • _ Manufacturtr \ ,.. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMTIED EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic x Certificated Repair Station Manufacturer A/F & 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 7/2/01 Signature of Authorized Individu ,6- John K. Urso. Inspector. (1,,,_.,- 7. Approval for Return to Servi 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 0 APPROVED • REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EY1CR782D Signature of Authorized individual Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 (12-88) EFTA00277696

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.) BOEING 727-31, S/N 20115, N908.1E, W/O 16236. INSTALLED A NEW KGS ELECTRONIC MODEL UC-28-14, 28 VDC TO 14 VDC CONVERTER AND THREE POWER OUTLETS IN THE COCKPIT IN ACCORDANCE WITH KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL AND ADVISORY CIRCULAR 25-10 (INSTALLATION OF MISCELLANEOUS NON REQUIRED ELECTRICAL EQUIPMENT) USING THE FOLLOWING JET AVIATION DRAWINGS SUBSTANTIATED BY F.A.A. FORM 8110-3 RESPECTIVELY WIRING DRAWING: • B727-16236-352, REV IR, DATED 5/25/01, SHEETS 1 & 2, TITLED - 28-14 VDC CONVERTER WIRING DIAGRAM. REFERENCE F.A.A. FORM 8110-3 DATED 6/7/01 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-CE. STRUCTURAL DRAWING: • B727-16236-1352, REV IR, DATED 6/6/01, SHEETS 1 THRU 5, TITLED - 28-14 VDC CONVERTER EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3 DATED 6/10/01 BY STRUCTURES DER NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. 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. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/20011 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.I3-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. 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-IB, CHAPTER 10, SECTION 2 AND AC 43.I3-2A, CHAPTER 1 PARAGRAPH 9. THERE IS NO CHANGE TO THE MANUFACTURERS MAINTENANCE FOR CONTINUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277697

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 06/07/2001 ... AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE " B727-16236-352, Initial Release, dated 05/25/01 B727-16236-580, Initial Release, dated 05/25/01 B727-16236-600, Initial Release, dated 05/25/01 • ---- 28-14 VDC CONVERTER WIRING DIAGRAM CABIN NO. 2 60 Hz SYSTEM SPARE WIRING (PROVISIONS) PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 25.1353 (a)(b) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c) FAR 25.1309 (a)(b)(g) FAR 25.1431 (a)(b)(c) FAR 25. 1322 (b) FAR 25.1529 FAR 25.1351 (a) CERTIFICATION - Under authority vested by direction data listed above and on attached sheets numbered NONE have of the Administrator and in accordance with conditions and limitations of appointment under Part la3 of the Federal Aviation Regulations. been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Regulations. K Recommend approval of I (We) Therefore E3 Approve these data (Systems )• SIGNATURE( ESIGN NGIN REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) - DERT-510087-NM Systems & Equipment - No an an J. ran FAA Foim 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 90I-6I3 FILENAME SC-727-CAB-PWR.DOC EFTA00277698

4 J EFTA00277699

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 10, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter,etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1352 28-14 VDC Converter Equipment Installation, Sht 1-5, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I ( )34 Therefore Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICAT1ON(D Structural David E. Haralson P.,..,,e. 1-4,-.1.-- DERT-810028-NE FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01209.doc EFTA00277700

aa a EFTA00277701

4 2 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 Identification ()— r5D6-i7 7/- INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructs 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 ex d $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only • 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer \ ,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG. Foreign Certified Mechanic x Certificated Repair Station Manufacturer A/F & 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 7/2/01 Signature of Authorized Individual John K. Urso. Inspector. 7. Approval 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 ns in the manner prescribed by the lID REJECTED 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 7/2/01 , Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance. ae " . FAA Form 337 (12-88) EFTA00277702

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with .alf 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.) BOEING 727-31, SIN 20115, N908JE, W/O 16236. INSTALLED A UNITRON 60 HZ CONVERTER P/N PS-62-66D AND 26 EA CABIN OUTLETS PER UNITRON 60 HZ CONVERTER INSTALL MANUAL NO. PS-62-66D-6. THIS MODIFICATION WAS ACCOMPLISHED PER THE FOLLOWING JET AVIATION DRAWINGS WHICH ARE SUBSTANTIATED BY F.A.A. FORM 8110-3 RESPECTIVELY WIRING DRAWING: • B727-13236-580, REV IR, DATED 5/25/01, SHEETS 1 THRU 5, TITLED - CABIN NO. 2 60 HZ SYSTEM REFERENCE FAA FORM 8110-3 DATED 6/7/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS: • B727-16236-1580, REV IR, DATED 6/11/01, SHEETS 1 THRU 7, TITLED - CABIN NO. 2 60 HZ EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3, DATED 6/13/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. 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. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-:1B, CHAPTER 11, SECTION 4. ELECIRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16, ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. 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.I3-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. THERE IS NO CHANGE TO THE MANUFACTURERS MAINTENANCE FOR CONTINUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277703

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE • 06/07/2001 -.. AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-352, Initial Release, dated 05/25/01 B727-16236-580, Initial Release, dated 05/25/01 B727-16236-600, Initial Release, dated 05/25/01 , 28-14 VDC CONVERTER WIRING DIAGRAM CABIN NO. 2 60 Hz SYSTEM . SPARE WIRING (PROVISIONS) . PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 25.1353 (a)(b) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c) FAR 25.1309 (a)(b)(g) FAR 25.1431 (a)(b)(c) FAR 25. 1322 (b) FAR 25.1529 FAR 25.1351 (a) CERTIFICATION — Under authority voted by direction data listed above and on attached sheets numbered NONE have of the Administrator and in accordance with conditions and limitations of appointment under Part IS3 of the Federal Aviation Regulations. been examined in accordance with established procedures and found to comply with applicable requirements or the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Regulations. El Recommend approval of I (We) Therefore 0 Approve these data (Systems siGNA7-0 £SIG G REPRESENTATIVES) DESIGNATION NUMBER(S) CLSSIFICATIONS) 11-ele,--- DERT-510087-NM Systems & Equipment No an J. ran AA Form 8110-3 (11-70) sUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME SC-727-CAB-PWR.DOC EFTA00277704

a • EFTA00277705

• DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 13, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter,etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1580 Cabin #2 60 Hz Equipment Installation, Sht 1-7, Rev IR Note: • 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I ( X Therefore 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 1,-;4Oae. ilicied......--- DERT-810028-N E FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01210.doc EFTA00277706

4k • `V EFTA00277707

No 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 O ly Office Identification c0-- r5DO - 1 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instr ions 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 xceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer ‘,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic X Certificated Repair Station Manufacturer A/F & 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 7/2/01 . Signature of Authorized Individual John K. Urso. Inspector. r\ 4- 16-'6(----! — 7. Approval for Return to Servige Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 wa inspected in the manner prescribed by the APPROVED III REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D ..... Signature of Authorized Individual 1 Ronald K. Bystrom. Manager Quality Assuranc FAA Form 337 (12-88) EFTA00277708

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.) BOEING 727-31, S/N 20115, N9083E, W/O 16236. INSTALLED AN AIRCELL ATG.01 FLIGHT PHONE SYSTEM CONSISTING OF AN ANTENNA P/N CI-5000, A TRANSCEIVER P/N 900002-2, and AN ANTENNA MATCHING UNIT P/N 83518, 4 EA HANDSETS P/N 400-10035-001 AND 4 EA HANDSET CRADLES P/N 400-10038-001. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-13236-330, REV. IR, DATED 4/30/01, SHEETS 1 THRU 3, TITLED - AIRCELL ATG.01 AIR / GROUND TELEPHONE REFERENCE FAA FORM 8110-3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1330, REV. A, DATED 5/29/01, SHEETS 1 THRU 4, TITLED - AIRCELL ATG.01 AIR / GROUND TELEPHONE ANTENNA INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/18/01, BY STRUCTURAL D.E.R. NO. DERT-510024-CE. • B727-16236-1331, REV. IR, DATED 5/24/01, SHEETS 1 THRU 6, TITLED -AIRCELL EQUIPMENT INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/3/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER AIRCELL ATG.01 FLIGHT PHONE SYSTEM INSTALLATION MANUAL REV IR, DATED 6/11/99 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-IB, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. 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. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. _ AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.I3-1B, CHAPTER 11, SECTION 4. FT FCTRICAIJELECIRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-IB, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-IB SECTION 16. ELECIRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. 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. PER THE AIRCELL ATG.01 FLIGHT PHONE SYSTEM MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT API-ECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333-CE. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS INSTALLATION. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277709

--M4y-29 - 01 01:59P N J Curran 352 243 1011 P C.) / DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05129/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane. Radio, Helicopter. etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-330, Initial Release, dated 04/30/01 • - - - • AIRCELL AGT.01 AIR/GROUND TELEPHONE PURPOSE OF DATA In support of major alteration to Boeing 727-31. serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1357 (a)(c) FAR 25.869 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) FAR 25.1351 (a) CERTIFICATION - Under sithoriry . eyed by direction data kited ibtwc sad** tinseled sheen niseslweed NONE or tht Administrator and is setordsset will clisdielons and /imitations et" 'pp:amine/se taedtr Tan 113 *fibs Federal Atistis• ;Ululation:4 have bets emainintd in aceordsnce with reublishtel peiscrchirts and Amid to esertrily with applicabh rtquirttnents et the Fedmri Aviation these data & Equipment Aspects. Design Approval Only, DIM Not Constitute Installation Approval) &Dilations. O Recommend approval of I (We) Therefore 1 Approve these data (Systems SIGNATURE ESIGNA GINEERI PRESENTATIVE(S) DESIGNATION N UM ILERM CLASSIFICATIONS) !at--. DERT-510087-NM Systems & Equipment No n J. C n EFTA00277710

o EFTA00277711

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 18, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL B727-31 TYPE Oftplane, RaSe, Iftlicopra: ac.) Airplane NAME OF APPLICANT Jet Aviation LIST OF DATA 1DEN fIFICALLUN It ILL Jet Aviation Engineering Drawing No. B727-16236-1330, Dtd. 5/29/2001, Rev. A END END Aircell AGT.01 Air/Ground Telephone Antenna Installation Beoing B727-31, N908JE, S/N 20115 END END END END END END END END Note: The certification evaluation of structure. Structural Repairs on tlotes: basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 6/18/2002. aspects only of the above listed data are approved is valid for the aircraft model and serial number is based on structural analysis on file at DER Services office in Ft. Lauderdale, FL. No. B727-31 Serial No. 20115 1) The structural herein. 2) This approval listed below 3) This approval corporate Model PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LIST SPECIFIC SECTIONS) 25.301, 25.303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CF.RTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets number been examined in accordance with established procedures and found to comply with applicable requirements of Aviation Regulations. Recommend approval of these data 1 (y) Therefore Fil Approve these data and Ii • tions of have the ederal SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBERS) CLASSIFICATION(S) Robert J. Belgau 19 0/276415 e.---- -. DEBT-510024-CE Structures FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001-082 EFTA00277712

I EFTA00277713

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 3, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radfo, Helicopter,etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE 8727-16236-1270 B727-16236-1331 . Argus 5000/CE Moving Map Equipment Installation Sht 1-5, Rev IR Aircell Equipment Installation, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority under Part 183 of the Federal Aviation in accordance with established procedures I ( X Therefore vested 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 REPRESENTATIVES) DESIGNATION NUMBER(S) CLASSIFICATION(S) Structural David E. Haralson Pe-,:fe. /4,-d._ DERT-810028-NE FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01207.doc EFTA00277714

a NO EFTA00277715

DEPARTMCNT OF TRANSPORTATION • . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 'HAKE BOEING MODEL NO. 727-31 TYPE (Airlakoc. Radio, Helicopter, ad) AIRPLANE NAME OF APPLICANT JET AVIATION • LIST OF DATA IDENTIFICATION TITLE. A.T.E. INC. STRUCTURAL REPORT No. ATE6I 12001 BOEING 727-31 S/N 20115, AERO-M SATCOM ANTENNA INSTL., UPPER B.S. 360-390; GPS ANTENNA INSTL., UPPER B.S. 312-328; AIRCELL AGT.01 ANTENNA INSTL., LOWER B.S. 400-420 DAMAGE TOLERANCE ANALYSIS; SR 1-31, REV. (IR) • NOTE; REQUIREDINSPECT1ONS AT'T'ACHED 20115 THESE DATA APPLY ONLY TO BOELNG 727-31 S/N . PURPOSE OF DATA TO APPROVE DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-3 I S/N 20115 1 APPLICABLE REQUIREMENTS (List spainc cations) . - FAR 25.571 (STRUCTURAL ASPECTS ONLY) • . CERTIFICATION — Under of appointment under Part 183 have authority vested by direction of the Administrator and in accordance with conditions and of 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 Recommend approval of these data Approve these data limitations • . I of l requirements of the Federal Aviation Regulations. I (Ye) Therefore i SIGNATURE(S) OF DESIGNATED ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATIONS) DERT-510333-CE STRUCTURAL • • • • . FAA Form 8110-3 (I t.70) SUPERSEDES PREVIOUS EDMON cro 901.613 EFTA00277716

• •• it EFTA00277717

MAJOR REPAIR AND ALTERATION O us Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Onl Office Identification 5 0— F 5 Do — 17 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructs 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 ex red $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 . Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type . Manufacturer ‘,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG. Foreign Certified Mechanic x Certificated Repair Station Manufacturer A/F & 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 7/2/01 Signature of Authorized individual John K. Urso. Inspector. laJ-- -- 7. Approval for Return to Service Pursuant Administrator BY to the authority given of the Federal Aviation persons specified below, the unit Administration and is identified in item 4 was _p_ected in the manner prescribed by the U REJECTED APPROVED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 (12-88) EFTA00277718

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.) BOEING 727-31, S/N 20115, N908JE, W/O 16236. ACCOMPLISHED AN UP-GRADE TO THE EXISTING HONEYWELL WEATHER RADAR SYSTEM FROM PRIMUS 870 TO PRIMUS 880. REMOVED THEl 1 & 2 WC-870 CONTROLLERS P/N 7008471-803 AND INSTALLED WC-880 CONTROLLERS P/N 7008471-405 (TSO C63c), REMOVED THE WU-870 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7012640-902 AND INSTALLED NEW WU- 880 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7021450-801 (TSO C63c). INSTALLED A HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM CONSISTING OF AN LP-860 PROCESSOR P/N 7011822-904 (TSO C110) AND AN AT-855 ANTENNA PIN 7014062-901 (TSO C110). THE LIGHTNING SENSOR SYSTEM INTERFACES WITH THE PRIMUS 880 RADAR SYSTEM THRU THE # I & 2 WC-880 CONTROLLERS. RELOCATED EXISTING SECURITY SYSTEM ANTENNA P/N DMC57-1 TO THE TOP OF THE RADAR ANTENNA & RECEIVER / TRANSMITTER UNIT. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-16236-260, REV. IR, DATED 5/29/01, SHEETS 1& 2, TITLED - WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) REFERENCE FAA FORM 8110-3 DATED 6/7/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. • B727-16236-261, REV. IR, DATED 4/10/01, SHEETS ITHRU 3, TITLED - HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM REFERENCE FAA FORM 8110-3 DATEDS/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1261, REV. A, DATED 5/30/01, SHEETS 1 THRU 7, TITLED - AT-855/RTA-880 ANTENNA INSTALLATIONS REFERENCE F.A.A. FORM 8110-3, DATED 6/1/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. • B727-I6236-1262, REV. IR, DATED 5/21/01, SHEETS 1 & 2, TITLED - LSZ-860 LIGHTNING SENSOR EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3, DATEDS/28/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER HONEYWELL PRIMUS 880 RADAR SYSTEM INSTALLATION MANUAL NO. 34-42-12, REV 3, DATED 2/15/00 AND THE HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM INSTALLATION MANUAL NO. 34-41-50, REV 5, DATED 2/15/01 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO. B727-16236-080, REV IR, DATED 6/19/01 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 ELFCTRICAL LOAD ANALYSIS UPDATE REPORT B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH 43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-IB, CHAPTER 4, SECTIONS I, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER II, SECTION 4. ELECTRICAIJELECIRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-IB, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. 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-IB, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN HONEYWELL PRIMUS 880 RADAR SYSTEM INSTALLATION MANUAL NO. 34-42-12, REV 3, DATED 2/15/00 AND THE HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM INSTALLATION MANUAL NO. 34-41-50, REV 5, DATED 2/15/01. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277719

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-260, Initial Release, dated 05/29/01 , k... WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) • PURPOSE OF DATA •In support of major alteration to Boeing 727-31, serial number 20115, registration•number N980JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) . FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION — Under authority vested by direction data Fisted above and on attached sheets numbered NONE have of the Administrator and in accordance with conditions and limitations of appointment ander Part 183 orate Federal Aviation Regulations, been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Regulations. El Recommend approval of I (I.Ve) Therefore X Approve these data (Systems SIGNATU F DESIGN NG INE INC REPRESENTATIVE(S) DESIGNATION NUMBERS) CLASSIF/CAT/ON(S) DERT-510087-NM Systems & Equipment Nor an. J. ran . FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME SC-727-RDRDOC EFTA00277720

I EFTA00277721

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 06/07/2001 r AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE , Boeing • MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION . TITLE B727-16236-260, Initial Release, dated 05/29/01 i.. WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N980JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) . FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION - Under authority vested by direction data listed above and on attached sheets numbered NONE have of the Administrator and in accordance with conditions and Etnitatimis of appointment under Part I &I of the Federal Aviation Regulations, been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Regulations. K Recommend approval of I (We) Therefore X Approve these data (Systems SIGNATU F DESIGN GINE G REPRESENTATTVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) • DERT-510087-NM Systems & Equipment Nor an J. ran FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME: SC-727-REIRDOC EFTA00277722

• EFTA00277723

May-29-01 01:58P N J Curran 41, ••=mowm..1 • :352 2L1-:3 1O11 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, ctc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-261, Initial Release, dated 04/10/01 - . HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM • PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 26.1357 (a)(c) FAR 25.869 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) _ FAR 25.1351 (a) CERTIFICATION - trader authority vested by direction dm) ram' aticre mid *a ttutitrd Skeels sumbered NONE of the Administratsr sad is accordance with cooditivos and limitations of appointment under Parr ILI artist Federal Avisiien Regulations, tune Ices east:sized is setordaset with esiablished procedures sad found to comply with applicable rectoiroueom .f the Fed eTht Avialie • these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Rttoilatlikt- O Recommend approval of I I (We)Therefore 0 Approve these data (Systems SIGNATU FD EN ERING RETRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION'S) —•TED 1 .1 &17- ---..- DERT-510087-NM Systems & Equipment Nor an . urran FAA Form 8110-3 (11.70) SUPERSEDES PREVIOUS EDMON GPO 901-613 FELENAME: SC-727-LTOSNSRDOC EFTA00277724

I EFTA00277725

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 1, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio, Helicopter, etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB - LIST OF DATA IDENTIFICATION TIRE B727-16236-1261 AT-855/RTA-880 Antenna Installations, Sht 1-7, Rev A B727-16236-1410 Dual FMS WI RTU Equipment Installations, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA . authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I Therefore ' Approve these data. , .. SIGNATURE(S) OF. DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) ,,.:, : CLASSIFICATION(S) •••..'$1,- David E. HaralOn P,-.2(e. ii,,,,z.-I-,' DERT-810028-NE --.7=7 - Structural -.-.4:-. -4, ' ,;:,s:4, . 447 • • :1•,: k• •44,-,44 . • - -• ,c-,"4•.-- • -.. FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01202.doc EFTA00277726

• EFTA00277727

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 B727-16236-1342 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I 0,tX Therefore 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) David E. Haralson Pc- t.., re /iced-46-- DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION L ER01205.doc EFTA00277728

• EFTA00277729

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 B727-16236-1342 ._ • LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR Aero-M SATOOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation in accordance with established procedures I 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) David E. Haralson P.,- e. // ,-1..,.--- DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01205.doc EFTA00277730

lr ft EFTA00277731

00 4 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 Identification 50- fsbo- 17 i INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instruc ' ns 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 BOEING Model 727-31 . Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 , . 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer \ s. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic X Certificated Repair Station Manufacturer AJF & _LIMITED 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 7/2/01 • Signature of Authorized Individual John K. Urso. Inspector. 1e---c' 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 w inspected in the manner prescribed by the C.4 APPROVED ■ 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 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance. FAA Form 337 (12-88) EFTA00277732

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.) BOEING 727-31, S/N 20115, N908.1E, W/O 16236. ACCOMPLISHED A TCAS CHANGE 7 UPGRADE TO THE EXISTING HONEYWELL TCAS II SYSTEM PREVIOUSLY INSTALi.ED UNDER PAGE AVJET CORPORATION STC SA3094SO DATED 8/24/93. REFERENCE F.A.A. FORM 337 DATED 8/25/93. THE TCAS PROCESSOR P/N 4066010-904 WAS MODIFIED TO P/N 4066010-910 (CUSTOMERS UPGRADED UNIT) IN ACCORDANCE WITH TIMCO MASTER DRAWING LIST 01T012L001, REV IR, DATED 5/21/01. REFERENCE F.A.A. FORM 8110-3 DATED 5/21/01 BY SYSTEMS AND EQUIPMENT DER NO.DERT-510239-CE. THE TCAS II CHANGE 7 PROCESSOR WAS INSTALLED AND TESTED IN ACCORDANCE WITH TIMCO ENGINEERING ORDER DOCUMENT 01T012E006, REV IR, DATED 5/21/01 WITH NO DISCREPANCIES. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE AIRCRAFT EQUIPMENT LIST WAS AMENDED AND ENTERED IN THE AIRCRAFT RECORDS. AIRWORTHINESS DIRECTIVE 94-01-04 AMENDMENT 39-8786 IS N/A TO THIS INSTALLATION BY PROCESSOR P/N. THERE IS NO CHANGE TO THE AIRCRAFT WEIGHT AND BALANCE. THERE IS NO CHANGE TO THE AIRCRAFTS MAINTENANCE FOR CONTINUED AIRWORTHINESS REQUIREMENTS DUE TO THIS INSTALLATION. THE REQUIRED F.A.A. APPROVED HONEYWELL INC, TCAS II FLIGHT MANUAL SUPPLEMENT DOCUMENT TCAS-APPS-0294, REV A, DATED 3/21/00 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277733

communications Aviation Communications & Surveillance Systems 21111 N. 19[11 Avenue Phoenix, AZ 85027-2708 602-436-7070 Fax: 602-436-6899 May 16, 2001 TIMCO 623 Radar Road Greensboro, NC 274 Attn.: Mr. Gregg Stutes Re: Letter of Authorization to use technical data Dear Mr. Stutes, This letter is to authorize TIMCO ("Recipient") to use the following technical data owned by L-3 Communications Corporation — Aviation Communications & Surveillance Systems (L-3) for the limited purpose indicated here below. The technical data subject to this Letter of Authorization (`date) is the L-3 developed data used to apply for the following FAA certifications: Supplemental Type Certificate STC SA4S34NM, as defined by ML4070349, for B727 aircraft. L-3 Authorization to use Data is limited to the following B727 aircraft tail number, namely: • B727 SIN 20115 L-3 Authorization to use Data is granted hereby for the sole purpose to provide the Recipient with technical information for its internal use and engineering review purposes. The Recipient recognizes L-3' s proprietary rights in Data and will limit its disclosure to a need-to-know basis for its employees. The Recipient will not use Data for any other purposes than the internal use and engineering review purpose established for this Authorization. The Recipient will not sell, license, rent, market, transfer, assign, distribute, or otherwise disclose to any third party, exploit or permit any other use of Data. L-3 does not provide any warranty whatsoever on Data, whether express, or implied, or implied by law, including but not limited to merchantability and fitness for any particular purpose_ EFTA00277734

I I EFTA00277735

In no event shall L-3 be liable for. • Any direct, incidental, indirect, special or consequential damages including but not limited to loss of use, revenue or profit, even if L-3 has been advised, knew or should have known of the possibility of such damages; or • Damages caused by the Recipient's failure to perform its obligations and responsibilities; or • Claims, demands or aeons against the Recipient by any other party. The term of this Authorization is one (1) calendar year from its date. If during such term L-3 believes that its proprietary rights in Data are being infringed or injured or otherwise are at risk, L-3 reserves the right to terminate Authorization hereunder and, upon notice to Recipient, request the Recipient to discontinue any further use of Data. Upon termination of Authorization hereunder, the Recipient will either destroy or return Data in its possession and notify L-3 that no further use of Data will take place. For any communication concerning this Authorization, please contact F.W. (Bill) Lynch, Certification Engineer: Phone: (602) 436.2421 Fax: (602) 436.6899 E-mail- [email protected] PIease, countersign this Letter of Authorization and return it to us as follows: original by mail (with the original signature of your authorized representative); a copy by fax to the undersigned. Thank you for your interest. S E.W. (Bill) L ch Agent for L-3 Communications, ACSS EFTA00277736

I I EFTA00277737

United gRatts graica Bepartment of Zransportation—fidtral aviation administration supplemental Zppe Certificate Y .2€21,..e..ezpitt-eur4 43.4ezed-io Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 A3WE Boeing 727-100 Series 25 Federal Aviation gLi' di'n'94-;& -- ---611 '.6CAanf e': Installation of Provisions only for a Honeywell TCZ-910 TCAS II System in accordance with Page Avjet Master Drawing List MDL-91- 41, Initial Release, dated November 19, 1991, or later FAA approved revisions. /'7m-tat This approval should not be extended to other airplanes 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 of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. zdte7a- ca, irv.e# / Az.n/e/Azzr- rre 44.eziyi.ende44.cw,LW, c14-7724nale z.' -cfa zik,wea &,e.11,214:14,/iy, //it • Cat in e3 ik t9 ‘41:Araidirtiz&im,ilezirte:nc.:Ilran'er-n, October 21, 1991 January 15, 1992 !Lk peZtJa,i: iinei4w./i•r hn Tigue (Signature nager, Atlanta Aircraft Certification Office (Title) Any alteration of this certificate is punishable by a.fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred in accordance with F.-1R 21.47. FAA folua 8110-2 (10-68) EFTA00277738

r I EFTA00277739

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE -67'24/0/ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-100 TYPE (AIRPLANE, RADIO, HEUCOPTER, ETC.) Airplane NAME OF APPLICANT TIMCO LIST OF DATA IDENTIFICATION TITLE TIMCO Master Data List, 01T012L001 Rev IR Dated 5/21/01 - Honeywell TCAS II Change 7 Software Upgrade for a Boeing 727-100 END OF DATA - - - . • PURPOSE OF DATA To document and approve the installation of a TCAS Change 7 in a Boeing 727-100 aircraft. STC SA4834NM is the approval basis for this installation. APPLICABLE REQUIREMENTS (Listspedricsections) FAR 25.1301 (a), (c) v - • CERTIFICATION - Under appointment under Part 183 of have authority vested by direction of the Administrator and in accordance with conditions the Federal Aviation Regulations, data listed above and on attached sheets numbered been examined in accordance with established procedures and found to Regulations approval of these data these data and limitations of comply with applicable requirements of the Federal Aviation 1 ) Therefore 0 Recommend ... Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) • CLASSIFICATION(S) Robert McClellan 14 DERT-510239CE System & Equipment FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION • GPO 901-613 EFTA00277740

• III EFTA00277741

TIMCO ENGINEERED SYSTEMS, I.. u, "WO N 5,40 CommY A TITLE: HONEYWELL STC / FAA PROJECT NO.: ENGINEER: P. FERGUS MASTER DATA LIST • TCAS II CHANGE 7 SOFTWARE UPGRADE SA4834NM / 650259 AIRCRAFT TYPE: FORM NO.: EN•0003 DATE: 01/01/00 MDL NO. 01T012L001 REV/DATE: IR / 5/21/01 BOEING 727-100 APPROVAL: ROBERT MCCLELLAN SHEET 1 OF 1 DOCUMENT NUMBER REVISION LTR DATE TITLE SHT 01T012C002 IR 5/21/01 HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 ISSUED vim 2 2 zttl wool collinot. 1 Th'sda's'Pr'Perv'''PrglIe0V: rTritTa:,','°iTtezierrdsarazix=sovr',d,==sur,Veotr=unThsc=roarnTdV,===.1Ler,:mgte=1,72;ebs=t7V-I"E"'"er""s`e"'In'and Copyright (C) 2000 TIMCO Engineered Systems, Inc. 011.012L0015 Stock No.: 091100108 EFTA00277742

I • EFTA00277743

TIMCO ENGINEERED SYSTEMS. !sc. CONFIGURATION DOCUMENT AN AWVI $.13 CO/MWY A TITLE: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 ENGINEER: P. Fergus APPROVAL: Robert McClellan Form No.: EN-0008 Date: 01/01/00 . CFG NO, 01T012C002 REV/DATE: IR/ 5121/01 SHEET 1 OF 1 I. CONFIGURATION DATA A. APPLICABLE MDL: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE # 01T012L001 B. EFFECTIVITY ISSUED 2 2 1. BOEING 727-100 SERIAL NO. 20115 MAY 20 C. DESCRIPTION CION.MEta CONTROL 1. THIS INSTALLATION WILL CONSIST OF USING STC SA4834NM AS THE APPROVAL BASIS TO PERFORM THE TCAS CHANGE 7 MODIFICATION TO THE TCAS COMPUTER UNIT, D. DEVIATION FROM PREVIOUSLY APPROVED DATA , 1. NONE Items marked with an asterisk (*) are for manufacturing and certification and will not be supplied. If required, the documents will be sent directly to the customer's certification authority only after TIMCO receives assurance that their confidentiality will be protected. DOCUMENT REVISION NUMBER LTR DATE TITLE SHT 01T012E006 IR 5/21/01 Installation of a Honeywell TCAS II CU with Change 7 in a Boeing 727-100 6 01T012R007 IR 5/21/01 Description and Substantiation of a TCAS II Change 7 Installation 2 'This data Is the properly of. and proprietary to, TIMCO Engineered Systems, Inc, and Is restricted for use by designated persons, firms or corporations with whom contracts have been entered Into. User agrees to Indemnify TIMCO Engineered Systems, Inc. and to hold It hornless against any claim arising by reason of the possession or use thereof. lis unauthorized use and duplication Is prohibited, and it Is protected under an unpublished copyright' Copyright (C) 2000 TIMCO Engineered Systems. Inc. •1 1:1017012 Jet AviattonN0IT012C002S.doc Stock No.: 091100403 EFTA00277744

1 F • e EFTA00277745

TIMCO ENGINEERED SYSTEMS. Pro. AmAwn. SALES Cosawm A ENGINEERING ORDER Form No.: EN•0002 Date: 01/01/00 E.O. TITLE: Installation of a Honeywell TCAS II CU with Change 7 in a Boeing 727-100 E.O. NO.: 01T012E006 AIRCRAFT: Boeing 727-100 REV: IR DATE: 5/21/01 ISSUED MAY 2 2 21101 DOCUMENT. CONTROL. INITIAL RELEASE REVIEWS R Fergus PkEPARE , -,',:- .,,:,.-''.:,! David Thornton tilEtKEtit ii-A:: ::T-f4aV :„ - •• .. :•-,',,,,.., Richard Cunningham ,QA--13gyIE -.. .-:-:,, -----=: s 41;-,,EE,_.;.•-,--,;: - -? Robert McClellan ',_, , Rtiv-E- 1 - : -:•.; -,. ..x...4-,N.-5.-s3,----A,_,-,- --,,,,. ,--44-*: ... . ..,, _........ .. •. ...,...... :•••••• •,-,•:-:.,,.„•,,,i--:•••-,4•:•.-!..--,-_,-,-,...t,„ TIMCO ENGINEERED SYSTEMS, INC. 623 Radar Road Greensboro, North Carolina 27410 Telephone: (336) 668-4410 This data is the property of, and proprietary to. TIMCO Engineered Systems. Inc. and is restricted for use by designated persons, firms or corporations viith whom contracts have been entered Into. User agrees to indemnify TIMCO Engineered Systems, Inc. and to hold it harmless against arty claim arising by reason of the possession or use thereof. Its unauthorized use and duplication is prohibited, and it is protected under art unpublished copyright,' Copyright (C) 2000 TIMCO Engineered Systems. Inc. 01T012E0065 Stock No.: 091100106 EFTA00277746

S a EFTA00277747

Honeywell Inc . 21111 North 19th Ave. Phoenix, .AZ 85027 Spec. No. TCAS -APPS- 0294 AFM SUPPLEMENT General TCAS/ACAS Applications FAA APPROVED WHEN EQUIPPED WITH HONEYWELL TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM ( TCAS II ) This supplement must be attached to the FAA Approved Airplane Flight Manual for aircraft that have been modified by installation of the Honeywell Traffic Alert and Collision Avoidance System (TCAS II) in accordance with a Honeywell STC (see SECTION I). The information contained in this document supplements and supersedes the basic manual only in those areas listed. For limitations, procedures, and performance information not contained in this supplement, consult the basic Airplane Flight Manual. FAA APPROVED Manager, Flight Test Branch, ANM-160L Federal Aviation Administration Los Angeles Aircraft Certification Office Tranport Airplane Directorate Date EFTA00277748

r 4.• • EFTA00277749

I 0 MAJOR REPAIR AND ALTERATION US Departmwt of Tran_sportatIon (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use O ly Office Identification So- r-sDo- f 7 cik)' INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instreitions 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 keed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type • • Manufacturer . s. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LTMIT11I2 EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic ---, x Certificated Repair Station Manufacturer AIF & 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 7/2/01 . Signature of Authorized lndi idual John K. Urso. Inspector. L,,, /C. 7. Approval for Return to Servl Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 w s inspected in the manner prescribed by the CI APPROVED III REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual , Ronald K. Bystrom. Manager Quality Assuranc / FAA Form 337 (12-S8) EFTA00277750

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.) BOEING 727-31, S/N 20115, N908JE, W/O 16236. INSTALLED A UNIVERSAL AVIONICS TT-3000 SERIES AREO-M SATCOM SYSTEM PER UNIVERSAL AVIONICS AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM INSTALLATION MANUAL NO. 23-15-02 DATED 3/7/01. SYSTEM CONSISTS OF 2 EA HANDSETS, 1 EA ANTENNA, 1 EA HIGH POWER / LOW NOISE AMP AND THE SATELLITE DATA UNIT. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-13236-340, REV. IR, DATED 4/30/01, SHEETS 1 THRU 3, 'I I1LED -1T-3000 AERO-M AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM. REFERENCE FAA FORM 8110-3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1340, REV. A, DATED 5/29/01, SHEETS 1 THRU 5, TITLED - AERO-M SATCOM ANTENNA INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/18/01, BY STRUCTURAL D.E.R. NO. DERT-510024-CE. • B727-16236-1342, REV. IR, DATED 5/2I/01, SHEETS 1 THRU 7, TITLED - AERO-M SATCOM EQUIPMENT INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 5/28/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. SYSTEM TESTED PER UNIVERSAL AVIONICS INSTALLATION MANUAL FOR TT-3000 SERIES AERO-M, DOCUMENT 23-15-02, DATED 3/7/01 WITH NO DEFECTS NOTED. NOTE: UNIVERSAL AVIONICS SERVICE BULLETIN NUMBER 10101.00-23-2669, BLOCKING OF BREATHING HOJ RS IN SATCOM ANTENNA P/N 10101-00, DATED 7/25/00, WAS INCORPORATED AT ANTENNA INSTALLATION. THIS HAS NO EH.ECT OF THE STRUCTURAL OR MECHANICAL INSTALLATION OF THE ANTENNA. AN EMI TEST, REPORT NO. B727-16236-080, REV IR, DATED 6/19/01 WAS CONDUCTED AND THE INSTAII.FD 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 B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/401 WAS COMPLETED IN ACCORDANCE WITH 43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC 43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED THE INSTALLATION CONFORM TO AC 43.13-1B, CHAPTER 5, SECTIONS 1 AND 2, CHAPTER 7, SECTIONS 1, 2,4 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 43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED IAW AC 43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17- 19 AND AC 43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC 43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH SECTION 16. ELEC1RONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURES INSTRUCTIONS AND AC 43.13-2B, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS MODIFICATION 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 AC 43.13-1B, CHAFFER 10, SECTION 2 AND AC 43.13-2A, CHAF1ER 1 PARAGRAPH 9. PER THE AERO-M SATCOM INSTALLATION MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT Al.PECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333-CE. THERE ARE NO COCKPIT PROCEDURAL CHANGES OR FLIGHT MANUAL SUPPLEMENTS REQUIRED FOR THIS INSTALLATION. END K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277751

May-29-01 01:58P N 3 Curran 352 243 1011 P _ 02 c DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA • IDENTIFICATION TITLE B727-16236-340, Initial Release, dated 04/30/01 - • TT-3000 SERIES AERO-M AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION - Vetter authority vested by direction data ;wed above aid on attached slims numbered NONE of theAdmInblrator and in accordance with conditions and reasitationa of appointment nodes- Part 113 or the Federal Aviatina Revalatiosts. hare been examined in accordance with established procedures and found to coutply with applicable nrelairensenta of the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Rscalm:ans. 0 Recommend approval of I (We) Therefore El Approve these data (Systems SIGNATUR FD NA D EN ' ERING REPRESENTAT1VE(S) DESIGNATION NUNIBERIS) CLASSIF1CATIONIS) r Zezee---_ DERT-510087-NM Systems & Equipment No an Jurran oral 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901.613 FILENAME: SC-727-SATCOMDOC EFTA00277752

a 3 EFTA00277753

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 18, 2001 _ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL B727-31 TYPE (Airplane, Radio. Hs! copra, etc) Airplane NAME OF APPLICANT Jet Aviation LIST OF DATA IDIENIIFICA1 ION III LE Jet Aviation Engineering Drawing No. B727-16236-1340, Dtd. 5/29/2001, Rev. A END END Aero-M Satcom Antenna Installation Boeing 727-31 / S/N: 20115 / N908JE END END END END END END END END Note: The certification evaluation of structure. Structural Repairs on Notes: basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 6/18/2002. aspects only of the above listed data are approved is valid for the aircraft model and serial number is based on structural analysis on file at DER Services office in Ft. Lauderdale, FL. No. B727-31 Serial No. 20115 • - I) The structural herein. 2) This approval listed below 3) This approval corporate Model PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LIST SPEC.' FIC SECTIONS) 25.301, 25.303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition appointment under Part 183 of 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 requirements of Aviation Regulations. ri Recommend approval of these data I ) Therefore 1,;i1 Approve these data and liml tions of O have the Fe eral SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S)DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau .„QA)15 e........................ DERT-510024-CE Structures FAA FORM 81I0-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001-082 EFTA00277754

Vi EFTA00277755

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 B727-16236-1342 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I Therefore 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) David E. Haralson it7,-„,e. 14.....r...._ DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01205.doc EFTA00277756

• • EFTA00277757

DEPARTMENT OF TRANSPORTATION • FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 • • - TYPE (A NAME captcr, iroule, it s dio. Heti etc.) AIRPLANE OF APPLICANT JET AVIATION LIST OF DATA WENTIFICAllON T171.-E A.T.E. INC. STRUCTURAL REPORT No. ATE6112001 BOEING 727-31 SIN 20115, AERO-M SATCOM ANTENNA INSTL., UPPER B.S. 360-390; GPS ANTENNA INSTL., UPPER B.S. 312-328; AIRCELL AGT.01 ANTENNA INSTL., LOWER B.S. 400-420 DAMAGE TOLERANCE ANALYSIS; SH. 1-31, REV. (IR) • - - NOTE: REQUIRED INSPECTIONS ATTAQBED . 20115 . THESE DATA APPLY ONLY TO BOERNIG 727-31 S/N . . . PURPOSE OF DATA . . TO APPROVE -DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-3I S/N 20115 , APPLICABLE REQUIREMENTS (Lis specific sectioas) . - . FAR 25.571 (STRUCTURAL, ASPECTS ONLY) ' . • . CERTIFICATION - Under of appointment under Part 183 have authority vested by direction of the Administrator and in accordance with conditions and of 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 Recommend approval of these data Approve these data limitations • . 1 of 1 requirements ' of the Federal Aviation Regulations. I (Ye) Therefore ,g, SIGNATURES) OF DESIGNATED ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATION(S) /' • t . DERT-5 I 0333-CE STRUCTURAL - . • . • _. FAA Form 8110-3 tit :70) SUPERSEDES PREVIOUS EDMON cro 901-613 EFTA00277758

.14 ii. • 4 • • EFTA00277759

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND REGISTRATION MARKS N908JE 2 MANUFACTURER AND MODEL BOEING 727-31 3 AIRCRAFT SERIAL NUMBER 20115 4 CATEGORY TRANSPORT 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provide by Annex 8 to the Convention of International Civil Aviation, except as noted herein. Exceptions: NONE 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, airworthiness certificate is effective as lo g as accordance with Parts 21, 43, and 91 of e F United States. DATE OF ISSUANCE R may 17 2001 ed, or a termination date is otherwise established by the Administrator, this e maintenance, prey: ative maintenance, and alterations are performed in • e I Aviation Regul o , as appropriate, and the aircraft is registered in the DESIGNATION NUMBER SO17 Any alteration. reproduction, or misuse of this flute may be punishable by a fine not exceeding 31,000, or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) AFS Electronic Forms System -JetForm FormFlow -1211998 EFTA00277760

Is P EFTA00277761

I UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I 1 NATIONALITY AND REGISTRATION MARKS N505LS . MANUFACTURER AND MODEL IP. BOEING 727-31 3 AIRCRAFT SERIAL NUMBER 20115 4 CATEGORY TRANSPORT 5. AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor. to be in condition for safe operation. and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein, Exception 4- NONE 6. TERMS AND CONDITIONS Unless sooner surrendered. suspended, revoked, or a termination date is otherwise established by the Administrator, this airworthiness certificate ts effective as long as the maintenance, preventative maintenance, and alterations are performed in accordance with Parts 21. 43. and91 of the Federal Aviation Regulations. as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE R 07-23-90 JAY Any alteration. reproduction, or misuse of this certi years. or both. THIS CERTIFICATE MUST AVIATION REGULATIONS. DESIGNATION NUMBER GLO7 to ma punishable by a fine not exceeding $1.000. or imprisonment not exceeding 3 DIS ED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL FAA Form 8100-2 (8-62) *U.S.G.RO.: 1994-568-762 EFTA00277762

I la r 2, a at SM S '► EFTA00277763

e l MAJOR REPAIR AND ALTERATION U.S. Department of (Airframe, Powerplant, Propeller, or Appliance) Transportation Federal Aviation Adniinistration _ Form Approved O/v1B No. 2120.0020 For FAA Use Only Office Identification - ,zto —./- 9 /0 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 Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N505LS 2. Owner Name (As shown on registration certificate) NORTHWEST DELAWARE CORP Address (as shown on registration certificate) 1105 N. MARKET ST WILMINGTON DE 19899 3. For FAA Use Only • . 4. Unit Identification . 5. Type Unit Make Model Serial No. . Repair Alteration AIRFRAME - above) — XX (As deieribed in item 1 - - POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B Kind of Agency C. Certificate No. • TIMCO . Lake City Municipal Airport Lake City, FL 32025 U.S. Certificated Mechanic DU4R141M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer ' D. I certify that the repair and/or alteration made to the units identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with 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 August 23, 1999 Signature of Authorized Individual Arthur E. Saylor a' ,4 6?"aft 7. Approval for Return To Sex-vice Pursuant Administrator BY to the authority given persons specified of the Federal Aviation Administration below, the unit identified in item 4 was inspected in the manner prescribed by the REJECTED and is 10 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 August 23, 1999 Certificate or Designation No. DU4R141M Signature of Authorized ividual Scott L. Palm FAA Form 337 (12-88) This 337 supersedes 337 dated August 7, 1999 EFTA00277764

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.) Boeing 727-31 Reg. No. N505LS S/N 20015 August 23, 1999 Page 1 The following major repairs were accomplished: 1. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 56 IAW TIMCO E.O. 99-1190 Rev. I/R dated 12 JUL 99 Approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delmainated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 IAW TIMCO E.O. 99-1191 Rev. I/R dated 23 Jul 99 approved per FAA Form 8110-3 by DER D. Joynes DER #DERY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR Engineering Repair Data Sheet and FAA Form 8110-3 by DER Jeffrey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished IAW TIMCO E.O.'s, ROHR Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished is on file at this repair station under work order 060/T-361. end K Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992.169.012/601S7 EFTA00277765

9) MAJOR REPAIR AND ALTERATION U.S. Department of (Airframe, Powerplant, Propeller, or Appliance) Transportation • Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification .---- / ---5 1) —C•C 7X 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 Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N505LS 2. Chvner Name (As shown on registration certificate) NORTHWEST DELAWARE CORP Address (as shown on registration certificate) 1105 N. MARKET ST WILMINGTON DE 19899 3. For FAA Use Only • 4. Unit Identification 5. Type' Unit Make Model Serial No. Repair Alteration AIRFRAME above) )O( , (As described in item 1 — POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. TIMCO • Lake City Municipal Airport Lake City, FL 32025 U.S. Certificated Mechanic DU4R141M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the units identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with requirements of Part 43 of the U.S. Federal Aviation Reguiations and that the information furnished herein is true and correct to the best of my knowledge. Date August 7, 1999 Signature of Authorized Gregory A Christman 4/ i ____- 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified of the Federal Aviation Administration below, the unit identified in item 4 was inspected in the aruier prescribed by the El REJECTED and is E3 APPROVED FAA Flt. Standards Inspector Manufacturer . Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Gro Date of Approval or Rejection August 7, 1999 Certificate or Designation No. DU4R141M Signature of Au - ed Individual out L. Palm FAA Form 337 (12-88) EFTA00277766

4 . 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.) Boeing 727-31 Reg. No. N505LS S/N 20115 August 7, 1999 Page 1 The following major repairs were accomplished: 1. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 45.5 IAW 'HMCO E.O. 99-1190 Rev. UR dated 12 JUL 99 approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delaminated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 IAW TIIVICO E.O. 99-1191 Rev. I/R dated 23 Jul 99 approved per FAA form 8110-3 by DER D. Joynes DER #DF.RY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR Engineering Repair Data Sheetand FAA Form 8110-3 by DER Jefa ey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished TAW 'HMCO E.O.'s , ROHA Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished are on file at this repair station under work order 060/T361. end K Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00277767

trul,21 1999, 22:06 PDT MsgNum: CPZ-LRK-99-00014H Page 2 of 2 117/Zr/99 WED 16:06 FAX 9 544 7667 0001 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 1 0 W A I:1 /141 i j 1 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION .__. MAKE Boeing MODEL NO. 727 TYPE (Airplane, Radio, Helicopter. etc.) Airplane NAME OF APPLICANT • Boeing Commercial Airplane Group • LIST OF DATA IDENTIFICATION TITLE . • • • : . . . CPZ-L Mk99-02041;R • Date&•9.1u1•199p- - • - CPZ-1_11. 199-000.061-I • Dated- 12 Jul-1999 . : - : . • CPZ-LRIC--99-0208TR: • -. ' Dated 19 Jul 1'999 • - • :: . _ - . . . ... — , . • Subject Center Engine Support Skin. Panel Corrosion, Delamination . • Requestor: TIMCO (CPZ) for The Limited (LII) Part Number/ Serial Number: 65-17556 Model No.: 727-100 Serial No.: 20115 Basic No.: E2218 Registry No.: NSOOLS Variable No.: E3704 Line No.: 735 • Flight Cycles: 21643 Hours: 31835 . - Service Bulletin /AD: N/A . - - . -., . TIMCO telex with description Of blendout and doubler repairs to corrosion and • -,..i delamination areas at StatiOnSI3713: 1387.85, and 1342.4. - Boeing reply that repairs ar6itiiidniiitiy. tgfaciory with prciviSi0ns. • , — — .. , - . • . •ITMCO telex with-statementthatl4aii: hai been coinpieted fier• disi:iiisition• andreq'tieSi • for 8110-3 form. • • • - • • • ' .. • . - • • • - • - • • .— • • ,.. • : . . • ' . - PURPOSE OF DATA Structural Substantiation of Repair Plan APPLICABLE REQUIREMENTS (List specific section) CAR 4b - - Subpart C: 4b.200 through 4b.202, 4b.270 Subpart D: 46.300 through 4b.304(a), 4b.306(a)&(b) CERTIFICATION - Under of appointment under Part 183 : authority vested by direction of the Administrator and in accordance with.conditions of the Federal Regulations, data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply Aviation Regulations. Recommend approval of these data Approve these data and limitations with applicable requirements of the Federil I (We-) Therefore • SIGNATURE(s) OF DESIGNATED ENGIN ING REPRESENTATIVE(s) DESIGNATION NUMBER(s) CLASSIFICATION(s) D. Joy nes ..---1) DERY-635317-NM Structures .....„...—,. FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION Page 1 of 1 EFTA00277768

a I e • EFTA00277769

07/15/99 15:54 FAX 3366651786 • ar•PZEIME.M.FIRM. • TIMCO ENGINEERING -0 LAKE CITY f?)002 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE July 12, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE ,Boeing MODEL NO. . 727 TYPE (Airplane, Radio, Herrcopler, etc.) Airplane NAME OF APPLICANT TIMCO LIST OF DATA IDENTIFICATION TITLE TIMCO E.O. 99-1190, Rev. I/R. Dated 12 JUL 99 TIMCO REPORT NO. S.A. 99-1190, Rev. l/R. Dated 12 JULY 99 8727; SEAT TRACK: STATION 662, RBL 56 CORROSION BLENDOUT REPAIR. STRESS ANALYSIS; SEAT TRACK CORROSION REPAIR AT STA 663 RBL 54 . END . . NOTES: 1. This approval is for Northwest Delaware aircraft N505LS, S/N 20115 only. PURPOSE OF DATA In support of a Major Repair accomplished on aircraft S/N 20115. This approval is for design and static analysis only and is not installation approval. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301, 25.305, 25.601, 25.603, 25.605, 25.609 and 25.613. CERTIFICATION - Under authority Part 183 of the Federal Aviation with established procedures and vested by direction of the Administrator Regulations, data listed above and on attached found to comply with applicable requirements approval of those data th ese data and in accordance with conditions and sheets numbered WA have limitations of appointment under been examined In accordance of the Federal Aviation Regulations. IN Recommend I (wile) Therefore O. Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBERS(S) CLASSIFICATION(S) STRUCTURES Wayne Fink DERT-510117-CE 4._------- _....... . __. SUPERSEDES orm - PREVIOUS EDITION ELECTRONIC FORMAT (4-99) EFTA00277770

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8- 4: bb YM ;6UF6K 27 FKUUKAM . • •. . . . - " • . • • • • • bl9bH.1.2232;g 2/ 8 — _ U.S. DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE August 3, 1999 4 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION TYPE (Airplane. Radio, Helicopter, etc.) . Airplane 4 NAME OF APPLICANT Rohr, Inc. MAKE Boeing MODEL NO_ 727 LIST OF DATA IDENTIFICATION _ TITLE EROS CI 036 dated August 3, 1999 41/4-.' • B- Cox Stress Analysis !Doted August 3, 1999 • • ' (Ref. ERDS C1036) Engineering Repair Data Sheet, Definition of discrepancy and repair design for P/N 1/A545300-1 (Aft Skin - Upper Skin Assembly) . Skin Disband VA545300-1 • • . - . PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS (List specoc sections) (1) FAR 25.301 (1) FAR 25.307(a) (1) FAR 25.605(a) (1) FAR 25.619 (1) FAR 25.303 . (I) FAR 25.601(a) (1) FAR 25.609(a) (1) FAR 25.305(a)(b) (1) FAR 25.603 (1) FAR 25.613(a)-(d) .c • CERTIFICATION — Under authority appointment under Part 183 of the ' NONE have been vested by direction of the Administrator and in accordance with conditions and limitations of Federal Aviation Regulations. data listed above and on attached sheets numbered examined in accordance with established procedures and found to comply with applicable Regulations. 7 Recommend approval of these data EgApprove these data • requirement) of the Federal Aviation I (We) Therefore SIGNATURE(S) OF LJESIUNATED ENGINEERING E ESENTATIvES Off$IGNATION NUMBER(3) CLAS3IFICATION(8) (1) Jeffrey D.Shutrump DERY-605526-NM Structures - . . " FAA Form 81104 (11-70) SUPERSEDES PREVIOUS EDITION (Computer Generated by Rohr, Inc.) EFTA00277772

4 Y a , so • • • EFTA00277773

O0OO MOO ROHR, INC. HaHH 6.50 Lagoon Drive Chub VIr2. Ca ttnta 91910 - Z198 ENGINEERING REPAIR DATA SHEET (EROS) FORM 8110.3 REQUIRED CLASS MAJOR F3 EROS NO. C1036 REV. S.O. NQ N/A REV. PAGE I OF 2 PART NO. VA545300-1 PART SERIAL NO. N/A MODEL V727RE COMPONENT AFT FAIRING -UPPER SKIN ASSY SERVICE I-CURS UNK CUSTOMER THE LIMITED DISCREPANCY: (BE SPECIFIC - PRINT CLEARLY ) ITEM A. The upper skin on the AFT fairing assembly, P/N .VA545300-1, on the #1 Engine position shows a disbanded condition on approximately 50% of the AFT surface, including two crescent shaped cracks on an existing repair (fiberglass?). On this same arevon the lower surface of the panel, an area of material is also missing and filled as above. The lower repair stops before transitioning to pan down of honeycomb. • See page 2 for sketch of location and description. MATERIALS: Upper Skin .032 2024-T3 QQ-A-250/5 Lower Skin .016 2024-0 QQ-A-25015 Heat treated to —T42 per MIL-H-6088 Honeycomb .310-3116-10 (5052) MIL-C-7438 PREPARED BY Don Adams REPAIR: ITEM A. Repair. UPPER SKIN REPAIR 1. Remove discrepant upper skin from assy. Care should be taken not to disbond the lower skin of the assy. 2. Fabricate a new upper skin from .032 gauge 202443 per QQ- A-250/5. 3. Remove lower surface Clad (bonding side). Do not thin below .029. 4. Make sure all remaining "old" adhesive is removed from core. Clean and prep skin (using PAA or Pasa-Jell 1 0 5) and exposed core (using Pasa-Jell 105) on panel. Clean repair area per 727' SRM 51-40-6, Par. G(2) (SRM 51-40-5). 5. Prime bond side of skin and core with BR-127 adhesiVe primer, per manufacturer specifications. 6. Apply two.coats of FM-73 adhesive material, per manufacturer specifications. 7. Bond replacement upper skin to core and lower skin per 727 SRM, 51.40-6, paragraphs E, J & K 8. Perform Post Bond inspection byvisually inspection of periphery for evidence of adhesive bead, and tap test the whole panel for voids. ORIGINAL rearms! when tilts stamp co is to rid ink DATE 8-02-99 AIRWORTHINESS APPROVAL DATE -_? 7 FOR.41 NO. E6687,5 Lz xggrIR! W1 t!ZEZZT696T9 EFTA00277774

> EFTA00277775

OOOO 42OOO ROHR ROHR. INC. &X Lag= Dave Chtia Vida. CAlrfunia 91910-2098 ENGINEERING REPAIR DATA SHEET (ERDS) SUPPLEMENT SHEET RDS NO. C1036 REV. .0. NO. N/A REV. PAGE 2 OF 2 (1;scR6Rirkticy ecivrieiver)) FORM NO. E7983-1 .11tIZ71 (DISPOSITION CONTIUNUED) LOWER SKIN REPAIR 1. Remove existing repair (fiberglass) from discrepant area on lower surface. . 2. Cut filler to size of discrepant area from .016 gauge 2024-13 per QQ-A-25015. 3. Fabricate doubler from .020 gauge 2024-0, per QQ-A- 250/5 to cover filler. Doubler to overlap filler periphery by 1.50 min. Optional to use 2024-T3, no heat treatment required. 4. Form doubler to match lower skin contour per BAC 5300. Heat treat to -T42 per BAC 5602 or MIL-H-6088. Verify hardness per SRM requirements. 5. Inboard and outboard edges of doubler to be tapered to .010 min. Care should be taken so the edges of the doubler land mid spaced between existing assembly fasteners_ 6. Install doubler using steps 3 through 8 above. 7. Install new panel, filler & doubler using BP fasteners to complete assembly. Apply sealant to edge of logo light cut out , and seal all gaps at assembly. 8. Clear Alodine all external clad surfaces per MIL-C-5541, Class 3. ORIGINALl , is in red Ink When this stamp uvrmusr, EFTA00277776

EFTA00277777

8- 3-99 4:55 PM ;SUPER 27 PROGRAM 6196912232;# 5/ 8 By B. COX DATE 08/02/99 cHK'D1-51)07O) DATE OM ERDS Cl DODD EH= ROHR ROHR, INC. PAGE 1 of 4 TITLE Skin Disbond VA545300-1 Use or disclosure of this information is subject to the restriction on the title page or on the first page of this document Super 27 I. Discrepancy: The outer skin of the upper skin assembly of the aft fairing is disbonded and the aft edge of the outer skin has two cracks. See sketch below from ERDS. I!. Proposed Disposition: Remove the outer skin of the upper skin assembly and bond on a new outer skin using FM 73 adhesive and BR.127..adhesive primer. The cracks at the aft edge have been reported to be along a previous repair that was filled with a fiberglass patch repair. The fiberglass patch will be removed and replaced with a metallic patch and doubler. All metallic materials will be the same as BP materials. III. Static Analysis: The aft fairing is analyzed in section 10 of Reference'. In section 10 of Reference ', the substructure has been analyzed to withstand all the aerodynamic loading without using any of the skin as affective. Therefore, this analysis will only investigate the capability of the adhesive to carry the shear stress to the core conservatively assuming that the skin will carry the aerodynamic loading. strut Stress Analysis (VA-CR1 54 Rev. C) 1,09112 Dui 'MA EFTA00277778

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