()V 0 - ' MAJOR REPAIR AND ALTERATION U.S Dpartrnal on to (Airframe, Powerplant, Propeller, or Appliance) man Federal Aviation Administration d, - Form Approved 0303 No. 2120-0030 For FAA Use Only Office Idaztillosion tl5o F.5 gel -1 S gi-6-- ')'sn" P", +2" re aerie issirtifi"1, FAR 43 Appendix B, pad* 43.94 (or who:quad. rivision Owed for instructions and stisposhicp of this form. This tion = 195 5. y ( . . ). a ton:port MI result an civil penalty not to cohan151,000 fix radi violation (Scale,. 901 hislaal 3. Aircraft MakeBoeing Medd 727-31 sawNo.20115 Nationality and Rogan:ice Made N908JE L Owner Marne (As shown as regLaratica ocitificatc) JEGE INC- Micas (xs Aomori rogistraticn certifunte) 103 FOULKRD STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model 1 Serial No. Repair Alteration AIRFRAME XX (As domIxd in hats 1 above) POWERPLAYT PROPELLER APPLIANCE Twc hbindacturcr 6. Conformity Statement A- Agaicds NarnexadMdrou B. Kind *Maw/ C. Catificate No. TIMCO Lake City Municipal Airport Lake City, FL 32025 U.S.Catificatoitachanic DU4R141M Foreign Cati6cood Mechanic X Catillaitof Repair &Mica Manufactura D. I certify that the repair ander alteration mad, to the logs idaulfief in itcnr 4 abonond dam-bida:ft rcruscorattichmon hereto have bon made in accordance vrillt ropaircinents of PartAl ofdoU.S. Wool Aviation Regulditosandihathe ioknaatica Danishitd hock istrucandoxinctto die test &my blade* Date August 1, 2001 Signature orAuthorized Individual Owen H. Pritchard II ..._ 7. Approval for licturriToSers c Pursuant Administrator BY to the authority of the given persons Federal Aviabon. specified Administration below, the unit identified in item 4 was inspected in the manner prescribed by die 0 REJECTED and is 12 APPROVED FM Fk. Standards Inspector hlimufacturcr Inspation Authicizatiai Other (Sptcy54 FAA Datignix X Repair Station Pasco Approved by Transport Ains Group Canada Donor 49(0=1 or Rejection August 1, 2001 Catifiratcor Dosignaticas No. DU4R141M Sigmas a Authiciud Ind' L. Palm FAA Form 337 (12-88) SDNY_GM_02759747 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246669 EFTA01331132

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 cot:fannies with the applicable alnvorenness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration matt and date work completed.) BOEING S/N 20115 REG. NO. N908JE . Page 1 August 1, 5001 The following major repairs were accomplished: NR# 27754 Repaired detaminated R/H Mid Flap Trailing Edge wedge by removing the delaminated section and fabricating and installing a new T/E wedge and strips TAW TIMCO REO-L00464 dated 7/17/01 FAA Form 8110-3 approved by DER. Richard C. Saltivan DER # DERT-405157-CE dated June 19, 2001. MU 27918 Repaired the delaminated and corroded Left Hand Inboard Mid Flap bottom upper Rock-shield panel by removing Rock-shield and corrosion, treated and primed area to be bonded, impregnated fiberglass overlays as required, applied conductive coating and. installed panel IAW B727 SRM 57-50-2, 5140-8, MM 51-20-0 & SB 727-32-247 RI dated June 5, 1981. SUMMARY 1. All work accomplished JAW Boeing SRM, TIMCO REO, FAA Form 8110-3 and ServiceBulletin. 2. Records of all work accomplished is on file at this repair station under work order 185003. 3. Aircraft Weight and Balance updated accordingly. end 0 Additional Sheets Are Attached SOSGOVEIOJQ4T PRINIONIOFFICE IW1.769.0i2,1007 SDNYGNI_02 759748 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246670 EFTA01331133

6 . us Departmeel of TrwepOrtallon (Airframe, Fearslablatica Adenlitstrailon MAJOR REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification INSTRUCTIONS: Print or type all and disposition of this form. This report $1,000 for each such violation (Section entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed SOI Federal Aviation Mt of 1956). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N008JE 2. Owner Name (As shown JEGE INC on regIsfralkx; certificate) Address (As shown on registration certificate) 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only in-, data idatIttheod %Val 2:nottniele retirements emenbe:/ acre. when JOS:161hr the est by appacrot the above a perton ir liet apperee 433. So -rs-Da- Ch" a re minsondet 4. Unit !dentinal on) 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described In Item 1 above) X POWER PLANT PROPELLER • APPLIANCE Type Manufacturer ... 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES 1516 PERIMETER RD. WEST PALM BEACH. LTD. FL 33406 U.S. Certified Mechanic CRS WEICI4752D AIRFRAME O. RADIO 1,2,3. LIMITFD AIF &FNG Foreign Codified Mechanic x Certificated Repair Station — Manufacturer D. I certify that the repair and/or alteration have been made in accordance with furnished herein Is true and correct made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto the requirements of Part 43 of the V.S. Federal Aviation Regulations and that the information to the best of my knowledge. Date 'A4/ . Signature of Authorized indivi lobo K. Urso. Inspector. 4 (Ler— 7. Approval for Return to Servl Pursuant Administrator BY to the authority given persons of the Federal Aviation specified below, the unit derained in item 4 was inspected in the manner prescribed by the Administration and Is Fs) APPROVED 0 REJECTED FAA Fit Standards Inspector Manufacturer Inspection Authorization Other (Specify) FM Designee X Repair Station Person Approved by Transport Canada Alnvorthiness Group Date of royal or Rejection App 7 1- / 0 / 4 Certificate Designation or No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manner Quality Ass FAA Form 337 ti2-as) SONY_GM_02759749 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024667 I EFTA01331134

NOTICE Weight and balance or operating finiltation changes shall be entered In the appropriate aircraft record. M afteratkn must be teakettle with all previous alterations to assure continued conformity with the applicable &neon/darks requirements. • 8. Description of Work Accomplished (If more space b required, attach arketional sheets, identify with aircraft nationality and registration mark end date wog* accomptshed) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001. W.O. 16234 PAGE 1 OF 2 INSTALLED A SINGLE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY SYSTEM (ISO CI13). THIS MODIFICATION WAS COMPLETED USING JET AVIATION DRAWING NO. B727-16236-270, ARGUS 5000 CIE MOVING MAP DISPLAY, REV. A. DATED 06/19/01. REFERENCE FAA FORM 8110-3. DATED 6/20/01, BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. THE EXISTING LASERTRAK WIRING WAS RE-BUSSED DUE TO RELOCATION OF LASERTRAJC C.D.I. THIS MODIFICATION WAS COMPLETED USING JET AVIATION DRAWING NO. 34-61-32-1, LAZERTRILIC SYSTEM MODIFICATION, REV IR, DATED 5/24/01. THE STRUCTURAL INSTALLATION OF THE AROUS.540weaimovate Ma.DISPLAY SYSTEM AND THE RELOCATION OF THE LAS ERTRAK Cal. WAS COMPLETED USING JET AMIUM40„ Iwo. ARGUS 5000/CE MOVING MAP EQUIPMENT INSTALLATION, REV. 112. DATED 0929/0 . MAFORM AlEp 06/03/2031. BY STRUCTURES DER NO. DERT-13100213-NE. ;on. -7- — THE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY IS A PICTORIAL NAVIGATION INSTRUMENT, WHICH PROVIDES VISUAL REFERENCE OF AIRCRAFT POSITION RELATIVE TO LANDING FACIL(TIES, NAVIGATIONAL AIDS AND SPECIAL USE AIRSPACE. THE ARGUS 5000/CE RECEIVES GEODETIC POSITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS- ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF" INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES ARE LOCATED ON P16 FORWARD CONTROL STAND. BELOW THE ARGUS 5000 CE MOVING MAP DISPLAY: ARGUS INFQ MOMENTARILY DEPRESSING THE ARGUS INFO ILLUMINATED (BLUE) SWITCH BRINGS UP INFORMATION ABOUT MAP OBJECTS ON THE ARGUS 5000/CE MOVING MAP DISPLAY. IF THE ARGUS $ 4 F 0 SWITCH IS PUSHED IN FOR 1 SECOND, THE ARGUS 5000/CE WILL RETURN TO THE MAP DISPLAY IN THE SAME MODE AND AT THE SAME RANGE SET. WHEN INFO WAS ENTERED. ARGUS MOMENTARILY DEPRESSING THE 612GUS SEL ILLUMINATED (BLUE) SWITCH CYCLES THE ARGUS 5000/CE DISPLAY THROUGH THE VARIOUS MAP OBJECTS. ARGUS TEST MOMENTARILY DEPRESS THE ARGUS TEST SWITCH TO ENABLE DISPLAY SIMULATION TEST. THE ARGUS 5000/CE MOVING MAP DISPLAY IS APPROVED FOR IFR ENROUTE NAVIGATION ONLY WHEN RECEIVING NAVIGATION INFORMATION FROM AN IFR APPROVED CPS, LORAN. OR OTHER LONG-RANGE NAVIGATION SYSTEM. THE ARGUS 5000/CE DATABASE MUST BE CURRENT (NOT EXPIRED). THE ARGUS 5000/CE IS APPROVED FOR USE AS A SUPPLEMENTAL NAVIGATION DISPLAY FOR VFR AND IFR OPERATIONS BUT IS IJMITED TO THE APPROVAL OP THE LORAN C OR GPS NAVIGATION SYSTEM. THE ARGUS 5000/CE MOVING MAP DISPLAY HAS BEEN SHOWN TO MEET THE CRITERIA OF FAA TSO.CI 13, AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS. AND HAS BEEN PREVIOUSLY INSTALLED UNDER EVENTIDE INC. FAA APPROVED STC SA0054NY. IN AN AIRCRAFT AND MEETS THE FAA REQUIREMENTS FOR OPERATION IN THE AIRCRAFT DURING INSTRUMENT FLIGHT AND CAN BE USED AS A REQUIRED INSTRUMENT. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER EVENTIDE AVIONICS INSTALLATION MANUAL NO. 5003. REVISION 03.07. DATED JULY 10, 1995 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 234 THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.I3-2A. 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- I 6236-041, REV IR. SHEETS 1 THRU 21. DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-111. CHAPTER 11, SECTION 3. PARAGRAPH 11.37. 121 Additional Sheets Are Attached * V.S. G.P.O 1990-761-753 SDNY_GM_02759750 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246672 EFTA01331135

NOTICE Wejght and balance or operating knitation changes shag be entered in the appropriate aircraft record An alteration must be conpatible with ail previous alterations to assure continued confonnily with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is requited, attach additional sheets, Identify with aircraft nationality and registration mark and date work acconwashed.) • AIRCRAFT: BOEING, TYPE: 727-31, SIN 20115, DATE 06/1412001, W.O. 16236. PAGE 2 0F2 AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-18, 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 I.5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MD. SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER I I, SECTION 4. EIECTRICAUELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER 1 I, 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 AC43.13-18 SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13.2.A, 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 i PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS OUTLINED IN EVENTIDE AVIONICS DRAWING NO. 140003, REV. B, DATED JUNB JUNE 0. 1999. AND STATES THAT THE ARGUS 5000/CE MOVING MAP DISPLAY SYSTEM IS "ON CONDMON". THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236401, REV 112, PAGES I THRU 6 DATED jilrle 2-1 OO1 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL ,END 0 Additional Sheets Are Attached * U.S. G.P.O 1890-781-753 SDNYGIvl_02759751 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246673 EFTA01331136

SDNY_GM_02759752 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246674 EFTA01331137

I Jet Aviation Associates Ltd. Bldg. 1515 Perimeter Rd. Palm Beach Intl Airport West Palm Beach, FL 33406 FAA CRS EYKR782D Document No. B727-16236.101 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.: N9OBJE SERIAL NO.: 20115 WITH A SINGLE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of a single Eventide Avionics Argus 5000/CE Moving Map Display receiving navigation inputs from the No. 1 UNS-1D Flight Management System (FMS) in accordance with manufacture's Installation Manual No. sop Revision 03.07, dated July 10, 1995 or later approved revision and FAA Form 337, dated VW/ 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. FM Approved: Federal Aviation Administration Flight Standard District Office -17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: JUN 2 1 2001 Page 1 of 6 SDNY_GM_02759753 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246675 EFTA01331138

SDNYGM027597. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246676 EFTA01331139

attn-2O-O1 O8:53 Jett Aviation Jun-20-01 O8:O3A N J Curran 352 243 1O11 P . O2 P 02 IMPPADIENT Of VIANWOATATION Matt MIA 00s. ADIMOTRADaN STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DAM 06/20/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAIk Boeing MOOD. NO. 727-31 TYPE Unarm. Rad*, *hoopla. tic) Airplane MAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL MT OF DATA IDENTIFICATION TITLE 8727.16236.270, Revision A, dated 06119/01 ARGUS 6000ICE MOVING MAP DISPLAY PURPOSE OF DATA In support of major alteration Io.Boelng 727-31, serial number 20115. regisUalion number N90BJE. APPLICABLE REQUIREMENTS (Lba specific sections) FAR 26469 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1629 FAR 25.1309 (a)(b)(g) FAR 25.1581 (a)(b)(d) FAR 26.1361 (a) FAR 25.1357 (a)(c) CERTIFICATION - t ion ..a..........• 6, anah • or a.,......«.m. ads swam. nante••••••••••••••healorpriSsam•••• I.n mutat no... «now rwr ia...... a... "ea —01/CE._. ...4.... 1^•••••en Hp.... *masa. 0 lientasead marvel of Sae Oslo I OM.) rbarefore ID Ann...Hem tam (Symms • tqcOnsessi Aspects. Di/sin AprOai thi).. Dia Mt Cant:eta bawl:Weft Apprt...• WAAMILCI CO t"C ainnENTAM11O4 OCJIGOATICM. PUMPS% C /AMICK • MINI. fee DERT-510087-NM Systems & Equipment o n J. n --, SDNYGIvl_02759755 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246677 EFTA01331140

SDNYGM02759756 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246678 EFTA01331141

JET AVIATION ASSOCIATES, ROAD LTD • ie SET NifffS1701111 1515 PER IMETER PALM BEACH INT'L AIRPORT MODIFICATION DRAWING ilidin iCH Fliiiiiiii.493 PIONIOOLY tOret la. *roof, esSe "Tsars, wd/ do* tweeted neoelok newts espy ore Idisoike US we we So navy erg .0 OSZOI ASSCOOO. OP %M.o./ ere USW V/ b eedSoot on*Soeedo. bode es Ti oel to •• Sea of goons on wool/edged onoSeta pens 4404.4 the sins weedogrego JO IIMMoil 0130000. km TITLE: LASERTRAK SYSTEM MODIFICATION PAGE: 1 OF 1 DWG NO.: 34 - 61 - 32 - 1 _ REASON: RE- BUSS LASERTRAK INSTRUMENT LGHTING FROM CENTER PANEL TO CAPTAINS INSTRUMENT PANEL DUE TO RELOCATION OF INSTRUMENT A NOlt$: 1. AIRCRAFT WIRING INSTALIATION CHAPTER 11, SECTIONS 1, AND 2. ALL WIRE PER MIL-W-22759 UNLESS 3. ALL SHIELDED WIRE PER IAL-C-2750010. 4. A.U. METE 20 MC UNLESS SPEOF1ED S. All. CIRCUIT BREAKERS PER 11536574. 6. ALTERNATE TWISTED WIRE COLORS Mat TRIPLE TWISTED RED SLUE YELLOW TWISTED PAIR: RED BLUE 7. LOWER CASE LETTERS ARE SHOWN 8. THIS MODIFICATION DRIOTINC SYSTEM PER THE WRANG SHOWN. REGARDING THE LASERTRM( SYSTEM DWG. 34-61-32. THIS MODIFICATION TO THE ORIGAMM. PAGE AVJET i-rim BRCIDIST ND. D9504 . n .. r Fl a i 01-20 1Nsirt L.'? t 0 II µ I-20 I dr ' MW FM AC. 43.13-18, 3-20. SIOELDEO. OTHERMSE. MAY BE SUE411TUTED: $LS (R) WIVE (R) (B) BLUE (El) (Y) ORANGE (0) (R) MITE (R) (6) BLUE (8) UNDERUNED. LE. S. ONLY CHANGES THE COSTING LASERTRAJC FOR ALL OTHER INFORMATION REFER TO ORCRIAL PAGE AWET DRAWING SIAU. 8E ATTACHED DRAWING FOR REfERNCE _ .... _0 19_20_ _ PAGE CMG. 33-11-11 rrisfina LO tticZt FAsERTRAK COI —I 3 h 1 0915 09315 1 20 I Rim LTs {SC II 9I 09315 9-20 LAL` rrift>7 141117, . a Ipi o SYMBOL MID NORM REFERS TO PARTS LIST REM NUMBER. mute tan:t .-8> 1 sada. AND NUMBER REFERS TO WSTALLATION NOTES. O sweet Mt LETTER LETTER ren REFERS TO LEE w SYMBOL ON DWG, NO. WIRE TOE NOTES: r 40C GIS .4 MC 040 .43> aS)LD Gle -B> .0415515 CND a, NEW WOE REMOVED WIRS COSTING WIRE ) (• . ( 1G. SCALE: NONE SER. NO.: 20115 PREPARED BY: G.L. KARR APPROVED BY: T. JARDINE A/C MODEL: 727-100 REG. NO.: N9OBJE DATE: 05/24/01 DATE: 05/24/01 SDNY_GIvl_02759757 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00246679 EFTA01331142

SDNY_GM_02759758 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246680 EFTA01331143

OEPAFtTMENT OF TRANSPORTATION I-DATE FEDERAL AVIATION ADMINISTRATOR STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 3, 2001 AIRCRAFT OR ARCRAFT COMPONENT MENTRCATER MAXE Boeing MOM NO. 727-31 TYPE (Mpent Radio. HokopteLeict Airplane NAME OF APPUCANY Jet Aviation Associates- WPB LIST OF DATA ICSITFICATON TITLE B727-16236-1270 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 APPUCAME REOUTTIMNS (LAl sped& secetas) 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 - Wider al/Monty vested by *Gaon of the Administrator aid in accordance vets caul under Past 183 of the Federal Aviation Revise onS.data listed above and on attached sheets numbered in iteowdenee with established procedures and round to eemPlY whil appecatio raquIrements of the Federal I (.4 thersevo ,0 hoosonnend *Prover of these data Approve these data bore and knitallons of eopoktrnant 0 have boon exantved Avlatke Nebula One. SKUMTURE(S) OF INSIGNATE0 010Inax.10 imppisaiNTATNE(S) OESIONATON reuratEMS) GLASSINE-010NR) David E. Haralson ,Poode. iliontio-- DERT-810028-NE Structural orm 8110 3 it t 40. SUPERSEDES PREVIOUS ECTOM Ell01207.dc< SDNYGlvl02759759 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024663 I EFTA01331144

SDNYGM02759760 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246682 EFTA01331145

o - O OS Depaterera el Transpoeudon Wend Administration MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) 4Vaeon Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification INSTRUCTIONS: and disposition S1,000 Print or type all entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instructions 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 for each such violation (Section 901 Federal Aviation Act of 1958). I. 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) IF-GE INC Address (As ahem on registration certificate) 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 . 3. For FAA Use Only on ests aresenteres deserted • tAliOrtid In aktiaair Werneree herein complise ragawireents r appatedeeerrryyy rad. mekxm t4psaseet FAR 43. 43.7. ' S re sad is tre ma above by • Penal 7 So- spo-t AllIrefh1 ol FAA Irmo-ow 4. Un Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL 33406 U.S. Certified Mechanic CRS EYKR782D AIRFRAME 1,3. RADIO 1,2,3. LIMITED A/F & ENG. Foreign Certified Mechanic X Certificated Repair Station — Manufacturer D. I certify have furnished that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information herein is true and correct to the best of my knowledge. Dale Signature of Authorized Individual /1/0) • John K. Ursa Inspector. it- It. --6- 7. Approval for Return to Se ce Pursuant Administrator BY to the authority given persons specified below, the unit dentified in item 4 was inspected In the manner prescribed by the of the Federal Aviation Administration and is 0 APPROVED O REJECTED FM Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Apprpvalpr Rejection 24 7C / Certificate or Designation No. EYKR782D Signature of Authorized Individual 4/ Ronald K. BretrOn Manager Quality FAA Form 337 024s) SONY_GM_02759761 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246683 EFTA01331146

NOTICE Weight and balance or operating Imitation changes shall be entered in the appropriate aircraft record. An Memnon must be compatible with all previous alterations to assure continued conformity with the applicable einvorthIness requirements. 8. Description of Work Accomplished (if more space is requ)rst% attach additional sheets, identity with Leonia nationality and registration mad( and date kiosk acoomFdshed.) AIRCRAFT: BOEING, TYPE 727-31, SIN 20115, DATE: 06/14/2001, W.O. 16236, PAGE 1 OF 2 REMOVED THE EXISTING NO. 1 AND 2 HONEYWELL NZ.920 EMS SYSTEMS AND 771E DL-900 DATA WADER UNIT. AND INSTALLED DUAL UNIVERSAL AVIONICS CORP. UNS-1D FLIGHT MANAGEMENT SYSTEMS (EMS) WITH INTEGRAL GPS SENSORS, A UNIVERSAL AVIONICS CORP. RADIO TUNING UNIT (RTU), AND A UNIVERSAL AVIONICS CORP. DTU-100 DATA TRANSFER UNIT (DTU). THIS MODIFICATION WAS COMPLETED USING EST AVIATION DRAWING NO. B727-16236-410, NO. 1 FLIGHT MANAGEMENT SYSTEM, REV IR, DATED 04/10/01 AND B727-16236-411, NO.2 FLIGHT MANAGEMENT SYSTEM, REV. IR DATED 04/15/01. THE RTU WAS INSTALLED USING JET AVIATION DRAWING NO. B727-I6Z36-293, FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT, REV Et, DATED 04/16/01. REFERENCE FAA FORM 8110-3 DATED 05/292001 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. raw. ot atm mares &Wel Pi, It at 'd° Ottnel 'en° "IOWA= If WC Span' arine• • THE STRUCTURAL INSTALLATION OF EACH EMS, THE DTIMEN0tHeitT0 WEFEC2MPLETEA OJET AVIATION DRAWING NO. B727-16236-1410, DUAL MIS W/RTU EQUIPMENT INSTALLATIONS. REV. IR, DATED 05.117/01„. lalE FAA FORM 8110-3, DATED JUNE 1, 2001 BY STRUCTURES DER NO. DEBT-81 S-ANTENNAS AILED • USING JET AVIATION DRAWING NO. B727-16236-1441, GPS ANTENNA INSTALLATI N, REV. A, DATED 05/29/01, REFERENCE FAA FORM 8110- 3. DATED 018/01 BY STRUCTURES DER NO. DERT-510024-CE. THE UNS-1D SYSTEMS RECEIVE BARO-CORRECTED ALTITUDE AND TAS INFORMATION FROM THE NO. 1 AND NO.2 AIR DATA COMPUTERS RESPECTIVELY, VOR/DME BEARING AND DISTANCE INFORMATION FROM THE NO. 1 AND NO.2 COLLINS VIR-432 AND DME-442 SYSTEMS. AND CROSS SIDE GPS INFORMATION AS WELL AS EACH UNITS INDEPENDENT GPS SENSOR DATA, FUEL FLOW DATA FROM THE AIRCRAFT FUEL FLOW SYSTEM AND IRS INFORMATION FROM THE EXISTING NO. I. 2. AND 3 HONEYWELL "IASERREF SYSTEMS. THE UNS-ID FMS HAS BEEN PREVIOUSLY INSTALLED UNDER UNIVERSAL AVIONICS SYSTEMS CORP. FAA APPROVED STC SA5072NM, IN AN AIRCRAFT AND CERTIFIED FOR YEA AND IFR NAVIGATION WHICH QUALIFIES THIS INSTALLATION AS A "FOLLOW ON" INSTALLATION PER AC 20-130A THE UNS-ID EMS SYSTEMS HAVE BEEN SHOWN TO MEET ALL OF THE REQUIREMENTS OF AC-20-130A FOR VFR-IFR NAVIGATION ENROUTE, TERMINAL, OVER WATER AND IN REMOTE AREAS, AND FOR NON-PRECISION APPROACHES. THE NO.1 AND 2 EMS SYSTEMS ARE DIGITALLY INTEGRATED TO THE EXISTING HONEYWELL FIVE-TUBE ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFTS). THE PILOT AND COPILOTS EFIS SYMBOL GENERATOR'S HAVE HONEYWELL SERVICE BULLETIN A21-2000-028 AND THE MULTI-FUNCTION GENERATOR HAS HONEYWELL SERVICE BULLETIN A21-2000429 TO INCORPORATE NON-PRECISION OPS SCALING VIA GAMA ARM 429 LPN INTERFACE WHICH MEETS REQUIREMENTS OF TSO C129A AND AC 20-130A. THE EMS SYSTEMS ARB CROSS-COUPLED TO EITHER THE PILOT OR COPILOT EELS FOR DISPLAY AND NAVIGATION. THE EFTS CONVERTS THE DIGITAL TO ANALOG OUTPUTS AND PROVIDES ALL LATERAL STEERING TO THE AUTOPILOT AND FLIGHT DIRECTOR SYSTEM. VERTICAL NAVIGATION (VNAV) FROM EITHER EMS SYSTEM IS NOT DISPLAYED OR COUPLED IN THIS INSTALLATION. THE FOLLOWING REQUIRED ANNUNCIATORS FOR THE FMS SYSTEMS ARE DISPLAYED ON THE EFTS DISPLAYS: yMS MSG INDICATES A MESSAGE IS TO BE ACKNOWLEDGED ON THE MSG PAGE. (COWR: AMBER) LOCATED ON EADL SELECTED CROSSTRACK IS ACTIVE (COWR: CYAN) LOCATED ON EHSL ZVSI INDICATES WAYPOINT ALERT TWO MINUTES PRIOR TO WAYPOINT IN EN ROUTE MODE, AND 15 SECONDS PRIOR IN APPROACH MODE. WHEN THIS ANNUNCIATOR FLASHES. IT INDICATES THAT AN UPCOMING VERTICAL FLIGHT PATH ANGLE (EPA) CHANGE IS WIT EN TWO MINUTES. (COWR: AMBER) LOCATED ON EHSL AN APPROACH HAS BEEN ACTIVATED. (COWR: CYAN) LOCATED ON EHSL Additional Sheets Are Attached * U.S. G.P.O 1990.781.753 SDNY_GM_02759762 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246684 EFTA01331147

get NOTICE WAY* and balance or operating limitation changes shall be entered in the appropriate akcraft recon1 An alteration must be compatible with all previous alterations Massone continued conformity with the applicable airworthiness requirements. a Description of Work Accomplished Of more space is required attach additional sheets, Identity with aircraft nationality and registration mark and date work accompashed) 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 UN/TS: j'MS UDC THE Ems IS IN HEADING SUB-MODE. (COLOR: BLUE) GPS INTRO 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 1m tr.O USING THE EXISTING PI OT AND COPILOT ANNUNCIATOR COUPLERS. THESE UNITS HAVE BEEN MODIFIED USING JET AVIATION MODIFICATION NO. 3349-02-1, CAPT. AND FIO ANNUNCIATOR COUPLER MODIFICATION. DATED 04/12101. REFERENCE FAA FORM 8110-3, DATED 05/29O001 BY SYSTEMS AND EQUIPMENT DER NO. DEBT-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 I OF 5. DATED 06/19/2001, WAS CONDUCTED AND THE INSTAL 1 PD EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.134B, 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 43.13-2& CHAPTER 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. B72746236.041, REV IR, SHEETS I THRU 21. DATED 06/110001 WAS COMPLETED IN ACCORDANCE WITH AC43.13- LB. CHAPTER II, 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-IB, CHAPTER 11, SECTION 4. ELECTRICALJELECTRONIC WIRING WAS SELECTED AND INSTALLED LAW AC43.13-1B. CHAPTER 11. SECTIONS 54, 13, 15. 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21,22 & 27. ROUTING. LACING AND TYING COMPLY WITH AC43.134B, CHAPTER IL SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-IB 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 THB AIRCRAFT RECORDS TAW AC43.13-I B, 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-ID FLIGHT MANAGEMENT SYSTEM TECHNICAL MANUAL NO. 34-60-09, DATED AUG 15/97. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN AT.E. INC. STRUCTURAL REPORT ATE6I12001 DATED 6/12/01. SUBSTANTIATED BY FAA. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333- CE THE REQUIRED FAA. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B72746236-100, REV SHEETS 1 THRU 9, DATED sone zi, 2co I HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END 0 Additional Sheets Are Attached SDNYGlvl_02759763 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246685 EFTA01331148

SDNYGM02759764 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002466R6 EFTA01331149

t ta, Jet Aviation Associates Ltd. Bldg. 1515 Perimeter Rd. Palm Beach Intl 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 72741 REGISTRATION NO.: N908JE SERIAL NO.: 70115 WITH DUAL UNIVERSAL:AVIONICS FLIGHT MANAGEMENT SYSTEMS (UNS1-D) INSTALLED ' - This supplement must be attached to the FM 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 VOR/DME systems in accordance with manufacture's Installation and Checkout Manual No. Rev. 2. dated August 15, 1997 or later approved revision and FAA Form 337, dated. 7 a 01 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. FM Approved: Federal Aviation Administration Flight Standard District Office -17 1050 Lee Wegener Blvd. Ft. Lauderdale, Florida 33315 JUN 2 1 2001 FAA Approved Date: Page 1 of 9 SDNY_GM_02759765 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246687 EFTA01331150

a' SDNY_GM_02759766 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246658 EFTA01331151

May-29-01 01:59P N C 352 243 1011 P . 06 voinameNTOPTRASSIOATATION MOM ASA110). Ammoniac". STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DAT I 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Booing MODEL NO. 72741 TYPE (Alalant Para Hamra. at) 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 8727-16236-41D, Initial Release, dated 04110/01 B727-16236-411, Initial Release, dated 04/15/01 3349-02-1, Initial Release, dated 04/12/01 FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT NO. 1 FLIGHT MANAGEMENT SYSTEM NO. 2 FLIGHT MANAGEMENT SYSTEM CAPT AND 1/0 ANNUNCIATOR COUPLER MODIFICATION PURPOSE OF DATA In support of major alteration to Boeing 727-31. sedal number 20115, registration number N908JE APPLICABLE REQUIREMENTS (List specific sections) FAR 26.581 (a)(b)(1) FAR 26.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581(40)(d) FAR 26.1301 (a)(b)(c)(0) FAR 26.1357 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 25.1381 (a)(b) FAR 25.1322 (b)(c) FAR 26.1431 (a)(b)(c) CERTIFICATION - v.a,...a,, •17.4 .7 and. W. Low msg.... ...as 6,......k..., NONE s....•........d a a. ass iitni en, 4 Igiatoed•bee.iditattynesol t.a.......r..".+0•ni ...I., ...fa... win, intAL•Spepnmlurnied lived i• ace, .kntvh, Sac data & Equips's( Aspect. Daip Appeal Oa). Das Nee Ontstilin Owl Meth. (us. ssiiiii Ansis•A Mt •nimn..... a a• F•4• 0 A.,•••••• losullsks A pp sus') *nubbin. 0 Flasemesliapprost el I (at)Tbertfore la Apron that dab (E)Tterat SlOGVIV, b NPOrita) OASSIPICATWOCLI g amnatn.antrAoraranion rt a DERT-510087-NM Systems & Equipment 7 i 5icons No an J. n (I I40)5UPERSEDES PRIMUS EDITION OPOSOI4l3 FILENAME SC-721.INISDOC SDNY_GM_02759762 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246689 EFTA01331152

" SDNYGM02759768 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246690 EFTA01331153

DEPARTMENTOF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 1, 2001 AIRCFLAPT OR AIRCRAFT COMPONENT IDENTIFICATION - - PARE Boeing 72731 N one. Ramo. Hoicopter. et) Airplane MMIE (TrARTLTONT Jet Aviation Associates- WPB UST OF DATA IDENTITICATION • TRIO B727-16236-1261 5727-16236-1410 AT-855/RTA680 Antenna Installations, Sht.1-7, Rev A Dual FMS W/ 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 sen.rice by FM authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 72731, S/N: 20115 AP P UCABLE REQUIREMENTS Mist spec* semen,/ 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 vAth conditions under Part 183 of tho Federal Aviation Regulations, data listed above and on attached sheets numbered In accordance telthestabrished procedures and found to comply with applicable requirement. of be Federal Recommend approvalc/ wise data. I 441 Riergere Moroi, mandate. and En:nations of appointment 0 have been examined Aviation Regulations. SIGNA fURE(S) OF DESIGNATED ENRNEERING PIPRESEttfARVE(S) DESIGNATION mastitis/ I CLASSSICATION(S) David E. Haralson DEC. 14,-.4..__ DERT-810028-NE Structural FAA Form 8110-311140) SuPERNOE3PREVCCOS ENRON EA01202.4“ SDNYGIvl_02759769 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024669 I EFTA01331154

SDNYGM02759770 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246692 EFTA01331155

U.S. DEPARTMENT OP TRANSPORTATION FEDERAL AVIATION ADMMISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 18,2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARE Boeing MODEL B727-3I TYPE Oilf.l.e.ithlis &Avner. oat.) Airplane NAME OF APPLICANT Jet Aviation LLST OF DATA IDENTIFICATION MLR Jet Aviation Engineering Drawing No. B727-162364441, Dtd. 5/29/2001, Rev. A E.ND END END Note: The certification evaluation of structure. Structural Repairs on . . Notes: GPS Antenna Installation Betting B727-31, N908.1E, SIN 20115 END END END END END END END basis of this aircraft Includes FAR 2.5.571 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 6/182002. aspects only of this above listed data are approved is valid for the aircraft model and serial number is based on structural analysis on file at DER Service: 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 anrspea TIC SECTIOM) 25.301,25.303, 25305, 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 163 of the Federal Aviation Rerulations, data listed above and on an ached sheets numbered been examined In accordance with establisbed procedures and found to comply nith applicable requirements of the Aviation Regulations. O Recommend approval of these data I (We) Therefore pi Approve these data and limitations of have Federal SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau DEBT-510024-CE Structures FAA FORM 81103 (11-70) SUPERSEDES PREVIOUS EDMO N DER SERVICES PROJECT NO. 2001-082 SDNY_GIvl _02759771 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246693 EFTA01331156

SDNY_GM_02759772 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246694 EFTA01331157

O s . usCrow:men a TranspartatIon (Airframe, Fhiaia1 /Melon Adtallfigtetrn MAJOR REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No.2120-0020 For FM Use On Office Identification 5O- FcDo- / 7 g e INSTRUCTIONS: Print or typo all and disposition of this form. This report 51.000 for each such violation (Section entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for is required by law (49 U.S.C. 1421). Failure to report can result In a civil penalty not to 901 Federal Aviation Act el 1958). 1. Aircraft Make BOEING Model 727-31 Serial Na 20115 Nationality end Registration Mark U.S.A. N9OSJE 2. Owner Name (As shown MOE INC. on registration certificate) Address (As sham on regisuatlon certificate) 103 POUIX 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 POW ERPLANT PROPELLER APPLIANCE Typo Manufacturer %., 6. Conformity Statement A. Agency% Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES 1515 PERIMETER RD. WEST PALM BEACH. LTD. FL. 33406 U.S. Certified Mechanic CRS BYKR7S2D AIRFRAME 1,3. RADIO 1,2,3. LIMITED ME et ENG. Foreign Certified Mechanic X Certificated Repair Station — Manufacturer 0. I certify that the repair and/or alteration have been made in accordance with furnished herein is true and correct made to the unit(s) Identified In item 4 above and described on the reverse or attachments hereto the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information to the best of my knowledge. Date . 7/2/01 Signature of Authorized Individual IO. v •-•"' John K Urso. inspector. CC DX 7. App oval for Return to Service Pursuant Administrator BY to the authority given persons of the Federal Aviation specified below, the unit dentified in Item 4 was inspeoeed in the manner prescribed by the Administration and is 0APPROVED IC REJECTED FAA FIL Standards inspector Manufacturer Inspection Authorization Other (Specify) FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 72/01 Certificate Designation or No. EYICR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Ass S t a pp FAA Form 337 (1248) SDNY_GM_02759773 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246695 EFTA01331158

NOTICE • II 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 727-34 SMI 20115, N9081E, W/O 16236. INSTALLED 2 EA NEW GARMIN GPS ANTENNAS P/N 011-00134-00 CI29A). I EA AT FUSELAGE STATION 2844, BL 0.0. AND 1 EA FUSELAGE STATION 9343 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- IB, 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 I- 5 AS APPLICABLE CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE ME. SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.1340. CHAPTER I I, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER IL SECTIONS 5.8, 13. 15. I7-19 AND AC43.13-2A CHAPTER 2. PARAGRAPHS 21.22 & 27. ROUTING. LACING AND TYING COMPLIES WITH AC.43.13-1B. CHAPTER IL 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 INTOTHE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.I3-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A. CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN ENGINEERING REPORT IMER-836. REV Ut, DATED 6/10101. 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 Addidonel Sheets Are Attached * U.S. G.P.O 1990.761.753 SDNY_GIvl_02759774 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (1)246696 EFTA01331159

ASK CUBIYUS 002 -- • 1/2. DEBARTDLENT OP TRANSPORTATION PEP AL AVIATION ADSTINSTRATION STATEMENT OF COMPIIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Tune 6, I001 AIRCRAFT OR AIRCRAFT COMPONENT ID&MI7CATIGN MAKE ROPING' MODEL. NO. FTT77-1I TYPE (Alvaro. Radio, Nolkod•ocr. ac.) Airplane NAME OP ArnycANT __ In Ayrto/Iim ~cribbed...1 to LIST OP DATA IDENTIFICATION TITLE B727-162361413 OR Sbeets I - 3 (615101) END DRAWING - DUAL AIDOLIARY GPS ANTENNAS INSTALLATION NOTE: Approval for the sat:cm:al aspects relaxed to the above design data will be covered by a separate Form 8110-3 which will be issued for bbd Proof of SIG/4401e and will include required inspection item@ to «are COniMeal Airwor1DVIedb associated with this modification. END END PURPOSE OF DATA To provide a record of design approval of the above data applicable to 8127-31, SIN 20115, Rog/McGinn No. N9081E. for manofactaring and conformity. See NOTE above. APPLICABLE REQ<JDMILNTS (Lin spxilic atakos) FAR 25.6601 FAR 25.609 FAR 25.603 FAR 25.611 FAR 25.605 FAR 25.613 altT/F7CATION . Under antoriry bested by direction of inc AM...Mira:a brat In doconlanco with wodåaoro and Idnionom or men =Art port ILO of etc PoSinl Abiadoo Ittdoboor ' n. dart figs atom sad on *wart/ gran tonehored WA Wm teen ext=6ed hb nordariloth earth!~ pc:adorn and found ob tomfly bin!) ‘opikabk reoblretbents of Or )ØAblation Redubtims. 1 (IX) 7banfoto D Recommend approval of obese dart X Amore them dim (Sac NO113 above) SIONKIW(S) OP DESIGNATED REPRZSENTAIITVEIS) DEDGNA170N NUADLER(S) CLASSIFICATION(S) C2 / 9 2 ,$-C.C‘ (10. TILB -11/4-4C4Fnm• DERT - 510394 - CE STRUCTURES Kaman W. Damp= FAA Form 8110.3 (11-70) SLIPE12SEDES PREVIOUS EDITION shed 1 of SDNY_GM_02759775 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246697 EFTA01331160

SDNYGNI02759776 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246698 EFTA01331161

U.S. DEPARTMENT OF TRANSPORTATION ' FEDERALAVIATION ADMINISTRATION , STATEMENT OF COMPLIANCE WITH 171E FEDERAL AVIATION REGULATIONS DATE June 11, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENITEICAT/ON MAKE PORING MODEL NO. 8727-11 TYPE (Ainittne. Radio. Helicopter. etc.) AIRPLANE NAME OF APPLICANT _ JeLAyiltion Assneisted Ltd LIST OF DATA IDENTIFICATION 1TTLE ENER-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 B727-3I 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 eriwing MaimVnanrA 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 detailed in drawing 8727-16236-1413. Refer FAR PART 25 as to 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 8727-31 S/N 20115 and to show compliance to the following FAR's: APPLICABLE REQUIREMENTS (List sped& sermons) 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 CERTIFICATION - Under authority vested by direcdon of the Adminittnuor and in accords= with condidons and limitations of appohmornt under part IS3 of the Faders! Aviation Regulations. dam tined above and on Matched sheds cumbered N/A have been examined in accordance with established procedures and found to comply with applicable reqeirements of the Federal Aviation Regulations. I (k) Therefore O Recommend approval of these data X Approve these am (Structural aspects only) ' SIONATURE(S) OF DESIGNATED REPRESENTATIVE(S) DESIGNATION NUM:KRIS) CLASSIPICATION(S) 9(1 44 ,1fell 10- .0 1A , 7,4 -/-44--. DERT - 510394 - CE . STRUCTURES Kenneth W. Thompson .. FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION sheet I of I SDNY_Ghl_027597 7 7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246699 EFTA01331162

SDNYGNI02759778 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00246700 EFTA01331163

0 j MAJOR REPAIR AND ALTERATION tIS Depentrant d Tronsoortatloi (Airframe, Poworplant, Propeller, or Appliance) Faint Aviation MmIntetnitca Form Approved OMB No. 2120-0020 For FAA Use Only Office identification INSTRUCTIONS: Print or type all entries. Soo FAR 43.9 Appendix B. and AC 43.9-1 (or subseque t revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can re tilt in a civil penalty not to exceed 31.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEINO Model 727-31 Serial No. 20115 Nationality arid Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shovwn 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. COS:tate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL 33406 U.S. Certified Mechanic CRS EYICR782D AIRFRAME 1,3. RADIO 1.2,3. LIMITED A/F & ENG. Foreign Certified Mechanic x Certificated Repair Station — Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished heroin Is true and correct to the best of my knowledge. Date 7201 Signature of Authorized Inane u ie.•(.4—e-- John K. Urso. Inspector. 7. Approval for Return to Servl Pursuant Administrator BY to the authority given persons specified below, the unit identified in item 4 was inspected in the manner proscribed by the of tho Federal Aviation Administration and is ISI APPROVED 0 REJECTED FM FIL Standards Inspector Manufacturer Inspection Authorization Other (Specly) FM Designee X Repair Station Person Approved by Transport Canada Alnyczthiness Group Date of Approval or Rejection 717/01 Certificate or Designation No. EYKR782D Signature Resale K. Bysof Authorized Individual trom. Managa Quality Asnses FAA Fenn 337 (1 2 4 el SDNY_GM_02769779 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024670 I EFTA01331164

NOTICE • Weight and balance or operating lirOalion changes shall be entered in the appropriate aircraft record. An alteration must be compatible with elf pvvious afteratione to assure continued conformfty WM the applicable alnyorthiness requirements. & Description of Work Accomplished Of more space is required, attach additional sheets, Idea* with aircraft nationaltly and registration mark and date work acconplished) BOEING 727-31. SIN 20115. N908.TE. 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 I & 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 06/01, 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-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 BL SHEETS 1 THRU 21, DATED 001112001I WAS COMPLETED IN ACCORDANCE WITH AC43.13-I B. CHAPTER I I, SECTION 3. PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-IB, CHAPTER 4. SECTIONS 1. 2. 3 AND 4, CHAPTER 65 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.I B. CHAPTER II. SECTION 0. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13.IB, CHAPTER II. 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 II, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURERS 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. 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 * V.S. G.P.O 1990-781.753 I SDNY_Gtol_02759780 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246702 EFTA01331165

a DIMItTMENTOF TPANSPOlTATION FEDIDlel. AVIATION ACIaltillSTPATION 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, Reliever. de) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-352, Initial Release, dated 05/25101 B727-16236-580, Initial Release, dated 05/25/01 8727.16236-600, 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 26. 1322 (b) FAR 25.1529 FAR 25.1351 (a) CERTIFICATION - thid.,....iumy void by dirstdoe atata Wet obeys W.. musing 'Neu mowed NON? hen a the Adaishirlase unt ha accentuate oh* fl atness and inaniadas Mappaianium wider Pan HU gar Fatal Mist.. Fteentaitoss We. maws Is accordance one esuatetstod smears e•O roma inesply eta nvikak ...mono trim room Aaiun* these data & Ed oiproatt Aspects. Desiga Approval Only. Does Not Constitute lostalls doe Approval/ Repladoes K ReC040Mend Approval of I (We)fberefore a Approve Mete data (Systems SIGMA tit PORESEXPATIST(S) DESIGNATION NUMMER(S) CLASSIFICATIONS) DERT-510087-NM Systems & Equipment o an J. ran FAA Form 8110-3 I-70)SUPERSEDES PREVIOUS EDMON ORO 901413 F/LIDUMIESD-727•CAD•PWR.DOC SDNY_GM_02759781 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246703 EFTA01331166

SDNY_GM_02759782 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246704 EFTA01331167

C r • OEPARIMENT OF TRANSPORTATION OAR FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 10, 2001 AMMAR OR ANICRAFT COMPONENT IDENTIFICATION MANE Boeing MODEL NO. 727-31 TYPE (Neer* Raba. Kelomtmetc.) Airplane NAME Cf APPUCANT Jet Aviation Associates- WPB LIST OF DATA IDENI1FICATION iTILE 8727-16236-1352 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 We monde sccdoes) 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 AdministnEcc and in accordance With OX4100t19 under Pal 183 of the Federal Aviation Replationsidata wee above and on attached sheets numbered In accordance wall established procedures and found lo comply Wei applicable requirements of the Federal K Recemmend approval of :nese data. OLaJI I ( X Therefore Approve ace date. and Iota lons of appointment 0 have been examined Aviation Regulat OM. SIGNATURE(S)OF DESIGNATED EN3INEERING REPRESENTATIVE(S) OES:ONATON NUMBER(S) CIASSWICATIONISI David E. Haralson 1:7O-ecr. N0,01.-- DERT-810028-NE Structural onn 8110-3 (1140) = SIeseK¢ PREWOUS EDITION SDNY_GM_02759783 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246705 EFTA01331168

SDNY_GM_02759784 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246706 EFTA01331169

0 us osiiiiviva es Trr, Federal annifinninion (Airframe, swum Office MAJOR REPAIR AND ALTERATION Poworplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Identification 50- r5Do-i7 afif INSTRUCTIONS: and disposition 51,000 Print or typo all of this form. This report for each such violation (Section entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequo I revision thereof) for I is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to 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 $1701471 JEGE INC. on registration certificate) Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 —, 3. For FAA Use Only 4. Unit Identification 5. Typo Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWER PLANT PROPELLER APPLIANCE Typo Manufacturer ,.. 6. Conformity Statement A. AgencYs Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES 1515 PERIMETER RD. WEST PALM BEACH. LTD. FL. 33406 U.S. Certified Mechanic CRS EYKR782D AIRFRAME 1,3. RADIO 1,2,3. LIMITED MP & ENG. Foreign Certified Mechanic X Certificated Repair Station Manufacturer D. I certify have furnished that the repair and/or alteration been made in accordance with herein Is true and correct made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information to the best of my knowledge. Date 7/2/0I Signature of Authorized Incavklual John K. tine. Inspector. N....“...._, 7. Approval for Return to Servl Pursuant Administrator BY to the authority given persons of the Federal Aviation specified below, the unit dentified In item 4 was erected In the manner prescribed by the Administration and is El APPROVED El REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (SPecifY) — FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group of Authorized Individual K. Bystrom. Manager Quality ASSWIDC eligig -c- Date of Approval or Rejection 712/01 Certificate Designation or No. EYKR782D Signature Ronald , FAA Form 337 ozem SDNY_Glvl_02759785 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246707 EFTA01331170

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft recant An alteration must be compatible with aft previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identity with aircraft nationality and registration mark and date work accomplished) BOEING 727-31, S/N 20115, N9081E. W/O 16236. INSTALLED A UNITRON 60 HZ CONVERTER P/N PS-62-66D AND 26 EA CABIN °MUTTS 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 I THRU 5, ITILED -CABIN NO. 2 60 HZ SYSTEM REFERENCE FAA FORM 8110-3 DATED 6/7/01, BY SYSTEMS & EQUIPMENT DER. NO. DERT-510087-NM. STRUCTURAL DRAWINGS: • B727-16236-1580. REV IR. DATED 911/01, SHEETS 1 THRU 7. TITLED - CABIN NO. 2 60 HZ EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8I10-3, DATED 6/13/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE AN EMI TEST, REPORT NO.: B727-16236080 REV IR. SHEETS 5, DATED 06119/01 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.B-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.I3-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER I, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2 MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. TEE 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-I B. CHAPTER 4, SECTIONS I. 2. 3 AND 4, CHAPTER 6, SECTIONS 3 AND & HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS I- 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 AC43.13z It CHAPTER II. SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-I B, CHAPTER I1. SECTIONS 5-8. 13, 15, 17-19 AND AC.43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING. LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER I I, SECTIONS 9.12 WIRE MARKING COMPLIES WITH AC43.13- I B SECTION 18 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 4t 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. 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 1990-781-763 SDNY_Glvl_02759786 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246708 EFTA01331171

DEParkitIT Of TRANSPORTATION STATEMENT OF COMPLIANCE WIATIA THE FEDERAL floN lw" 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 B727-16236-362, Initial Release, dated 05/25/01 B727-16236-580, Initial Release, dated 05/25/01 8727-16236.600, 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 26.1363 (a)(b) FAR 26.1301 (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 26.1629 FAR 25.1351 (a) CERTIFICATION - orma.o.lts mud by &yaks data Estal •bekt and us shucked gnu eakend NONE kin of Ot Adalek*In satIlkliftenbeke kith cort4kMes nil Speknikee of app•Satewst nier nn is, ktOt Eaten. AWila. Reg...kink bent *maimed to makrtfrate with klalksberd prikkluils sad bask ki on*, kid. kpplkabk ',eineme of thit Etkeni MOS, dam & Equipment Aspects, Deign Approval Only. Des Not Constitute hatallatioa Approval) Rekalidea O Recommad approval albeit I (We) 7Iterefore F2 Appieve these data (Systems =NATE osnusorrAnYtm orsictunon NUMBEATO CASSIOCATIONIO lne-O--. DERT-510087-NM Systems & Equipment No an J. an AA Form 8110-3 I-70)SUPERSEDES PREVIOUS WTTON GPO 901-613 sun. SC-72LCAB-PWR In SDNYGlvl_02759787 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246709 EFTA01331172

SONY GM 02759788 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246710 EFTA01331173

a C DEPARTMENT Cr TRANSPORTAPON FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 13, 2001 NRCRAFT OR AIRCRAFT COMPONENT ICENTIPICATON FAKE Boeing MODEL NO. 727-31 TYPE (Airplane. Radio. ireaoretexem) 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 REOUIRFJJENTS Mkt speedo sealsrei 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 Past 183 of the Federal Aviation Regulalrentdsita Ested above and on attached sheets numbered In accordance with testae:I:had procedures and found to comply with eppdcatte reqthements of the Federal i ( X Thereon Gootameed aPPIWal of these data Altera.* Dm data. and limitations of appoinreere 0 have been examined AVAtrall Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRF-SF-IITATIvE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) David E. Haralson Pmde. /10,./...- DERT-810028-NE Structural oan 8110-3 iii40)SUPERSE0tty names tornat EJI01210.6ac SDNYGlvl_02759789 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002467 I I EFTA01331174

SDNYG1,102759790 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246712 EFTA01331175

'ID us Depinsta 01 TrerwolaWn Firdnil sinumersoon (Airframe, *Nam MAJOR REPAIR AND ALTERATION Poworplant, Propeller, or Appliance) Form Approved OMB Na 2120-0020 For FAA Use 0i)ly Office Identification c0— /-57jO- 17 e-ta INSTRUCTIONS: and disposition 81.000 Print or typo all of this form. This report for each such violation (Section entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for 'nal ens is required by law (49 U.S.C. 1421). Failure to report can ro ult In a civil penalty not to xceod 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark US.A. N9O&TE 2. Owner Name (As shown MGR INC. on registration certificate) 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 AJRFEAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate Na JET AVIATION ASSOCIATES 1515 PERIMETER RD. WEST PALM BEACH. LTD. FL 33406 U.S. Certified Mechanic CRS EYKR782D AIRFRAME 1,3. RADIO 1,2,3. LAMED MP & ENG. Foreign Certified Mechanic X Certificated Repair Station Manufacturer D. I certify have furnished that the repair and/or alteration been made in accordance with herein Is true and correct made to the unit(s) Identified in item 4 above and described on the reverse or attachments hereto the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information to the best of my knovetedge. Dale 7/2/01 Signature of Authorized Individual John K. Urso. Inspector. 7. Approval for Return to Service Pursuant AdrrdnIstrator BY to the authority given persons of the Federal Aviation specified bedew, the unit Administration and is &sniffled in item 4w inspected in the manner prescribed by the O REJECTED .7J APPROVED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specity) FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 7/2/0I Certificate Designation or No. EYKR782D Signature of Authorized Individual Ronald K. irom. Manager Quality Bys FAA Form 337 0248> SDNY_GM_02759791 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002467 I 3 EFTA01331176

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be avowable 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 accompffshed) BOEING 727-31, S/N 20115. N9083E. W/O 16236. INSTALLED AN AIRCELL ATG.01 FLIGHT PHONE SYSTEM CONSISTING OF AN ANTENNA PIN CI-5O30, A TRANSCEIVER PIN 900002-2, and AN ANTENNA MATCHING UNIT P/N 83518, 4 EA HANDSETS P/N 440-10035-001 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. 111, DATED 4/30/01, SHEETS I THRU 3. TITLED- AIRCELL ATO.01 AIR /GROUND TELEPHONE REFERENCE FAA FORM 8110.3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.ER. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-I330, REV. A, DATED 529/01, SHEETS 1 THRU 4, TITLED- AIRCELL ATG.01 AIR I GROUND TELEPHONE ANTENNA INSTALLATION REFERENCE FAA 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. -WILED -AIRCELL EQUIPMENT INSTALLATION REFERENCE FAA. FORM 8110-3, DATED 6/3/01, BY STRUCTURAL D.ER. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER AIRCELL ATG.01 FLIGHT PHONE SYSTEM INSTALLATION MANUAL REV IL DATED 611 I/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 43.13-1B, 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.I3-2A, CHAPTER I, 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 'MU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-18, CHAPTER II, 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.I3-1B, CHAPTER 7. SECTIONS I- 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-IB, CHAPTER 11, SECTION 4. ELECTRICAUELECTRONIC 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 MANUFACTURERS INSTRUCTIONS AND AC43.13-2A, CHAPTER 2. PARAGRAPHS 21 THROUGH 26 AND CHAFFER 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 IQ 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 AFFECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATEA I 12001 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 Addtional Sheets Are Attached * U.S. GPO 1990.761.753 SDNY_GM_02759792 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246714 EFTA01331177

a _bgAy-29-01 01:5DP N J Curran 352 243 1011 P.IJ/ DEM MUM a TUNSIORTAT KIN ITDISAL /MAT /COI NatroOSTIATCW. STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05129/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE IAIIDIOne. Rat*. fkikopIer. ete1 Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B72746236430, Initial Release. dated 04/30/01 AlRCELL AGT.01 AIR/GROUND TELEPHONE PURPOSE OF DATA In support of major alteration to Boeing 727-31. serial number 20115. registration number N9OSJE. APPLICABLE REQUIREMENTS (List specific sections) FAR 26.581 (a)(b)(1) FAR 25.1357 (afle) FAR 25.889 (aX4) FAR 25.1431 (a)(b)(e) FAR 25.1301 (a)(b)(e)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) FAR 25.1361 (a) CERTIFICATION - Wt. rOn.liy....4 by ilima II Mgt St AIS/ISInall ill OtiOalate dos Wed den Was ataid tinnosbn,4 HONE Ins ton onistd ka Ilaelksitt Ilardeds. O Rename/DO mpprcnnol orange date I (We)T Denton la Apply/web/se tlics (Spleen & EalfSeatat Aspects as aikmen...• swan.. d ors.......«. .4.5 eaaflobefplotalun mll fond iv —* ebb npbnkk Dear Approval Osly, Doe Nit Contilirlt h. la a A. raunsaA.s. ;twins., nialnann *Ia. flan, miry. Inlathithe AppaNa0 SICNATVet Watt 07frtE517 , 4,0, ttrattll DISIGNATIOni M,Mma) CIASSIOICATONSI A- A) DERT41008741M Systems & Equipment No n J. C n rA - r-- --- - • ) 901411 FILDIAML SC-7274URCELLOCC SDNYGIvl_02759793 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246715 EFTA01331178

SDNYGM02759794 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246716 EFTA01331179

U.S. DEPARTMENT OF TRANSPORTATION FEDFItal AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Jane 18,2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL TYPE ~L.% AS,A tiegaId• 114 NAME OF APPLICANT Boeing B727-3I Airplane Jet Aviation LIST OF DATA ilnallsR.AIRsn limn Jet Aviation Aircell AGT.01 Air/Ground Telephone Antenna Installation Engineering N Drawing o. Beoing B727-31, N9OSJE,S/N 20115 B727-16236-1330, END END END_END END END END END Dtd. 5/29/2001, Rev. A Note: The certification basis of this aircraft includes FAR 25.571 Damage -tolerance and fatigue evaluation of structure. Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of END END _ the structure must be performed before 6/18/2002. Notes: 1) The structural herein. aspects only of the above listed data are approved 2) This approval is valid for the aircraft model and serial number listed below 3) This approval is based on structural analysis on file at DER Services corporate office in Ft. Lauderdale, TV. Model No. B727-3I Serial No. 20115 PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LIS r SPECIFIC SECTIOMS) 25301, 25303,25.305,25J07, 25.601, 25.603. 25.605.25.609, 25.613 authority mad by direction of Me Administrator and in monism with cOnclitiOn and ti anorak Federal Aviation Regulations, data listedabove sad on *Mak d sheet. eves cm of CATION- Under Lexs1EI appointment under Part bare beta emitted Is accordance with established procedures and freed to comply with applicable mainmasts alba ra Ariake Regulation,. O Recommod approval *Mae data I (rye)Therefore Fil Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBERS) CLASSIFICATIONS) Robert J. Ilielgau DERT-510024:CE Structures 4f.------. 4,45 FAA FORM 81104 (II-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001-082 SDNYGlvl02759795 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246717 EFTA01331180

SDNY_GM_02759796 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246718 EFTA01331181

DEPADEPARTMENTOF TRANSPORTATON FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 3, 2001 AIRCRAFT OR AIRCRAFT COWONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Aaeems. Read NOtercterte) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA OIRCITICATION TIRE B727-16236-1270 8727-16236-1331 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 FM authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, SIN: 20115 APPLICABLE RE-OUIEFIAPNTS Rid Speak section') 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 vested by direction of the Administrator and in accordance with conditions under Pm 183 of the Fedora, Av4ition Regulations,data listed above and on attached sheets numbered In armaidmice with established procedures and found to comply Mrh applicable requirements of Federal I ag llurefere i Recommend approval of these dais. APprove coca data. and limitations Cl appoMment 0 have been examined Aviation Regu'ations. SGNATURE(3) CC DEVGNATED ENGINEERING REPRESENTA1TVEr$1 DESIGNATION tathaftEurgf CLASSUICAMONS) David E. Haralson DEC. Awe.-- DERT-810028-NE Structural orrn (1,-70)SUFVLSEOES MEMOS °MON ER011074(4 SDNYGlvl_02759797 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246719 EFTA01331182

SDNY_GM_02759798 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246720 EFTA01331183

L) DaAtenittolOFTRAIMOVIAllai . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING r NO. 727-31 TYPE t*Avis.itaRedds.v. viv.4 AIRPLANE •IAME OF APPLICANT JET AVIATION LIST OF DATA nava/EAU* MU A.T.E. INC. STRUCTURAL REPORT No. ATE6112001 BOEING 727-31 SIN 20115, AERO-M SATCOM ANTENNA INSTL, UPPER B.S. 360.390; OPS 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) t PIOTE• REOU(RED INSPECTIONS ATTACHED THESE DATA APPLY ONLY TO HOED* 727-31 SIN 20115 PURPOSE OF DATA TO APPROVE DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-3I SIN 20115 APPLICABLE REQUIREMENTS Rai wait xviivei FAR 23311 (STRUCTURAL ASPECTS ONLY) CERTIFICATION - Ueda authority vestal by &mica &the AdealnidesMe sod in matdance with conditiceu and amassnit • of appolevocM caw Pan 1113 ante Fedaal Aviation Replations, data listed above and en attached sheets maned loft haw beta ittatained In azawdatice with atatilithott mantras and found lo comply with appEcable recpiranents or the Federal Aviation lissuladoon Paammmd approval I (0) re k r Approve data of these . SO:Ran/REM OF DESIGNATED ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATION(S) IiZ— e n/ 0 /Lot . DERT-510333-CE STRUCTURAL FAA Fens 9110-3 wad SIAMIS100 pitman crow. Of 0101411 SDNYGlvl02759799 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024672 I EFTA01331184

SDNYGM02759800 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246722 EFTA01331185

0 MAJOR REPAIR AND ALTERATION us Dorris% ol Tramp:aka (Airframe, Powerplant, Propeller, or Appliance) fibril Minkel AchnintsinUcc Form Approved OMB No. 2120-0020 For FAA Use On! Office Identification SO-F5 Do - i 7 Int 1 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instruct' 1 and disposition 1 this form. This report is required by law (49 U.S.C. 1421). Failure to report can to tat in a civil penalty not to o 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. N91:187E 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 APPUANCE Type Manulacturbr 6. Conformity Statement A. Agencys Name end Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1615 PERIMETER RD. WEST PALM BEACH. FL 33406 U.S. Certified Mechanic CRS EYKR782D AIRFRAME 1,3. RADIO 1,2,3. LIMITED A/F & ENG. Foreign Certified Mechanic X Certificated Repair Station — Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished heroin is true and correct to the best of my knowledge. Date 7/2/01 Signature of Authorized Individual John K. Urso. Inspector. X-11L-r- 7. Approval for Return to Service Pursuant Administrator BY to the authority given persons specified below, the unit dentified In Item 4 was spected In the manner prescribed by the of the Federal Aviation Administration and is El APPROVED Ull REJECTED FM Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Ainvonhiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYICR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 0243) SDNY_GM_02759801 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246723 EFTA01331186

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with al 1 previous alterations to assure continued conformity rah the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach ackNional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, Sal 20115. N9081E. W/O 16236. ACCOMPLISHED AN UP-GRADE TO THE EXISTING HONEYWELL WEATHER RADAR SYSTEM FROM PRIMUS 870 TO PRIMUS 880. REMOVED THEY 1 & 2 WC-870 CONTROLLERS P/N 7008471-803 AND INSTALLED WC-880 CONTROLLERS P/N 7008471.405 (ISO 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 (ISO C63c). INSTALLED A HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM CONSISTING OF AN 1.11-860 PROCESSOR P/N 7011822-904 (ISO C110) AND AN AT-855 ANTENNA P/N 7014062-901 (ISO CI10). THE LIGHTNING SENSOR SYSTEM INTERFACES WITH THE PRIMUS 880 RADAR SYSTEM THRU THE If 1 & 2 WC-880 CONTROL t FRS. RELOCATED EXISTING SECURITY SYSTEM ANTENNA PM 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. R. DATED 5/29/01, SHEETS 14 2, TITLED - WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) REFERENCE FAA FORM 8110-3 DATED 6/7/01. BY SYSTEMS & EQUIPMENT D.E.A. NO. DERT-510087-NM. • B727-16236-261, REV. IL DATED 4/10101, SHEETS ITHRU 3, TITLED- HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM REFERENCE FAA FORM 8110-3 DATED5/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPOR]% • B727-16236-1261, REV. A, DATED 5/30/01. SHEETS 1 THRU 7, TITLED- AT-855/RTA-880 ANTENNA INSTALLATIONS REFERENCE FA.A. FORM 8110-3, DATED 6/1/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE • B727-16236-1242, REV. It. DATED 5/21/01, SHEETS 1 & 2, ITILED - LSZ-860 LIGHTNING SENSOR EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3, DATED5/28/01. 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 writ NO DISCREPANCIES. AN EMI TEST, REPORT NO. B727-1'6236-080, REV IR DATED 6/19101 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC WADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.I3-2A, 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 111, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH 43.13-IB, CHAPTER 11, SECTION 3. PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.134 B. 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. I3-1B, CHAPTER 11, SECTION 4. ELECTRICAUELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-18, CHAPTER II, 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 1I, 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 ME AIRCRAFT RECORDS TAW AC43.13-1B, 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-1160 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 0 Additional Sheets Are Attached * V.S. G.P.O 1990-761.753 SDNY_GM_02759802 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 1x)246724 EFTA01331187

DOARTMDFFOF TIWIStallATICO4 MODAL AVIATION AD/AINISTILA11011 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 72741 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 • !... • 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 25.5131 (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 26.1629 FAR 25.1316 (b) CERTIFICATION - thocknAtioDy voted by dtrAik. mu rums above mad m awns .Neu steams NONE Nn et OA Adnosainoor and La Mardsett with csaditlass mad Itaitadoas or appokause•A sidfr Wei tunic.' h. attentimott wilb ettailabed pnadern awl fend to comply with VOW* these data & Equipment As Dales Approval Only. Dom Not Constitut nn lilathe /Wen' Minas PnilaSesh requimentni the (atm, Aristke Installation Approval) Reptant O Retommend approval of I ere)fbereare al Approve these data (Systems SIGNATU FD REFILIZENTATIVOS) DESIGNATION MUDIEMS(S) ClASSMCMONT /zap. DERT-510087-NM Systems & Equipment an J. ran FAA Form 8110-3 1-70) SUPERSEDES PREVIOUS EDITION GPO 901413 FlIEHAME SC-7274tDR_DDC SDNYGIvl_02759803 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246725 EFTA01331188

SDNYGM02759804 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246726 EFTA01331189

DENJUUDIT OF lltANSPORTAIIPN FEMME AVIATION ADMDLISTAATION i . STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Booing MODEL NO. 72731 TYPE (Airplane, Retro, Hdicarier. ac) Airplane NAME OF A P PI. ICA NT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-260, Initial Release, dated 05/29/01 WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) PURPOSE OF DATA • in support of major alteration to Boeing 72741, serial number 20115, registration number N980JE. APPLICABLE REQUIREMENTS (List specific statees) FAR 25.681 (a)(b)(1) FAR 26.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) . FAR 26.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION - Doter saoierity nand by tettlaa tato Sand &boat al ea .rasp &nen enabend NONE Inn tribe Adnkatrater nal I. malting ',nib atilt:nu w linianieu otatgaa'ainnel utter bent eannIsta ia &contact with acsallabed prontnand And in comply wad appluatit these dais & Equipment Aspects. Dcsltn Approval Only. Dom Not Constitut n,1 1u aloha Eiden: Aviation *,cation, intim:nit of Ma Enka, Minim Installs tloo Approval) Regattap. K RetOMITItIld approval of I evo Terefore tEl Aopove these data (Systems SIGNA F DEM C strustransivErn DESIGNATION MOSSO) RASSIFICA110/1(1) DERT-510087-NM Systems & Equipment o an J. FAA Form 81104 ill-anSUNERSEDES PREVIOUS EDMON GPO 901-613 EILESIANt& SC-7274UORDOC SDNY_Glvl_02759805 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246727 EFTA01331190

SDNY_GM_02759808 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246728 EFTA01331191

May-29-O1 O1:58P N J Curran 352 243 Steil OUNUNIFIll Of TRANS/ORTATICet 1100.Q. MIATIONAOMSCISTILOP3N STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 72741 TYPE Misplace. Rothe. ittlieopeet. .lc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TIRE 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 N90I3JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 26.1367 (a)(c) FAR 25.869 (a)(4) FAR 26.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) " FAR 25.1351 (a) CERTIFICATION - veer. =nem, wadi lry tombs' aro Aeolakintor an ea seensnee nu mains na seinen senoncena nen Pen inane erns Minim Lynne. *to raid O,nad 1d st,......a...• _I;(32INE M Fa moist. Is newts, kb swam mate,. - kind ....pi was meats ..ass art frees swim,. Iterlanos. O Reonnotod approval cube Oats I Paeyllternote a Approve One data (Spiess At tepennest Aspects. Delp Approval Ooty, Don Not Ccestitate lostallados Approval) SICAAT r lib itnoznacIrrnin(a OtSICNATION MOMS) CULUMCA110.110) rfc l C gin. 4 0 _ DERT-510087-NM Systems & Equipment 0 No an urran FAA Form 8110-3 el 1.70) SUPODILDES PREVIOUS EDITIONOOS01413 FELENAME.SC.4274.7OSNSILDCC SDNYGIvl_02759807 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246729 EFTA01331192

SDNYGM02759808 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246730 EFTA01331193

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 1, 2001 AIRCRAFT OR MRCRAFT COMPMENT IDErinFICATON MAKE NOMA NO. TYPE (AarIones Redo. Helms:W. oI ) NAME OF APPOCJINT Boeing 727-31 Airplane Jet Aviation Associates- WPB UST OF DATA IDENTIFICATION TITLE 5727-16236-1261 AT-855/RTA-880 Antenna Installations, Sht 1-7, Rev A 6727-16236-1410 Dual FMS W/ 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, Mt 20115 APPOCASTERECIUREMENTS (Use speoac sedan) 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 OrnitilliOnS of appointment under Fart 183 of the Federal Aviation Regulations, data fisted above and on attached sheets rermbered 0 have been examined In acCordance Ath established procedures and found to Consul), with apigicabre fer:cements Of the Peden! Aviation Regulations. ReCOSIIRS.VS accesSill 04 thesis two. 1 (IX Therstore *Move these date. SIGNATURE(S)OF DESIGNATED ENGINEERING REPAESENTA TIVErR DESIGNATION MAMER(S) ,• ; . CIASSFICATION(51 ir David E HaralsOn P...ie. N DERT-810028-NE .7,, , Structural . .14. •r: OIm ti sUPEASEDESTALMOOSIMII011 esone2ser SDNY_Glvl_02759809 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024673 I EFTA01331194

SDNYGM02759810 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246732 EFTA01331195

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 28, 2001 AIMCRAFT OR NACRAFT COMPONENT iDENTW1CATICN ALINE Boeing MODEL NO. 727-31 TYPE (AliSant Real, Ifetcomer. etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDEMTFICAMON TITLE 8727-16236-1262 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 Oh DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPUCABLE REWIRE:MATS Rat speak cocoons) 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 *action of the Admire-.eater and In accordance with conditions under Pan 183 ad the Federal Aviation Regulalieas, data listed above and on attached sheet: numbered In accordance with established procedures and found to comply with applicable requirements of ME Federal i 4 Theielore Recommend approval of these dam 0 Appian these data. and limerdlons of appoinenent 0 have been examined Aviation Regulations. SIGNAIL DESIGNATED EENGGINEERiUG REPRESENTATIVE(S) DESIGNATION R( ) CLASS ROMS) David E. Haralson Po-ee. wont_ DERT-810028-NE Structural FAA Form 8110-3 (ii-le) SUPERSEDES PREVIOUS ELMO/4 ER012054“ SDNY_Glvl_0275981 I SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246733 EFTA01331196

SDNYGNI02759812 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246734 EFTA01331197

OEPARIMENtOF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPUANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDEMIFICADON MAZE Boeing MODEL NO. 727-31 TYPE (iMolisne. Rado. lixtinemr, et) Airplane NAME Of APPUCONT Jet Aviation Associates- WPB UST OF DATA IDEM1RCATPON THE B727-16236-1262 8727-16236-1342 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 APPUCABLE REOUIRPMcNTS NV specifeneirenta 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 Adadon RepulatlenS. data Wed above end on attached sheets numbered In accordance with estabilshed procedures and found to comply vah appkablo requirements of the Federal I DX 'Therefore 2 ReCCOVIlet4 approval of those data. Approve IMSOCiati. and limitations of appointment 0 have been examined Aviation Regulaliorm. SIGRATURE(S)OFDESIGNATEDENDerLEANGREPRESENTATNEtS1 DESIGNATIONriumaER(R) CumSIFICADOMSf David E. Haralson ase. th.....e.__ DERT-810028-NE Structural FAA Form 8110-3 ulTre SUPERSEDES PREVOll5 ECOION ER01205 doc SDNY_ GE/1_02759813 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246735 EFTA01331198

SDNYGNI02759814 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246736 EFTA01331199

• 0 4 us Dpartenint al Transportilkm NSW AdmInIstratIon (Airframe, Avtattal MAJOR REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Uso Only Mt °Identification 62,6 50-fisbo- t7 INSTRUCTIONS: and disposition 51,000 Print or type all of this form. This report for each such violation (Section entries. Soo FAR 43.9 Appendix B, and AC 43.9-1 (or subseque t revision thereof) for ins is required by law (49 U.S.C. 1421). Failure to report can re ult in a civil penalty not to exceed 901 Federal Aviation Act of 1966). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N9081E 2. Owner Name (As shown MOE INC. on registration certificate) Address (As shown on registration certificate) 103 FOULK RD. sm 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 1515 PERIMETER RD. WEST PALM BEACH. LTD. FL 33406 U.S. Certified Mechanic CRS EVICR782D AIRFRAME 1,3. RADIO 1,2,3. ME & ENG. Foreign Certified Mechanic K Certificated Repair Station Manufacturer D. I certify have furnished that the repair and/or alteration boon made in accordance With herein is true and correct _LIMITED made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information to the best of my know/edge. Date 7n101 Signature of Authorized indi ual ee John K. Urso. Inspector. it.... K. Ct--c- 7. Approval for Return to Servl Pursuant Administrator BY to the authority given persons of the Federal Aviation specified below, the unit dentified in item 4 w inspected 'n the manner prescribed by the Administration and is I21 APPROVED CI REJECTED FAA Flt. Standards inspector Manufacturer Inspection Authorization Other (Specify) .. Date FM Designee X Repair Station Person Approved by Transport Canada Ainvorthiness Group of Approval or Rejection 7/2/01 Certificate Designation or No. EYKR782D Signature of Authorized Individual Ronald K. flystrom. Manager Quality Assurance. 4 FAA Form 337 (12-04) SONY_CM_02759815 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246737 EFTA01331200

NOTICE Weight and balance or operating limitation changes shall be entered In the appropriate aircraft record An alteration must be compatible with ad previous alterations to assure continued °creamily MV) the applicable airworthiness requirements. 8. DesaiptIon of Work Accomplished (If more space Is required attach; additional sheets, Identify valh aircraft natiimality and registration ma* and date work accomplished.) BOEING 727-31, S/N 20115. N908.113, WIG 16236. ACCOMPLISHED A WAS CHANGE 7 UPGRADE TO THE EXISTING HONEYWELL WAS 11 SYSTEM PREVIOUSLY INSTALLED UNDER PAGE AVJET CORPORATION SW SA3094.50 DATED 8/24/93. REFERENCE FAA. FORM 337 DATED 8/25/93. THE WAS 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 B CHANGE 7 PROCESSOR WAS INSTALLED AND TESTED IN ACCORDANCE WITH TIMCO ENGINEERING ORDER DOCUMENT 0 IT012E006, 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 WA TO THIS INSTALLATION BY PROCESSOR P/N. THERE IS NO CHANGE TO THE AIRCRAFT WEIGHT AND BALANCE THERE IS NO CHANGE TO THE AIRCRAFIS MAINTENANCE FOR CONTINUED AIRWORTHINESS REQUIREMENTS DUE TO THIS INSTALLATION. THE REQUIRED F.A.A. APPROVED HONEYWELL INC. WAS U FLIGHT MANUAL SUPPLEMENT DOCUMENT "ICAS-APPS-0294, REV A, DATED 3/21/00 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL _END K AddaMnal Sheets Are Attached * U.S. G.P.O 1990-781-753 SDNY_GM_0275981 6 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246738 EFTA01331201

eornmtmtcations Aviation Communications Si Surveillance Systeme A]0.V»]-Ylce May 16, 2001 TIMCO 623 Radar Road Greensboro, NC 274 Artm: Mr. Gregg Stutes Re: Letter of Authorization to use technical data Dear Mr. Styles, 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 ("Data") is the L-3 developed data used to apply for the following FAA certifications: Supplemental Type Certificate STC SA4834NM, as defined by ML4070349, for B727 aircraft. L-3 Authorization to use Data is limited to the following B727 aircraft tail number, namely: • B727 S/N 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. SDNY_GAl_02759817 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246739 EFTA01331202

SDNYGNI02758818 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246740 EFTA01331203

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 actions 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, Certifi Fax Pinter., 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 F.W. (Bill) L ch Agent for L-3 Communications, ACSS SDNY_GM_02759819 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246741 EFTA01331204

SDNY_GM_02759820 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246742 EFTA01331205

%Wad Zinn of arks Btpamnent of transportation —OW ablation administration *pplemental `Egg &vacate ireap...—/As4414a.e..120 SA3094so} Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 artiead.44,66.70.4.44-40...24r/a.,,,e1h.henaa...datmactmandeoan. ..Itien,fluti.ohe tatesteoruench41-.4‘.euirecordhassirrewmastehrearl glerlallangt, etraSideci-40. - gertieanah•-: A3WE 405-4: Boeing 727-100 Series 25 i ts Federal Aviation SlaP iAn'9491. -Pl r ta r ; 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. ...eneiatientwazeage-naedion.1 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. S terlOca4,2,tae.awcplinrcerlepareartt pY dehaaleiysrewalehrilrentaina.Atwra.ma— wetuhretsUafriteheiwoveXectiwobwhettowhinati:wit..eZhir sa edelftecheehleaaed.100 Lie .51triitiwih/m/..h a, : -47.iteliesetenew: October 21, 1991 January 15, 1992 Y04. ietahweik 9:4 .„ ww4404, hn ligue aismg„, ger, Atlanta Aircraft Certification Office (Tide) Any alteration of this certificate it punishable by e fine of exceeding $1,000, or imprisonment not exceeding &yews, or both. This arttfate me; be hottftered le etweedonee with FAR 21.17. PAAIets 10-2 (Mal) SDNY_GM_02759821 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246743 EFTA01331206

SDNYGNI02759822 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246744 EFTA01331207

' U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATLON REGULATIONS DATE •5 7 24/0/ — AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-100 TYPE (MRPLavE. ROC% If SJCOPIER EICJ Airplane NAME OF APPUCANT TIMCO UST 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 aircrafL STC SA4834NM is the approval basis for this installation. APPLICABLE REQUIREMENTS ommeotre Raw FAR 25.1301 (a), (c) ... • CERTIFICATION - Under appointment under Part 183 have authority vested by direction of the Administrator and in accordance with conditions of the Federal Aviation Regulations, data listed above and on attached sheets numbered been examined in accordance with established procedures and found to Aviation Regulations approval of these data these data and limitations of comply with applicable requirements of the Federal I 1( ) Therefore • Recommend IE Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMBERS) • CLASSIFICATION(S) Robert McClellan ateesie DERT-510239CE System & Equipment _., FAA Form 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION SDNY_Givl_02759823 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246745 EFTA01331208

SDNYGM02759824 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246746 EFTA01331209

LbL9rZOO- V.L.43 Taco EIONEEREO SYSTEMS. be ouweve• Sae *raw A TITLE: HONEYWELL STC / FAA PROJECT NO.: ENGINEER: P. FERGUS TCAS II CHANGE SA4834NM MASTER DATA LIST ` a 7 SOFTWARE UPGRADE MDL NO. 01T012L001 REV/DATE: IR/ 5/21/01 / 650259 AIRCRAFT TYPE: 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 MAY 22 2°1 gloom con-too. 1 ,......,,,,,,,...y...PrZe0.7%0EV= SSyge.A.=:= Oketel•b po l estrtsfedpenr ilfwearanZtrilhrtzrecis luItterie.d Inkn titsgms to Indsm.folt.CO EFIVSH.Sr..... a. OW0, 10 2002 nmeo Ehameews snow.. V. 0IT0IX001$ Sod ft :091MM EFTA01331210

SDNY_GM_02759826 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246748 EFTA01331211

to co rn H H 0 rn 0 O -a -o CO tD u, 9 Y' 1= 1O w NJ O_ 6PL9tZ00-V.L43 TACO ENGMEJMEOSYSIF.A8 tic CONFIGURATION DOCUMENT seam* SuntanMI A TITLE: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 ENGINEER: P. Fergus APPROVAL: Robert McClellan Form t ix: OON DAV: 01, M 01/00 • ' CFG NO. 01T012C002 REV/DATE: IR/ 5/21/01 SHEET I OF 1 I. CONFIGURATION DATA A. APPLICABLE MDL: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE # 01T012L001 B. EFFECTIVITY ISSUED 1. BOEING 727-100 SERIAL NO. 20115 KAY 22 AM C. DESCRIPTION pooMENT C0NIR0L 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 customers 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 011012R007 IR 5/21/01 Description and Substantiation of a TCAS II Change 7 Installation 2 9103 Oar. proptery Cl. inSpic9dObry W. TACO England SWIMS. Me and b rogricled IM VW by desireted pan Ms cc ono-aces C. ton ',anima Mn been (1111Ctid no Use sap lo inlearn TACO Farmed Slain kw- sad so Mb II Pandas againsi My Wn sash. by tenet el Mt p014antort et Ws Otter. In urauChalted use tad Ougalon Is recette. and II Is poleclet yoke an InPUtathed <WOW COWIght(C) 2000 Bum enSeedod syntax Inc N LVIT012 Jet Artiflo101T012CC02tdoc StXlchlr 0911004 03 EFTA01331212

SDNY_GM_02759828 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246750 EFTA01331213

TECO ENGINEERED SYsmes. nc ettearet tan Creener A ENGINEERING ORDER Fenn?. la: EN-0002 Date: (WOWS 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 HAY 222001 P0OMENT CONTROL INITIAL RELEASE REVIEWS P. Fergus PREPARED73Y.rir::152;24€,AsIgg David Thornton • CNECIOD.BNC-0..VCE'-gizi7Ltij;iza.e.'it.i Richard Cunningham 7:okftelireing eciCIA(Sreg- '4&iitarl, Robert McClellan APPIRWITALaigksfrargAigiti TIMCO ENGINEERED SYSTEMS, INC. 623 Radar Road Greensboro, North Carolina 27410 Telephone: 1Ws Oats Ls the wopeny a. and voyntary to. TIM M Engineered %%lent. Inc. and Is mated for metydcgv4E persons. ems ce carp:esters nsth %nem conIncts have been entered It Usti agreed b IndinneY TIMCO Ern:imam Sygenn I t. and to hoSI II harries DOW any claim arising by reason of the ccasecan dela Cured. ca smut/milted Lae ar4 0.clication b rchaittl. and Ills prattled undcr an unpubazb'ecl copra' Ccppicht (C) 2000 TACO Enreesed Systems. Inc CriT012E0)SS Sloe* no 091 ladled SDNYGlvl02759829 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8,9, 10, 15, and 17 EFTA_0024675 I EFTA01331214

SDNYGM02759830 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246752 EFTA01331215

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 Corsion 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 Tranwort Airplane Directorate Date teat. Zeirt, SDNY Glv102759831 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246753 EFTA01331216

SDNYGM02759832 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246754 EFTA01331217

tp usmow:met as Tiensparlasba (Airframe, Federal AvIallon AclergasentIon MAJOR REPAIR AND ALTERATION Poworplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FM Use y:i illy Office Identification 50- f5Do- (7 ,-ti INSTRUCTIONS: Print or type all and disposition of this form. This report 51.000 for each such violation (Section entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for inst ons is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to od 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 • Serial No. 20115 Nationality and Registration Mark U.S.A. N908.TE 2. owner Name (As sham JEOE INC. en registration certificate) Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DP. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in ltem 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 1515 PERIMETER RD. WEST PALM BEACH. LTD. FL 33408 U.S. Certified Mechanic CRS EYKR782D AIRFRAME 1,3. RADIO 1,2,3. LIMITED ME & FNG. Foreign Certified Mechanic jc Certificated Repair Station — Manufacturer D. I certify that the repair and/or alteration have been made in accordance with furnished herein is true and correct made to the unit( ) Identified in item 4 above and described on the reverse or attachments hereto the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information to the best of my knowledge. Date 7/2/01 Signature of Authorized in "dual John K. UrsaInspector. la f(.- U --e- 7. Approval for Return to Servl Pursuant Administrator BY to the authority given persons of the Federal Aviation specified below, the unit dentified in item 4 w inspected "n tho manner prescribed by the Administration and is El APPROVED 0 REJECTED FM RI Standards Inspector Manufacturer Inspection Authorization Other (Specify) FM Designee X Repair Station person Approved by Transport Canada Ainvorthiness Group Date of Approval or Rejection 7/2101 Certificate Designation or No. EYICR782D Signature of Authorized Individual Ronald K. Bystrom. Managa Quality FAA Form 337 (Im) SDNY_GM_02 759833 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246755 EFTA01331218

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate akciaft record. An aftamtion must be compatible with WIprevious alterations to assure continued conformity with the appacable 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, N9081E. W/O 16236. INSTALLED A UNIVERSAL AVIONICS 7T-3000 SERIES AREO-M SATCOM SYSTEM PER UNIVERSAL AVIONICS AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM INSTALLATION MANUAL NO. 23-15-02 DATED 317/01. SYSTEM CONSISTS OF 2 EA HANDSETS, 1 EA ANTENNA, I 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 I THRU 3, TITLED -TT-3000 AERO-M AIRBORNE SATEUITE 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 I THRU 5, TITLED- AERO-M SATCOM ANTENNA INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/18101, BY STRUCTURAL D.E.A. NO. DERT-510024-CE. • B727-16236-1342, REV. IR, DATED 5/21/01, SHEETS I 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 7T-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 HOLES IN SATCOM ANTENNA PIN 10101-00, DATED 7/25/00, WAS INCORPORATED AT ANTENNA INSTALLATION. THIS HAS NO EFFECT 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 INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC WADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER I, 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 06/11/2001 WAS COMPLETED IN ACCORDANCE WITTI 43.13-1B, CHAPTER II, SECTION 3, PARAGRAPH II-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC 43.13-IB, CHAPTER 4, SECTIONS I, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED THE INSTALLATION CONFORM TO AC 43.13-111, 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 TFIE REQUIREMENTS OF AC 43.13-1B, CHAPTER I I, SECTION 4. ELECTRICAUELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC 43.13-1B, CHAPTER I1. SECTIONS 5-11, 13. IS, 17- 19 AND AC 43.13-2A CHAPTER 2. PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC 43.13-IB, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH SECTION 16. ELECTRONIC 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 TAW AC 43.13-1B, CHAPTER 10. SECTION 2 AND AC 43.I3.2A. CHAPTER 1 PARAGRAPH 9. PER THE AERO-M SATCOM INSTALLATION MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT AFFECT 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. DEBT-510333-CE. THERE ARE NO COCKPIT PROCEDURAL CHANGES OR FLIGHT MANUAL SUPPLEMENTS REQUIRED FOR THIS INSTALLATION. END K Additional Sheets Are Attached * U.S. O.P.0 1990-781.763 SDNY_GM_02759834 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246756 EFTA01331219

May-29-01 01:5BP N J Curran 352 243 1011 P _ 02 DUARTMENT Of 111AMPORTAI ION Maltµ AVIATION AtIMIMSTRATION STATEMENT OFCOMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Aitplanc. Radio. Helicopta. ttC) Airplane NAME Of APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA ' IDENTIFICATION TM,E B727-16236-340. Initial Release, [fated 04130101 TT-3000 SERIES AERO-M AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM PURPOSE OF DATA In support of major aeration to Boeing 727-31. serial number 20115. registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 26.581 (ahhH1) FAR 25.1351 (a) (a)(4) FAR 25.889 FAR 25.1357 (a)(c) FAR 26.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 26.1316 (b) CERTIFICATION - Vat. start, we by 'Innis. NN. Aro len. on re ...nee.. dab eladrsamased Sena.. e s.,...e ...dr tunst...."..i............,...d....s . Nciat_ i an beet nroero. ...urea nb nlaibillierlitedn Md 4 .'4 n ...Pi> .'"Wfr Itivelmies. 0 Recommtod approval of i hose data I (We)Tkrefore El Appian tam data (Swoon At Equipment Astarrets. Dellipi Approval Ooty. Don Not C.:marital dar in of .1. nonstAnm••• linema. at r‘i Ur...a N. rani ...`.. Instanal 'co Approval) Slam F MOOG liZPRIMITATTIfircy DOIGMATOMNIAMiuS) cusSIIICArketin Leze.0 __ DERT-510087-NM Systems & Equipment No an urran — - ---- - II40)SUPERSEDE3 PREVIOUS ECCION CP0901-613 PTIXNANCE SC.727-SATC0MDDC SDNY_GM_02 759835 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246757 EFTA01331220

SDNY_GM_02759836 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246758 EFTA01331221

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June IS. 1001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL B727-3I TYPE fahlov.Ra. ffrgetfle. ac) Airplane NAME OF APPLICANT Jet Aviation LIST OF DATA WEN I INCA I ION Illibt Jet Aviation Engineering Drawing No. B727-16236-1340, Dtd. 5/29/2001, Rev. A _END_END_ END Note: The certification evaluation of structure. Structural Repairs on Notes: Aero-M Sateen Antenna Installation Boeing 727-31 / S/N: 20115/N908,1E END END END END END END END basis of this aircraft Includes FAR 25.571 Damage-tolerance and fatigue Per Advisory Circular 25.1529-I 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 cf the above listed date are approved Ls 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 ll The structural herein. 2) This approval listed below 3) This approval corporate Model PURPOSE Approve data for antenna Installation (Structures Only) OF DATA APPLICABLE REQUTRMENTS (Lt.ST SPEC! PIC S ECTIONS7 25.301, 2.5303, 15.30S, 25307, 25.601, 25.603, 2.5.605, 25409, 15.613 CERTIFICATION- Ueda authority voted by direction of die Administrator and In accordance with condition appointment wader Pan In of the Federal Arline,. Regulations, data hued shoe and ea attached sham numbered been trammed In accordance veldt ateibbed procedure and found to comply with applicable mermen of Aviation RtsviadOOS. I 0 I Therefore Recommend 'enema of these data pi Approve that data and 1St of have the Fe SIGNATURE(S) OP DESIGNATED ENGINEERING REPRESENT') E(S)DESIGNATION NI/MIENS) INASSIFICATION(S) Robert J. Begat! DERT-S10024-CE Structures FAA FORM 81103 (11.10) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001.0S2 SDNYGlvl02759837 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246759 EFTA01331222

SDNYGM02759838 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246760 EFTA01331223

L. r CCPARTMENT OF TRANSPORTATION FE OERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DAIS May 28, 2001 AIRCRAFT OR AIRCRAFT COMPCNENT CODIFICATION MALE Boeing MODEL NO. 727-31 TYPE(Mitne. Radio. hlebtoplet. etc) Airplane NAME Of APPUCANT 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 FM authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE RECUREMERIZ CUR spacemen:WV FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.5810)XO 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the AdminastRitOr and in accordance with conditions under Faun of the Federal Aviation RegLiatiors, data haled above and on attached sheets numbered in accordance with established procedure and found to corny with applicable requIremenO of the Federal Recommend append of Rase den. I (t$ Time:eta Approve these nets. • and EmItaLions of appointment 0 have been alias/nod Aviation Reputations. IS) CF DESIGNATED ENGOE (S) Si NATION NUmbut(s) I CLASSMI LOtt(S) David E. Haralson Po-re. 1-4,4-__ DERT-810028-NE Structural h RSECI ER01205.6de SDNY_GIvl_02759839 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024676 I EFTA01331224

SDNYGM02759840 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246762 EFTA01331225

DIPAATISITCOTWISPORTATION . FEDERAL AVIATION ADMNGSTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARL BOEING MODEL NO. 727-31 Manum. limmum egia AIRPLANE 4A/AE OF APPLICANT ME JET AVIATION LIST OF DATA umwrdimAnOw wns A.T.E. INC. STRUCTURAL REPORT No. ATE6I12001 BOEING 727-31 S/N 20115, AERO-M SATCOM ANTENNA INSTL, UPPER B.S. 360-300; OPS ANTENNA INSTL, UPPER B.S. 312-328; AIRCELL AOT.01 ANTENNA INSTL, LOWER BS. 400-420 DAMAGE TOLERANCE ANALYSIS; SH. 1-31, REV. (ER) NOTE- REOUIREUNSPECTIONS ATTACHED THESE DATA APPLY ONLY TO BOEING 727-31 S/t4 20115 PURPOSE OF DATA TO APPROVE • DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-31 S/1420115 APPLICABIS REQUIREMENTS (lAttswAd sada.) FAR 25-571 (STRUCTURAL ASPECTS ONLY) CERTIFICATION- Under authority wasted by &, on of the Administrator and in accordance will conditions and Senitatiera • of appointment under hri IS) oft Fehr& Aviation Itesolmions. dais :IFS *ova and on asembed dims numbered I of I have boa °unlined In accordaus with ettibfabed procedures and found to comply add' applicabk nmultesnenta of ow Federal AVOWS Regulagices. i, Rceommcad appronl of data I (0)Tbatfo Approve se . SIGNATURE(S) OF DESIGNA ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATION(S) 9 wAle.mt DERT-510333-CE STRUCTURAL FAA Form *110-3 OVA) se/rumen memos eomeei CeOf01413 SDNY_Glvl_02759841 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246763 EFTA01331226

SDNYGM02759842 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246764 EFTA01331227

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SDNY_GM_02759844 CT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, a EFTA_00246766 EFTA01331229

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SDNY 02/b9866 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 0024676% EFTA01331231