EFTA01331032.pdf

OMB tee memo ElecircricTrecknehatet EV: W31/20.4 fll 0 BY MAJOR REPAIR AND ALTERATION or FAA Usi Only us Osean- ent or Tremont/fen (Airframe, Powerplant, Propeller, or Appliance) Newel Mitten AdenInlotretien INSTRUCTIONS: Print or type ail entries. See Title 14 CFR §43.9, Part 43 Appendix B, and AC 419.1 (or subsequent revision thereof) for instructions and disposition c4 this form. This won Is rethireid by Law (49 U.S.C. §44701). Failure to repot can ankh in a civil penalty for each such violation. (49 U.S.C. §48301(a)) Nationality and Registration Mark Senaf No. N908JE 20115 1. Aircraft Make ode eves BOEING 727-31 Name (As shown on registration certificate) Address (As shown on registration certificate) Arklent )02 FOULS HO ST E 202 2. Owrer JEGE INC Cry VetAfiNGTON Stew OE ip 11003.3742 Ceu try SA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. lil AIRFRAME (As described in Item I above) O O POWERPLANT 0 O O PROPELLER Two O APPLIANCE Manufacturer S ConfomiltyStetement A. Agencys Name and Address B. Kind Of Agency tams Bergen Ak ServkeASok•OMplen U. S. densidned wawa I Manufacturer Ads.“ SS OrI ma vein Foreman Commend mechanic C. Certificate No. Cry ft isethedels ore' FL x Cortietled Seater Stow SD4R514M Po 'POO Corr/ USA CSISCeleeMeireenteCeorperrat0IN D. I certify that the repair ancVor alteration made to the unit(s) identified in Om 5 above and described on the reverse or attachments hereto have been made In accordance vMh the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information famished herein is true and correct to the best 01 my knowledge. blended range fuel SDate of Authorized Incividual ow 14 CFR Part 43 O . APP. 0 4 :// David K. Crosby 15 JAN 2016 /.....• ../ ov I for m to Service Pursuant to the authority g yen persons specified below, the u ' retied in rem 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration end is XIApproved I—Rejected FAA Fri Standards Pawns Approved by Canadian Manufacturer Maintenance Organization Depannuthr or Transport Inspector BY 0010r (Speedy) FM Designee X Repair Station Inspection Authorization Minato or 7 4-iitu ate of Authorized Individual Designation No. SD4R514M i / 92 a 1. David K. Crosby 15 JAN 2016 FAA Form 337 (10/06) SDNY_GM_02759647 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246569 EFTA01331032  NOTICE Weight and balance or operating hmitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible AIM all previous alterations to assure continued conformity with the applicable airworthiness requirements. II Description of Work Accomplished fa more space is muffed. attach &rational sheets. Identity with aircraft nationaAty 811:1reptstration mark end date work competed) N908JE 15 JAN 2016 The following work was accomplished on Work Order 82484. Nationality and Registalion Mark Date INSTALLED: Aviation Communication & Surveillance Systems (ACSS) STC Number ST02406LA, entitled 'Installation of TCAS version 7.1 In accordance with FAA approved AML No. ST02406LA. dated February 06, 2012, or later FAA approved revision.' The following Aviation Communication & Surveillance Systems (ACSS) Traffic Collision Avoidance System (TCAS II) equipment andlor components were removed for modification: 1. RT-910 TCAS II Computer Unit (Change 7.0) PIN 4066010-913 The following Aviation Communication & Surveillance Systems (ACSS) Traffic Collision Avoidance System (TCAS II) equipment and/or components were installed after factory modification: 1. RT-910 TCAS II Computer Unit (Change 7.1) P/N 4066010.914 The above modified equipment and/or components was installed in accordance with ACSS TCAS II/2000 Change 7.1 AML STC Master Data List, Document No. 8900067-002 Revision E dated August 07, 2013 (FAA accepted on September 9, 2013 Los Angeles ACO) or later FAA approved revision, as listed on the FAA Approved Model List (AML), Document No. ST02406LA, dated September 25. 2013 or later approved revisions, and the ACSS Traffic Alert and Collision Avoidance System, System Description and Installation Manual, Pub. No. C15-3841.005, (ATA No. 34-43-00). Revision 004 dated 15 Oct 2013, Including Temporary Revision No. 8 dated 15 Jun 2011 or later appropriate revisions. The required FAA approved Airplane Flight Manual Supplement (AFMS), Spec. No.: 8008565-001. Rev. IR dated August 9, 2012 or later FAA approved revision has been inserted into the Airplane Flight Manual. The aircraft Weight & Balance change negligible and Equipment List amended. The electrical load was computed and found not to exceed 80% of the system output. Log book entry made. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (ICA) 14 CFR 425.1529 The Instructions for Continued Airworthiness are contained within the ACSS TCAS II/2000 Change 7.1 AML STC Instructions for Continued Airworthiness, Document Number 8008572-001 Revision B dated 18 April 2013 or later FAA accepted revision. END A00it cred Sheets Ate Atteehial FAA Form 337(10/06) SDNY_GM_02759848 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246570 EFTA01331033  -r BANYAN Federal Aviation Administration Date: January 15, 2016 Aircraft Registration Branch AFS-750 PO Box 25504 Oklahoma City, OK 73125 Ann: Record Keeping Subject: ,ubmIttal of FAA Form 337 for N311AG Boelna 727-31. SM 20115 for the installation of the AC S TCAS II Chance 7.1 IAW ACSS STC ST02460LA Enclosures: 1. Original FAA Form 337 for the Installation of ACSS STC No. ST02406LA. dated 15 JAN 2016. The above listed enclosures are being submitted as per 14 CFR 43, Appendix B paragraph (a)(3). Please contact myself with any questions or concerns. Banyan Air Service Fort Lauderdale Executive Airport • 5360 NW 20" Terrace • Ft. Lauderdale FL 33309 www.banyanair.com SDNY_GM_02759649 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024657I EFTA01331034  . . . • SDNY_GM_02759650 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246572 EFTA01331035  1.1 21M 0,20 Douro* Troclong tivatw OMO En: &'3t11014 l 0 MAJOR REPAIR AND ALTERATION 0 saw OW LIS Dopeerent . al!romantic., (Airframe, Poworplant, Propeller, or Appliance) Foilsniknoesa AAISSetteeen INSTRUCTIONS: Pita or type at entries. See Title 14 CFR §43.9. Pad 43 Appen B. and AC 43.9-1 (or subsequent revision thereof) for insvuctions and disposition of this form. This report is required by law (49 U.S.C. $44701). Rause to report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) Nationality and Registration Mark Serial No. N908JE 20115 1. Aircraft Make Model Series BOEING 727-31 Name (As shown on registration coreficete) Address (As shown on registration certificate) maw iC0 Mout ROAD SUITE 202 2. Owner JEGE INC CO, WILIMeTION 5.01• CE Zro 1010S.3712 Cava, U.ASTED STATES .. .. _ 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteraton Lint Make Model Senal No. El 0 AIRFRAME (As described in gem 1 above) In POWERPLANT El El O PROPELLER Twee O D APPLIANCE renureckcer 6. Conformity Statement AL Agency's Name and Address B. Kind ol Agency Nam BOCA AJRCRAFT PANNTENANCE LLC x U S. carlificaled Mechem I Mandecluter km.. sesAmicaT Yew.* I Foreign Cenfteled PiethenC C. Certificate No. Cer BOCA PATON Wee Ft Cenficated Rope., Saloon, re 31131 cc..„, wart° SMITS CertiScated Maintenance Orearrieben A&P 2884154 D. I certify triat the repair and/or alteration made to the unite idenblied in item 5 above and descnbeS on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my ItnoMedge. Extended range fuel SignalureiDate honied Ike ma per 14 CFR Part 43 O APP. 8 r / "/d) 7. Approval for Return to Service Pursuant to the wAhonly even persons specirted below, the unit identified In nem 5 was Inspected in the manner prescnbed by' the **nenestratorol the Federal Aviator, Administration arid Is nApproved illiejected FAA Fk. Standards Per Aneovel by Caneden Manufacturer Meinlonance Organization Deparenerd el Transport Inspector BY Other (Sneer)) FAA Designee Repair Station X Inspecaon Authorization Celli cote Or win Aix.d incWidual Designation No. A&P/IA 3434119 1/9/20/5- FAA Form 337 (10/06) Page I SDNY_Givl_02759651 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246573 EFTA01331036  NOTICE Weight and balance or operating limitation changes shell be entered in the appropriate sirens!? record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Week Accomplished of more space is required. attach additional shoots (dent h secret nationaiW and registration math and date ewe completed.) • Milt2015 Nationality and Regolnition &lark Date REMOVED AVIATION COMMUNICATION AND SURVEILLANCE SYSTEMS (ACSS) TCAS SYSTEM PROCESSOR P/N 4066010-910 (S/N 91050384) AND ROUTED TO MANUFACTURER FOR INCORPORATION OF SERVICE BULLETIN 8008230-001, REVISION 02 (ATA SB 4066010-34-6036). REINSTALLED REPAIREDI MODIFIED TCAS PROCESSOR P/N 4066010.913 (SIN 91050384) AFTER INCORPORATION OF ACSS ATA SB 4066010-34-6036. PERFORMED OPERATIONAL TESTS WTTH NO NOTED DISCREPANCIES PER ACSS TCAS II SYSTEM DESCRIPTION AND INSTALLATION MANUAL (SDIM), ACSS PUB 0 CIS-3841-005 (ATA NO. 34-43-00). NO CREW OPERATIONAL PROCEDURES HAVE BEEN AFFECTED BY THIS SOFTWARE UPGRADE. MODIFICATION IS WITH REGARD TO PROCESSOR SOFTWARE ONLY AND THEREFORE: WEIGHT AND BALANCE IS NOT AFFECTED. ELECTRICAL LOAD IS NOT AFFECTED. CONTINUED AIWORTHINESS REQUIREMENTS ARE NOT AFFECTED. ALL WORK WAS PERFORMED AS PER FAA AD 2012.02-08. CAddltaUtiSh4)013 Are Attached FAA Form 337 (10/06) Page 2 SDNY_GM_02759652 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246574 EFTA01331037  Mobile Repair Team Boca0Aircraft • NAAINTENJANJCE CRS# 380R5358 3300 Airport Road Hangar 2 Suite 121 Boca Raton. Florida. 33431 MOO . baKia43 ft /WWI** lirral tiber a - 3?CA &SC\ O ?Tc±--- 20i:C— werehistio o asks to oe PFIiirlifeil (--,D (ICs Ik-tcw I C- 7 C ,t,Cci\Air NE \ ete,, Pe7Strirre Ars`rito ( VeTirilerff&) pi ee \I\ CA- N3 -N.... Cc, • erso sj A therized t rf c2 erO Tr, to S7 e Ira ^spectionsand Appr ved or Reit f • 10 Service e 6rnp oyee ©26117@italitcDr OCTIMillein J. C,S2 0rilik A •ri vi.‘ 0,,,.4 24 ,v•,T., -z y S Le r) 5- V Authorization efrUtist Kousmg Adequate a imps and Equipment a Parts and Materials Available Technical Data Available Et' RSIA/OO.1 Copy AviaLabla Et- Destination: F.J6 Notes: • Manager's / Lead's Signature Authorizing MRT Date. Form MRT 4/1/2011 SDNY_GM_02759653 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246575 EFTA01331038  • • • SDNYGM02759654 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246576 EFTA01331039  romtApporWl Enoric Treckna finest OIM we z‘200:00 0 tirJOrSOF VS Deow's.sei MAJOR REPAIR AND ALTERATION **flare 0* of Ttetspalien (Airframe, Powerplant, Propeller, or Appliance) codonlAvisdea AdeSiatrulen INSTRUCTIONS: Print or type as entries. See Title 14 CFR §43.9, Put 43 Amer* B. and AC 43.9.1 (or subsequent revision Owed) for inanabons and disposition of thi$ form This report is required by law (49 U.S.C. §44701). FaNure lo report can result in a civil penalty for each SuCh ViOlitiO . (49 U. S.C. 546301(e)) Nationality and Registration Mark Serial NO. N908JE 20115 1. Aircraft make Model Setts BOEING 727 31 Name (As ShOWII on togivronon °Miyake) AddreSS (As Shown on legtsinstiai cortMOAAM JEGE INC. wow. 103 FOULK ROAD SUITE 202 2. Owner stew 0 tar WILMINGTON to 19803-3742 Coat/ UNITEDSTATES 3. For FAA Use Only 4. Type S. Unit Identification Renew ARMWon Unil Make Model Serial No. O AIRFRAME (As dexROue on Item I above) Z El POWERPLANT O O O PROPELLER rya O APPLIANCE O Minufacturte 6. Conformity Statement A. Agency's Name and Address B. Kra al Agency woe FLIGHTSTAR AIRCRAFT SERVICES. 110. 06. coneested Necinent I Manutacturer Mises 8021FLIGHTLINE RD BLDG. 615 Fotiolati Girtkaki MOChark C. Certircate No. on JACKSONALE s FL i CertliCato0 nervier SIMON zy 32221 cater UNITED STATES FOTR986N CentkomaiminsenmotOrosnaMon 0. I certify trial the repair andfor alteration made to the WAS) klenflflOO in item 5 above and deserted an the reverse or altativntelit here*, have been made in accordance with the requirements of Part 43 al the U.S. Federal Alston Regulations and that the inforrnetlen fuenished herein is 'rut and cared to the best of my knowledge. Extended range fvel Sigr)ie Of Aulh5rnatO Individual per 14 CFR Part 43 App. B O ,e.,t..., Act/.. - / PETER JACKSON 91482 MARCH 01, 2012 T. Approval for Return to Service Pursuant to Ow authority given persons specified beiow, the unit identified in item 5 was inspected in the manner pronatted by tie A0MiriSedlOf of Me Federal AvIEIPOO Administration and is gl Approved O Rejected FAA FR. 9landards Pence. APProved try Caliklen Manufacturer Maintenance Organization Mamba DepOrlfrent of Minivan BY Other (Speofy) FM Designee x Repair Station Inspection Authorization Onto:ale or Si u ,tiol dAu honied Individual Oesignation No. PETER JACKSON 91482 MARCH 01. 2012 FOTR986N osa.4920 " FAA Fun 337 uses) SDNY_GM_02759855 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246577 EFTA01331040  NOTICE Weight and balance or operating limitabon changes shah be entered in the appropriate aircraft record. An alteration must be compatible with at previous alterations to assure continued confomety with the applicable airworthiness requirements. S. Description of Work Accomplished (amore space is required. attach oddoonal sheets. Identify with aircraft national:I], and registration mark and date work comPieredl N908JE MARCH 01, 2012 Stationary and Registration Mark Date W/O 21219 1. WR 25306: REPLACED RIGHT WING FRONT SPAR VERTICAL STIFFENER AT APPROX. W.S. 200 WITH PIN 65-16200-3M IAW BOEING 727 SRM 51-30-2 REV. 103. 2. N/R 25522: REPAIRED RIGHT HORIZONTAL STABILIZER REAR SPAR LOWER CHORD BETWEEN STAB. STA 56 TO 113, IAW COTNEY AEROSPACE DRAWING AL81.55.101 REV. IR. FAA FORM 8110-3 DATED FEBRUARY 03, 2012 ISSUED. MATERIAL USED: ANGLE; PM54-2304 7075-T6511, DIM. 4" X 55.75% ANGLE; AND10137-3001 7075-76511, DIM. 16.375" X 3.75', RADIUS BLOCK; 7075-T6, 0.125', DIM. 12.5' X 2'. 3. N/R 25523: REPLACED RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER ON AFT SPAR AT ELEV. STA 53.91 IAW BOEING DRAWING 65-16876. MATERIAL USED: EXTRUSION; BAC 1505-29222 707576511. 12.5' LONG. END ❑ &Mb,* Meets Na Awned FAA Form 737 noes) SDNY_GM_02759656 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (X1246578 EFTA01331041  Farm Approwel 11 wt Paden; Mats OW No 21204020 0 US Ogionmel MAJOR REPAIR AND ALTERATION 1.2•20is oda. Us O.* at Three:ono, (Airframe, Powerplant, Propeller, or Appliance) net.ii Media Aciaanithatiee INSTRUCTIONS: Print or type all entries. See Trde 14 CFR 643.9, Part 43 Appendix 13, and AC 43 9-1 (or subsequent revision thereof) for instructions and disposition of this but This report is required by law (49 U.S.C. §44701). Faire to report can result in a ovil penalty for each such violation. (49 U.S.C. 448301(1)) Natiortady and Registration Man( Serial No. USA N9C8JE 20115 1. Aircraft loam model Series Boeing 727 31 Name (As shown on regisuahon contain) Address (As sham on nesistration conical.) Amens 101FOUI K an STF 2112 2. Owner cry VVILhliNGTON sue DE_ JEGE INC 7. 19803-3742 coney ‘USA 3. Fa FAA Use Onty 4. Type S. Unit Identification Repair wierason Unit Make Model Sate No. (As clescdbedM Rem/wow) • if AIRFRAME O • POWERPLANT • • PROPELLER tyre O APPUANCE O lasnutaClurer it Conformity Statement A. Agency; Name aid Address El. Kind of Agency rem TIMM) u. S. Conf.:ow MeChenic I Manubicluart New 102 SE Academic Ave. Foreign Ceircaled meowno C. Certificate No. oil I eke City see Florida . / Cortriesise Reps, Station rr 32025 Owe, USA coneeter Mainianarek0Mtnawn DU4R141M Class IV D. Icor* Smith. repair anclior alteration made to the snit( ) identified in item S above and denoted 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 idonnation finished herein is true and correct to the best of my tnoweitge. Extended range fat Signs ate of A m671 par 14 CFR Pan 43 • APP. 8 A Gregory A. Christman - 28 FEB 09 7. Approval for Return to Service Pursuant to the authorey given persons below, the uNt Identified n dem 5 was inspected in the manner prescand by the Administrator of the Federal Adak., Administration and is 2 Approved O Rejected FM Fe Standards Manufacturer Maintenance Organization eenons Append by Deneefien Inspector Cepailement of Teensy:A BY Omer (SPIT*/ FM Designee I Repair Inspection ArAlloriZatiOn CerlifiCale Of Sign I Designation No DU4R141M Class n/ Anthony V. Baroni - 28 FEB 09 FAA Form 337 nom> SDNY_GM_02759857 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246579 EFTA01331042  NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft retold. An alteration must be compatible with all previous excretions to assure continued conformity with the applicable airworthiness requirements. 8. Descdpdon of Work ACC0Mplish0d (If mote space is required, reface addtional sheets Wen* with atone nationatty and registration mak and date work completed) USA N908JE February 28, 2009 Nationally and Registration Mark Dale The following major modification was accomplished: 1. N/R #31809 Accomplished Deactivation of Rogerson Auxiliary Fuel System installed under STC #SA2734VVE in accordance with Quiet Wing Technologies Inc. Modification instructions No. M727-3-2008 Revision NC dated 19 NOV 08. approved per FAA Form 8110-3 by DER Mark Ostendorf #DERT-605421-NM dated 12/23/08. Minor deviations accomplished per Modification Instructions JEGE 8727-100 dated.2-26-09. SUMMARY 1. All work accomplished IAW STC fiSA2734WE and Quiet Wing Technologies Mod M727-3-2008. 2. Records of all work accomplished is on file at this repair station under Service Order #185008. 3. All Repairs are permanent unless otherwise stated. end Additional Sheets Ate Attached FAA Form 337000N SDNY_GM_02759858 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246580 EFTA01331043  Foe. Aocromi4 Becoa,t Lapp Mover ow en. zizo-coth ffri orthezoc MAJOR REPAIR AND ALTERATION ret MAUviiithe LiS owwwww of TSAI:WIN/0+ (Airframe, Powerplant, Propeller, or Appliance) Iodeni ANsfion Adminiontion INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9, Part 43 Appendix a and AC 43.9-1 the subsequent revision memo° for instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure to report can result In a civil penally for sad. such violation. (49 U.S.C. §46301(e)) Nationality and Registration Mark Serial No N908JE 20115 1. Aircraft Maly Model Series Boeing 727 -31 Name (As shown on tegistathon condicate) Address (As shown on togishation certificate) JEGE Inc mufti. 103 Foul( Rd Sle 202 2. Owner Gib WiminatOn sew DE at 19003,3742 coon USA 3. For FAA Us. Only 4. Type 5. Unit Identification Repair Alteration Unit make Model Sonar No. (As desated in Item 1 80010) 0 (Z AIRFRAME o O POWERPLANT E 0 PROPELLER APPLIANCE 0 0 Manulack4s, 9. Conformity Statement A. AgencYs MIMS and Address B Kind of Agency rithe FLIGHTSTAR AIRCRAFT SERVICES. INC. u. S. Certhcated Mechanic I manuthcesw sass BLDG. 815,6025 FLIGHTLINE RD. 44441;n Certificsiod medwic C. Certificate No. ok, JACKSONVILLE es., Fl., / Catecated Raper Sheen be 32221 c....„, USA FOTR986N Ceonciders meinuensnce Organization D. I certify that the repair oridlor alteration made to the unli(+) identified in Mon 5 above end described on the reverse or attachments hereto have been made in accordance well the requirements of Pari 43 of the U.S. Federal Aviation Regulations and that the information i Mnlshed heroin is Duo and correct to the best or my knowledge. Extended range fuel Signature/Dale of Author! ad Individual per 14 CFR Part 43 0 CHRIS ADAMS 30 JULY 2008 APP. B It 7. Approval for Return to Service Pursuant to the authority given persons specified below, the MN Identified in item 5 was nspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is IZ Approved Rejected L FAA FN. Standards Persona approved bye:moan Manufacturer Maintenance Organization Desarvneri or Transport InspectOr BY Other (Spotty) FM Designee x Repair Station Inspection Authorization Corti math or Signature/Ciato of Authorized Individual Designation No. CHRIS ADAMS 30 JULY 2008 FOTR986N l id Cej , FAA Form 337 tooth SDNY_GM_02759659 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024658 I EFTA01331044  NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft reCOnl. An alteration must be Compatible with all proWous alterations to assure contoured conformity with the applicable eiwnxthiness requirements. S. Oaticrlption of Work Accomplished (Ilmore space Is required, stla0 additional shoats. Identify mei aircraft nahenegity and repotratlon mark and dote work comaltfed) N908JE Nationality ON Registration Mn L 0 JULY 2008 Oats WIO 8181 1. COMPLIED WITH DFDR 11 CHANNEL UPGRADE IAW MODIFICATION ORDER EMTEO 2.80158.801 REV. B. DATED 07-30-2008 . FAA FORM 8110-3 DATED 07.30.2008 ISSUED. ENO ❑ Additional Shoots Ara Attached FAA Form 337 threat SDNY_GM102799660 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246582 EFTA01331045  0 MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-0020 U.S. Departmtel of (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Transportation Federal Aviation Office Identification Admabin tin INSTRUCTIONS: Print or all aeries. See FAR 43.9, FAR 43 Appendix B and AC 43.9.1 @shy:gas revision Chaco( for instructions and disposition of this form. This report is roquira q law (49 U.S.C. 1421). Ware to report can result ma cull penalty not to exceed $1,000 for cad. such vxdatan (Section 901 Federal Aviation Act of 1916). Make MODEL BOEING 727-31 Serial No. Nationality and Registraioo Mark 20115 USA N908JE I. Aircraft Name (As shoal on regisnatiOn eatificalc) Address (as shown on registration certificate) WOE INC 103 FOULK RD STE 202 2. Owner WILMINGTON, DELAWARE 19803.3742 3. For FAA Use