EFTA Document EFTA01331032

0 BY MAJOR REPAIR AND ALTERATION us Osean- ent or Tremont /fen (Airframe, Powerplant, Propeller, or Appliance) Newel Mitten AdenInlotretien OMB tee memo EV: W31/20.4 ElecircricTrecknehatet fll or FAA Usi Only 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)) 1. Aircraft Nationality and Registration Mark N908JE Senaf No. 20115 Make BOEING ode 727-31 eves 2. Owrer Name (As shown on registration certificate) JEGE INC Address (As shown on registration certificate) Arklent )02 FOULS HO ST E 202 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. O lil AIRFRAME (As described in Item I above) 0 O POWERPLANT O O PROPELLER O APPLIANCE Two 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 Or I 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 ow 14 CFR Part 43 O APP. 0 S Date of Authorized Incividual . /.....• ../ 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 BY FAA Fri Standards Inspector Manufacturer Maintenance Organization Pawns Approved by Canadian Depannuthr or Transport FM Designee X Repair Station Inspection Authorization 0010r (Speedy) Minato or Designation No. SD4R514M 7 4-iitu ate of Authorized Individual 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) The following work was accomplished on Work Order 82484. N908JE 15 JAN 2016 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 Aircraft Registration Branch AFS-750 PO Box 25504 Oklahoma City, OK 73125 Ann: Record Keeping Date: January 15, 2016 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 0 MAJOR REPAIR AND ALTERATION LIS Dopeerent . al !romantic., (Airframe, Poworplant, Propeller, or Appliance) Foilsniknoesa AAISSetteeen O M O 1.1 2 1 M 0,20 Douro* Troclong tivatw En: &'3t11014 l 0 saw OW 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)) 1. Aircraft Nationality and Registration Mark N908JE Serial No. 20115 Make BOEING Model 727-31 Series 2. Owner Name (As shown on registration coreficete) JEGE INC Address (As shown on registration certificate) maw iC0 Mout ROAD SUITE 202 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) El In POWERPLANT El O PROPELLER O D APPLIANCE Twee 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, A&P 2884154 re 31131 cc..„, wart° SMITS CertiScated Maintenance Orearrieben 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 per 14 CFR Part 43 O APP. 8 SignalureiDate honied Ike ma 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 BY FAA Fk. Standards Inspector Manufacturer Meinlonance Organization Per Aneovel by Caneden Deparenerd el Transport FAA Designee Repair Station X Inspecaon Authorization Other (Sneer)) Celli cote Or o. A&P/IA Designation N 3434119 win Aix.d incWidual 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 REPAIRED I 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 AI WORTHINESS 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_02 759652 • 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 . lirral tiber baKia43 ft /WWI** a - 3?CA &SC\ O ?Tc±--- 20i:C— werehistio o asks to oe PFIiirlifeil (--,D (ICs Ik-tcw I C- 7 C Cci\Air NE \ ete,,,t, Pe7Strirre Ars`rito ( VeTirilerff&) pi ee \I\ CA- N3 -N.... Cc, erO Tr, to S7 e erso sj A therized t rf c2 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., r) -z y S Le 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 0 MAJOR REPAIR AND ALTERATION VS Deow's.sei of Ttetspalien (Airframe, Powerplant, Propeller, or Appliance) codonlAvisdea AdeSiatrulen romtApporWl OIM we z‘200:00 tirJOrSOF Enoric Treckna finest **flare 0* 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)) 1. Aircraft Nationality and Registration Mark N908JE Serial NO. 20115 make BOEING Model 727 Setts 31 2. Owner Name (As ShOWII on togivronon °Miyake) JEGE INC. AddreSS (As Shown on legtsinstiai cortMOAAM wow. 103 FOULK ROAD SUITE 202 tar WILMINGTON stew 0 to 19803-3742 Coat/ UNITEDSTATES 3. For FAA Use Only 4. Type S. Unit Identification Renew ARM Won Unil Make Model Serial No. Z O AIRFRAME (As dexROue on Item I above) O El POWERPLANT O O PROPELLER O O APPLIANCE rya 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 Girt kaki MOChark C. Certircate No. on JACKSONALE s FL i CertliCato0 nervier SIMON FOTR986N zy 32221 cater UNITED STATES CentkomaiminsenmotOrosnaMon 0. I certify trial the repair andfor alteration made to the WAS) have been made in accordance with the requirements of fuenished herein is 'rut and cared to the best of my knowledge. klenflflOO in item 5 above and deserted an the reverse or altativntelit here*, Part 43 al the U.S. Federal Alston Regulations and that the inforrnetlen Extended range fvel per 14 CFR Part 43 O App. B Sigr)ie Of Aulh5rnatO Individual t..., Act/. . - / PETER JACKSON 91482 MARCH 01, 2012 , e. , 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 BY FAA FR. 9landards Mamba Manufacturer Maintenance Organization Pence. APProved try Caliklen DepOrlfrent of Minivan FM Designee x Repair Station Inspection Authorization Other (Speofy) Onto:ale or Oesignation No. FOTR986N Si u ,tiol dAu honied Individual osa.4920 " PETER JACKSON 91482 MARCH 01. 2012 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 Stationary and Registration Mark W/O 21219 MARCH 01, 2012 Date 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 K &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 0 MAJOR REPAIR AND ALTERATION US Ogionmel Farm Approwel OW No 21204020 1.2•20is 11 wt Paden; Mats 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)) 1. Aircraft Natiortady and Registration Man( USA N9C8JE Serial No. 20115 loam Boeing model 727 Series 31 2. Owner Name (As shown on regisuahon contain) JEGE INC Address (As sham on nesistration conical.) Amens 101 FOUI K an STF 2112 cry VVILhliNGTON sue DE_ 7. 19803-3742 coney ‘USA 3. Fa FAA Use Onty 4. Type S. Unit Identification Repair wierason Unit Make Model Sate No. • if AIRFRAME (As clescdbed M Rem/wow) O • POWERPLANT • • PROPELLER O O APPUANCE tyre 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 DU4R141M Class IV rr 32025 Owe, USA coneeter Mainianarek0Mtnawn 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 par 14 APP. range fat CFR Pan 43 • 8 Signs ate of A m671 A Gregory A. Christman - 28 FEB 09 7. Approval for Return to Service Pursuant Administrator to the authorey given persons below, the uNt Identified n dem 5 was inspected in the manner prescand by the of the Federal Adak., Administration and is 2 Approved O Rejected FM Fe Standards Inspector Manufacturer Maintenance Organization eenons Append by Deneefien Cepailement of Teensy:A BY FM Designee I Repair Inspection ArAlloriZatiOn Omer (SPIT*/ CerlifiCale Of Designation No DU4R141M Class n/ Sign I Anthony V. Baroni - 28 FEB 09 FAA Form 337 nom> SDNY_GM_02 759857 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 Nationally and Registration Mark The following major modification was accomplished: February 28, 2009 Dale 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 ffri Foe. Aocromi4 ow en. zizo-coth orthezoc Becoa,t Lapp Mover LiS owwwww MAJOR REPAIR AND ALTERATION ret MAUviiithe 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 N908JE Serial No 20115 1. Aircraft Maly Boeing Model 727 Series -31 Name (As shown on tegistathon condicate) JEGE Inc Address (As shown on togishation certificate) 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 Ceonciders meinuensnce Organization FOTR986N D. I certify that the repair oridlor alteration made to the unli(+) have been made in accordance well the requirements of Mnlshed heroin is Duo and correct to the best or my knowledge. identified in Mon 5 above end described on the reverse or attachments hereto Pari 43 of the U.S. Federal Aviation Regulations and that the information i Extended range fuel per 14 CFR Part 43 0 APP. B Signature/Dale of Author! ad Individual CHRIS ADAMS 30 JULY 2008 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 L Rejected FAA FN. Standards InspectOr Manufacturer Maintenance Organization Persona approved bye:moan Desarvneri or Transport BY FM Designee x Repair Station Inspection Authorization Other (Spotty) Corti math or Designation No. FOTR986N Signature/Ciato of Authorized Individual CHRIS ADAMS 30 JULY 2008 Cej , l id FAA Form 337 tooth SDNY_GM_02 759659 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 (Il more space Is required, stla0 additional shoats. Identify mei aircraft nahenegity and repotratlon mark and dote work comaltfed) WIO 8181 N908JE Nationality ON Registration Mn Oats L0 JULY 2008 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 K 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 U.S. Departmtel of (Airframe, Powerplant, Propeller, or Appliance) Transportation Federal Aviation Ad ma bin tin Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification 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). I. Aircraft Make BOEING MODEL 727-31 Serial No. 20115 Nationality and Registraioo Mark USA N908JE 2. Owner Name (As shoal on regisnatiOn eatificalc) WOE INC Address (as shown on registration certificate) 103 FOULK RD STE 202 WILMINGTON, DELAWARE 19803.3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration AIRFRAME )O( (As descriked in item I above) POWERPLANT PROM 1ER APPLIANCE Type Mumfaeturer 6. Caaferalty Statuses • A. Agency's Name and Addreu B Kind of Agency C. Certificate No. TIMCO 102 SE Academic Ave. Lake City, FL 32025 U.S. Certificated Mechanic DU4R141M CLASS IV Foreign Cenificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair sad/or alteration made to the units identified in km 4 above end described on the reverse or attachment% Mato have been made in accordance with Migliternatt3 of Part 43 of the U.S. Fedend Aviation Regulations and that the information furnished herein is true and correct to the bat of my knowkdge. Date April 28, 2008 Sisputure of Authorixed Owen H. Pritchard Individual t Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below, the unit identified in itan 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is 121 APPROVED 0 REJECTED FAA F1L Standards Inspolor Manufacturer Inspection /unhorizstion Other (%4c169 FAA Designee X Repair Station Person Approved by Transport Canada Ainuatinen Group Date olApproasi or Rejection April 28 2008 Certificate or Designation No. DU4R141M CLASS IV Signature Antb of 'vides! y V 7 WrE :;1. FAA Form 337 (12-88) Us. 00VEINMENT MINTING orna 1992.76-012.0157 SDNY_GM_02759661 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246583 EFTA01331046 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Boeing Model 727-31 S/N 20115 Reg. No. N908JE Page 1 April 28, 2008 The following major repair was accomplished: 1. OPS #24157 Repaired frozen bolt at I/B elevator hinge of RJH horizontal stabilizer by removing .023" corrosion, HFEC, no cracks noted. Fabricated and installed I ea. bushing IAW TIMCO REO-L01064 Rev. IR dated 04/14/08 approved by FAA Form 8110-3 by Richard C. Saltivan #DERT-40157-CE dated Apr. 17, 2008. SUMMARY 1. All work accomplished JAW TIMCO REO and FAA Form 8110-3. 2. Records of all work accomplished is on file at this repair station under service order 185006. 3. Aircraft was weighed and Weight and Balance updated accordingly. 4. All repairs are permanent unless otherwise stated. -end-- C I Additional Sheets Are Attached * us GOWN*41DIT PIUN114O OPICE ISMI4S-0IMI SDNY_GM_02759662 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246584 EFTA01331047 0 US Oepanntert MAJOR REPAIR AND ALTERATION Or Transportation (Airframe, Powerplant, Propeller, or Appliance) Fount aviation ...... Form Approved OMB No. 2120.0020 For FAA Use Only Office IderlaheatiOn So- rs vo- i INSTRUCTIONS: Print or type a entries. See FAR 43.9. FAR 43 Append& B. and AC43.9-1 (or subsequent revision thereof) for Instructions disposition of this form. This report is required bylaw (49 U.S.C. 1421). Failure to report can result In a civil penalty not to exceed $1,000 for such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20115 Nationally and Registration Mark USA N908.1E 2. Owner Name (As shown on registration minket.) J.E.G.E, Inc. Address (as shown on registration certificate) 103 Far* Road STE 202 Wkniegton, DE. 19803-3742 3. For FAA Use Only S.L.'. • . :"'::: • in de Idevaieti arwortors itzwirentwes e serrred bthe snow -.... spew c....... airersit OCT r diddr. 43-7 sa_f 5V 0- 1-7 el ite= Dim 4. Unit Identificat 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME '""'"'"""*"•(As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8. Conformity Statement A Agency's Name and Address 8. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 u.s. Certificated Mechanic Radio C SD4R514Mlass 1.2.3 Limited Airframe Foreign Certificated Mechanic 0 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified In kern 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 arid that the information furnished herein is true and correct to the best of my knowledge. Date o f g OCT-4912 01004 Signature of Authorized Inch ( O Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given personsSpecified below; the unit identified In Item 4 was inspected n the manner prescribed by the Administrator of the Federal Aviation Adrrinistration and Is Si APPROVED O REJECTED BY FAA Fit. Standards Inspect( Manufacturer inspection Authorization Other (Specify) FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Refection Oeneoc.;:goa4 Certificate or . lion No. Designa SD4 . 11.514M Signatur thodzed I -oZ -- • Steve Ouellette FAA Form 337 (12436) SDNYGA402759663 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246585 EFTA01331048 NOTICE Weight and balance or operating limitation changes shall be entered In the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach edationat sheets Identify with aircraft nationality and registration mark and date work completed) The purpose of this 337 is for the work performe,on 119087E under Banyan Air Service; Avionics Division work order #71301 completed on A 02 3/46 A. Installed an AirCell Iridium ST-3100 P/N 400-10680-001 and removed a previously installed AirCell AGT.01 P/N 900001-2. Minor wiring changes were made at the mating connector IAW installation manual P/N 800-10680 Rev. B dated June 2005. B. The above installation was performed in accordance with AC43.13-IB, Chapter 7, sections 1-5, AC43.13-1B Chapter.11;sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24 & 25 and the aircraft's maintenance manual. : A functional test of the aboVedquipment has been performed FAR25.B09 and FAR25 .1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. E. Instructions for continued airworthiness is attached.. END O Additional Sheets are Attached SDNY_GM_02759664 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246586 EFTA01331049 Instruction for Continued Airworthiness for AirCell ST 3100 Aircraft Subscriber Equipment System Installed on Boeing 727-100 N908JE S/N 20115 Revision O. Dated: 9/17/2006 SDNY_GM_02759665 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246587 EFTA01331050 SDNY_GM_02759666 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246588 EFTA01331051 • APPLICATION REVISIONS DESC. NEXT ASSY USED ON REV DESCRIPTION DATE APPROVED ST 3100 ASE SYSTEM BARON 95-BSS A BASELINE RELEASE 2002-10-16 K. FRANTZ B SEE OEN 00579 2002.10-25 K. FRANTZ irniet ALL SHEETS CARRY THE SAME REVISION LETTER UNLESS OTHERWISE SPECIFED DIMENSIONING & TOLERANCINt LAW ASAE Y14.5M-1994 DIMENS/ONS ARE II IN STANDARD TOLERANCES. .% t ±. .1 X< = 1.02 YYJC = ± .010 • ir e AirCell, Inc. lir C 11 1172 Century Drive Suite 280, Building B Louisville, CO 80027 APPROVED DATE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ST 3100 ASE SYSTEM PREPARED BY K FRANTZ YEAR-MO-DA 2002-10-16 MECH DESIGN Z HOH YEAR-MO-DA 2002-10-16 ELEC DESIGN B. SOUKUP YEAR-MO-DA 2002-10-16 TECH SUPPORT B. NIELSON YEAR-MO-DA 2002-10-16 SYSTEMS K FRANTZ YEAR-MO-DA 2002-10-16 ENGINEER,* J. POISON YEAR-MO-DA 2002-10-16 SI2E A CAGE CODE 1NO67 DRAINING NUMBER . 820-10680-001 REV B FILE FORMAT: Microsoft Word 2000 SCALE: NONE WEIGHT: NA SH 1 of 8 FILENAME: 820.10680-001-B.doe 65010377, A.St71 SPEC TEMPLATE DOC SDNY_GM_02759667 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246589 EFTA01331052 SDNY_GM_02759668 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246590 EFTA01331053 ge e p e 9 ft ft ft ft ft ft ft ) ft ) ) ) TABLE OF CONTENTS 1 GENERAL INFORMATION 3 1.1 SCOPE Cc THIS DCCUP•ENT 3 1.2 TECI-MAL SLFPCRT CONTACT WORMATION 3 1.3 GENERAL NOTES 3 1.4 Acmsomes 4 2 SYSTEM DESCRIPTION 2.1 TCPLEVEL SYSTEM COVIGURATICN 2.2 OPERA1O4OF1HE SYSTEM 6 3 OPERATIONAL TIME LIMITS AND SCHEDULED MAINTENANCE 4 UNSCHEDULED MAINTENANCE 4.1 TRnan Fs-DOINGPRO:IMRE 5 AIRWORTHINESS LIMITATIONS 7 7 7 7 FIGURES AND TABLES Table 2.1-1 System Component Definition 6 Figure 2.1-1 Block Diagram of ST 3100 ASE System 6 AltrCelf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE A CAGE CODE 1NQ67 DRAWNG NUMBER 820-10680-001 REV B FILE FORMAT: Microsoft Word 2000 I SH 2 of 8 FILE NAME: 820.10680-001 43.doc ST EOM ASCE SPEC TEMPLATE DOC SDNY_GM_02 759669 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024659 I EFTA01331054 SDNY GM 02759670 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246592 EFTA01331055 1 GENERAL INFORMATION 1.1 SCOPE OF THIS DOCUMENT This manual defines the instructions for continued airworthiness (ICAW) for an AirCelI 3000 Series Aircraft Subscriber Equipment (ASE) system. The manual is written to demonstrate compliance with FARs 23.1529 and 25.1529. Specifically, this manual defines the Instructions for the Model 3100 Satellite Telephone System (ST 3100). This manual is subdivided into sections to support the general operation, Inspection and maintenance of the ST 3100 system. Section 1 defines general information for the maintenance and airworthiness of the ASE system. Section 2 provides general Information on the configuration and operation of AirCell ASE systems. Section 3 presents a discussion of the scheduled maintenance and operational time limits for the system. Section 4 and Appendix A provide instructions for system operational checks, troubleshooting, unscheduled maintenance and component replacement. Section 5 provides a brief statement addressing airworthiness limitations for the ST 3100 system. 1.2 TECHNICAL SUPPORT CONTACT INFORMATION Technical support for AirCell products is available from 08:00 to 17:00 United States Mountain Time (Time Zone GMT —7 hours) Monday through Friday. The contact information for AirCell Technical Support is as follows: From a landline: Phone (in the US): 1.888.286.9876 (toll free) Phone (outside the US): 001.303.379.0278 (toll call) From an AirCell phone: From an Air Mode/AMPS phone (in the US): 611 (toll free) From a SAT Mode (Iridium) phone (worldwide): 2471 (toll free) Email: customerservice@aircell.com Note: The toll free numbers for AirCell phones will only work for AirCell provided phones and services. 1.3 GENERAL NOTES • All pages in this document carry the same revision level. Revision status is indicated by a letter printed on each page of this manual. • The material in this manual is subject to change. Before planning or performing any installation or maintenance operation, check with AirCell Technical Support to verify that this manual is complete and has the latest revision. • AirCell, Inc. welcomes your comments, suggestions, and corrections concerning this manual. Please include in your correspondence the publication number, equipment part number, page or figure number, and a brief description of any problem or consideration you noted. Please send your comments to: AirCell, Inc. Corporate Publication Coordinator 1172 Century Drive Suite 280, Building B Louisville, Colorado 80027 cpc@aircell.com t kirrCelf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NQ67 820-10680-001 B FILE FORMAT: Micro oft Word 2000 I SH 3 of 8 FILE NAME: 820-10680-001 -B.doc csioon kSZE SPEC TEURATE.DOC SDNY_GM 02759671 f 4 I I $ t G Q G i Q Q V ert V et a • a ot Se SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246593 EFTA01331056 SDNY GM 02759672 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246594 EFTA01331057 *) • • • • • 0, b ► 1.4 ADVISORIES WARNING Statements in this section contain critical safety information. Read these statements carefully before installing this unit. WARNING Observe standard safety precautions and wear safety glasses to prevent personal injury while performing maintenance on this unit in the aircraft. WARNING Shut off power before connecting or disconnecting the ST 3100 system, as voltage transients may damage the unit or the interface wiring. WARNING Components or subassemblies found in this unit may contain materials such as beryllium oxide, acids, lithium, radioactive material, mercury, etc. that can be hazardous to your health. If the component enclosure mat is broken, precautions must be taken against personal contact or inhalation in accordance with OSHA requirements 29CFR 1910.1000 or superseding documents. AirCell strongly discourages the opening or disassembly of sealed components. WARRANTY AND CERTIFICATIONS Any alteration of this product voids the FAA or FCC certification and the AirCell warranty. 2 SYSTEM DESCRIPTION The ST 3100 ASE system provides access to a range of two way communication options from an aircraft, including voice and data applications. With the ST 3100 system these services are available when the aircraft is in the air or on the ground. The AirCell satellite mode communications link Is provided using the 1600 MHz Iridium LEO (Low Earth Orbit-485 miles altitude) satellite network, which provides coverage from the ground up over the entire surface of the earth. 2.1 TOP LEVEL SYSTEM CONFIGURATION The ST 3100 system consists of a number of primary system components. The heart of the system is the ST 3100 ASE Transceiver, which includes internal electronics to support operation in the Iridium satellite network. Other system components include the externally mounted antenna, a low loss coaxial cable, and various user interfaces including multiple ASE handsets (up to 9), an RS-232 data port, and an audio panel interface. AirCelf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWNG NUMBER REV A 1NQ67 820-10680-001 B FILE FORMAT: Micro oft Word 2000 I SH 4 of 8 FILENAME: 820-10680-001•Eldoc CGS XOTT. A. SIZE SPEC TONI-Alt 1:QC SDNY_GM_02759673 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246595 EFTA01331058 SDNY_GM_02759674 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246596 EFTA01331059 • *4_,,,..Transceivet The primary components of an ASE system include Line Replaceable Units (LRUs) and AirCell specified assemblies (such as coaxial cables or wiring harnesses) that are manufactured or purchased by the system installer. A list of the LRUs and specified assemblies is provided in Table 2.1.1, and a representative block diagram is provided In Figure 2.1-1 to demonstrate the interconnection of a typical ST 3100 system. For detailed information on the system components, please refer to ST 3100 ASE System installation manual (AirCell document 800-10680). or contact AirCell Technical Support for assistance. Table 2.1.1 System Component Definition System Component Designatlo n Description AirCell PH. Approved Alternate(s) AirCall PH of Alternate System Transceiver tRU ST 3100 _ASE Transceiver 400-10680-001 none : Mounting Tray LRU 3/8 ATR Wen Mounting Tray 800007.1 3000 Seder Mounting Rails 151.10689.001 System Wiring Harness Specified Assembly 26 wire System Harness NA ASE Handset LRU Flush Mount ASE Handset 400-10001.10x' Standard ASE Handset Podable Colic:ad ASE Handset Custom Retracted° ASE Handset 400-10035-001C 400-10015-00r 400-10019-COr Satellite ASE Antenna LRU _ 1600 MHz Satelte ASE Antenna, Patch Style 015-10306-001 1600 MHz Satellite ASS Antenna. Blade Styx 015-10683-601 Satellite Channel Coaxial Cable Specified Assembly Low Loss Coaxial Cable NA (vendor item)" • 'X' designates the color of the ASE handsets. The system coaxial cable Is a required item that is not provided by AirCell. The system Installer will need to purchase this Item from an approved vendor as defined later in this document. 1172 Century Drive 4Airrce •e AirCell, Inc. il Suite 280, Building B Louisville, CO 80027 SIZE A CAGE CODE 1NQ67 DRAWING NUMBER 820-10680-001 REV B FILE FORMAT: Microsoft Word 2000 SH 5 of 8 FILE NAME: 820-10680-001-B.doc Mixon. xsai SPEC TDAPLATE SDNY_GM_02759675 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 t • (4 ee (4 9 4! • ar ai a ai EFTA_00246597 EFTA01331060 SONY GM 02759676 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246598 EFTA01331061 6 0 0 0 0 0 p I I p p p I I I p If I p p I \-I ME SATEUJ1E AHIDMA FUSELAGE ME SYSITU %OR SAT AN1D1NA MIX ENGIRD NO COWECTION SYS DIOR AM SYS HS CNCIR ASE 'wow CHANNEL ASE SYS HS Oat CI MED ASE HANDSET CANNEL ASE SYS HS CN ] AN HANDSET CHANNEL CD TO AUDIO PANEL ASE SYS RS232 OCT, O TO 1.5.23.2 DATA TERMNAL TO NRCRAFt PMER (28 We) AtrotArr FUSELAGE Figure 2.1-1 Block Diagram of ST 3100 ASE System Note: Each 'Handset Channel' listed above is capable of supporting up to 3 ASE handsets, making it possible to integrate up to 9 handsets in the ST 3100 system. 2.2 OPERATION OF THE SYSTEM The user interface and operation of the ST 3100 system is designed to be very similar to the operation of a terrestrial cellular or PCS phone. Some key features of the ST 3100 system are as follows: • The system will power up when the avionics master switch for the aircraft Is powered on. The AirCell system Is always on when the avionics master Is powered on. • ' The Satellite mode network provides coverage anywhere on (or above) the surface of the earth with a clear view of the sky in all directions. • To place a call from the system handset, the user must verify that the system is 'in service'. SAT mode calls are typically dialed as international long distance calls (00 + country code + phone number). After dialing, the user must press the " SND key on the handset, and the phone call will proceed as a typical cellular or PCS call. At the completion of a call, the user may press the " END key to terminate the call. • The user may receive Incoming (ground to air) phone calls depending on the in service condition. The user can answer these calls by pressing the ' SND ' key on the handset. • Data calls can be made from Air to Ground over the ST system by connecting a Data Terminal Equipment device (such as a PC) to the RS-232 port of the system. The ST system has a built in modem function, so some user setup of the DTE will be required. More detailed operating Instructions are provided for this system in the ST 3100 User's manual (AirCell document 810-10680). cifinCell. AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE A CAGE CODE 1NQ67 DRAWING NUMBER 820-10680-001 REV B FILE FORMAT: Micro oft Word 2000 SH 6 of 8 FLE NAME: 820-10880.00143.doc OPYKOn A.SLZE5PFC lEMPLATEDOC SDNY_GM_02759677 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246599 EFTA01331062 SDNY_GM_02759678 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002466((1 EFTA01331063 3 OPERATIONAL TIME LIMITS AND SCHEDULED MAINTENANCE The ST 3100 system is designed and manufactured to be maintenance free after installation. Asa result of this design, there are no operational time limits or periodic maintenance checks or procedures that must be performed for the system. Inspections and/or system verification checks are only required In the event of a system failure (On Condition), as defined in Section 4 of this document. As an option, the system operator may perform a visual inspection of the various system components at the aircraft annual inspection, or other periodic maintenance Interval as defined by the aircraft manufacturer. 4 UNSCHEDULED MAINTENANCE The ST 3100 system is designed for "On Condition" maintenance only. In the event of a system failure, the system user/aircraft operator is advised to follow the troubleshooting procedure defined in Appendix A of this manual. After performing the basic procedure, the user will either have returned the system to normal operation, or should contact AirCell technical support for additional guidance. Note that, in the process of performing the troubleshooting procedure, authorized field service personnel are permitted to perform repairs to wiring harnesses, RF cable assemblies, mounting interfaces, or (with prior approval from AirCell Technical Support) to remove and replace any of the primary system Line Replaceable Units (LRUs). AirCell does not, under any circumstances, authorize field repair or subassembly level maintenance on any LRU. Sealed LRUs should always be returned to the AirCell FAA Repair Station for evaluation and repair. 4.1 TROUBLESHOODNG RROCEDLRE Appendix A provides a guide to identify simple problems that may be identified and/or resolved with simple field inspection and test processes. It is advised that the procedure in this appendix should be performed before contacting AirCell Technical Support for additional instruction. No specialized tools or equipment are required to perform this procedure. In the event that a step in this procedure is not dear, or the results of a procedure are not conclusive, the test operator should feel free to contact Technical Support for assistance., 5 AIRWORTHINESS LIMITATIONS The AirCell ST 3100 ASE system is a non-critical communications system. In accordance with FAR 23.1529 (with Pan 23 Appendix G) and FAR 25.1529 (with Part 25 Appendix H) this system has no Airworthiness Limitations for either Part 23 or Part 25 aircraft. The airworthiness limitations section is FAA approved and specifies maintenance required under Sections 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been approved. AIrCell, Inc. SIZE CAGE WOE DRAWING NUMBER REV AirCell 1172 Century Drive A 1NQ67 820-10680-001 B Suite 280, Building B FILE FORMAT: Micro oft Word 2000 SN 7 of 8 Louisville, CO 80027 FILE NAME: 820.10680-0014.doc WMCOTT. A.SZE WIC TEMPIATEOCC SDNY_GM_02759679 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246601 EFTA01331064 SDNY_GM_02759680 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246602 EFTA01331065 4./ 0 • • I p • 9 p p b ) ) ) ) ) ) ) ) ) ) ) ) ) ) ) Appendix A ST 3100 ASE System Troubleshooting Procedure AirC iv. ell AirCell, Inc. 1172 Century Drive SIZE A CAGE CODE 1NQ67 DRAWING MJ!,16ER 820-10680-001 REV B Suite 280, Building B FILE FORMAT: Microsoft Word 2000 SH 8 of 8 Louisville, CO 80027 I FILE NAME: 820.10680401-B.doc ter1.1077). SZE SPEC TENRATE DOC SDNY_GM_02759681 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246603 EFTA01331066 SDNY GM 02759682 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246604 EFTA01331067 AirCell Symptom Possible Caine Discussion Verification Step(s) Symptom I Power is not available to ASE The handset display should always CI Verify that the aircraft power system (master avionics switch) is on. Handset Display is System be illuminated when power is O Verify that the ASE system circuit breaker is closed. not illuminated applied to the ASE transceiver. Because the failure of a handset display is unlikely, a 'dead' display O Visually inspect the displays of all installed handsets in the system. If all handsets are off, proceed to the next bullet in this list. If most handsets arc illuminated, but one is not, then proceed to Symptom 2. (One or more suggests that there is a problem with O Wall handset displays are dead, the problem is likely in the power system wiring handsets integrated in system, no handset the input power to the ASE system. In the event that the one or more before the ASE transceiver. Visually check the system connections and the wiring , harness leads between the transceiver and the aircraft power system. Repair or displays are handset display(s) are not reconnect any obvious problems. illuminated) illuminated, the user/operator should verify that aircraft power is on and O If needed, ring out the power lints per the system wiring diagram. Repair any broken wires or rework to match the system wiring diagram. available to the ASE transceiver. O If this procedure does not resolve the problem, contact AirCell Technical Support for additional guidance. Symptom 2 Handset Display is Bad connection or faulty wiring between handset and In a system with multiple handsets, if some handsets are operating and O Some ASE systems integrate multiple handsets. If more than one handset is • installed on the system, check the display on all handsets. If only one of multiple not illuminated transceiver• some arc not, then it is likely that either the handset is bad or the handsets is not illuminated, then the problem is either a bad handset or in the handset connection! wiring harness between that handset cradle and the transceiver. wiring between the handset and the O Perform a visual inspection to verify that all connections arc made in accordance (ASS System has or transceiver is faulty. with the system wiring diagram. Correct any obvious problems. multiple handsets, and the displays of most handsets are on, but one handset is not Bad hand set O If all system connections arc correct, then switch the 'dead' handset with a known good handset and retest the system. lithe handset is still dead in the new location, then the handset is bad. Contact AirCell Technical Support for repair/replacement instmetions. illuminated.) O If the known good handset is now dead, then the problem is in the system wiring/connections between the handset and the transceiver. Ring out the lines per the system wiring diagram. Specifically check for 9V power and ground leads on the HS power line from the transceiver system connector. Repair any broken wires or rework the system wiring hamar to match the wiring diagram. 0 If this procedure does not resolve the problem, contact AirCell Technical Support for additional guidance. 8 I -o c (0 C9I a-1 aC 06. tr) cc a. cc 0 c4 0 0 A-1 o_ 0 ST 3100 ASE System );.• •• ;a, *. Troubleshooting Procedure 820-10680-001, Rev B • c73 i • hn-ftteittilt. tit EFTA01331068 SDNY_GM_02759684 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246606 EFTA01331069 viiv vs sew wwwwwww ur sir er var vs se is se it IP ler vb 1St IP eV nil WI le1 k irCe1F Symptom Possible Cause Discussion VerificationStep(*) Symptom 1 Handset Display is illuminated and display indicates no signal for Satellite (SAT) mode. Possible Cause 3A System antenna does not have Line of Sight (LOS) view to satellite. The ST 3100 transceiver operates in Satellite (SAT) mode. When in coverage the ST system should detect and register for SAT mode service. If the system does not register, then it is likely that either the antenna does not have a LOS to a satellite (3A), or there is a problem with the RF channel in the aircraft (38). In this condition, it is unlikely that there is a problem with the system transceiver, Verification Test 3A O Verify that the system SAT antenna has a clear LOS to the sky in all directions. A clear LOS is defined to exist when there are no obstructions (such as buildings, trees, vehicles etc) that are higher than 30 degrees above aircraft horizon in any direction. This should never be a problem in flight. O Use the handset to enter the SAT lock mode (FCN, 3, 3) keys on the handset. The handset will display the word "IRIDIUM" when the SAT mode is locked. O Once the LOS has been established the system should register on the SAT network within 60 seconds. The system is registered when the "NO SVC" indicator is not visible on the handset display. O If the "NO SVC" indicator extinguishes, then the SAT mode is engaged, and the problem is resolved. The user may choose to make a test call and verify the operation the system. O If the-NO SVC" indicator stays illuminated, then the system cannot register, and it is likely that there is an installation or equipment problem. Either contact AirCell Technical Support for additional guidance, or proceed to Verification Test 38. No Satellite mode signal Possible Cause 3D There is a problem with the Satellite RF channel. Verification Test 3D O While the aircraft is on the ground, perform a visual inspection orate ASE system satellite antenna. Verify that the antenna is installed to the aircraft fuselage in accordance with the system antenna installation drawings. Verify the mechanical integrity of the antenna, and that the antenna is reasonably free of dirt, oil, ice and other undesired coatings. O Visually inspect the RF satellite channel, including the coaxial connections to the antenna and the system transceiver. Inspect the coaxial connectors to verify that they are connected in accordance with the system wiring diagram, and that they arc not damaged. Look for breaks, kinks or other damage to the coaxial cable. 0 The user is authorized to correct installation errors (such as cabling errors), or to repair minor damage (such as broken coaxial connections, damaged coaxial cables, etc). The user is not authorized to open or modify sealed LRUs. O If these steps do not resolve the problem, contact AirCell Technical Support for additional guidance. Other conditions For all other conditions, contact AirCell Technical Support for guidance. A-2 ST 3100 ASE System Troubleshooting Procedure 820-10680-001, Rev B Ql OO v) cc w < a_ cc Lu C Lu U Lu 0 O I- I-U Lu cTo' D EFTA01331070 SDNYGM_02759686 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246608 EFTA01331071 0 a osarenant MAJOR REPAIR AND ALTERATION nmortation For Powerplant, Propeller, or Appliance) Ask., So- Fs AdISIMMIOn Forrn Approved OMB No. 2120-0020 For FM Use Only Office klentificalion DO- iq INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision theme° for inalnadtkaa and diseosltion of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1.000 breach such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20115 Nationally and Registration Mark USA N908JE 2. Owner Name (As shown on registmeon certificate) J.E.G.E, Inc. Address (as shown on registration certificate) 103 Foot Ftoad STE 202 INihnington, DE. 198033742 3. For FM Use Only .., 4. Unit identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ►all (As described in Hem 1 War POWERPLANT PROPELLER APPLIANCE Type Manures:haw 6. Conformity Statement A. AgenCits Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft Lauderdale, FL 33309 U.S. Certificated Mechanic Radio C SDIR514M lass1.2,3 Limited Airframe Foreign Certificated Mechanic 0 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unk(s) Identified ki kern 4 above and described on the reverse or attachments hereto have been made in accordance wan the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein S true and coned to the best of my knowledge. Date October 10. 2006 Signature of Authorked c_Inr2a2,__ Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given pensoressecified below, the unk identified in kern 4 was inspected in the mater coescralial by the Administrator of the Federal Aviation Administration and SO APPROVED O REJECTED BY FM Ft. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FM Designee X Repair Station Person Approved by Transport Carlin AIWOrthilltin Grow Dab c4Approval or ion Reject Da October 10, 2006 Certificate or 0esienston No. SD4R5I4M sian2re:TrIzed I I Steve Ouellette - e--- FAA Fam 337 (1248) SONY_GM_02 759687 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246609 EFTA01331072 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An Operation must be compatible with eh pmvious alterations to assure continued conformity with the applicable ainvorthlness requirements. 8. Description of Work Accomplished (// mole space is required. Witch edthtionsi sheets Identify Sin aircraft natiOnelity and registradan mark and date work completed) The purpose of this 337 is for the work performed on N908Th under Banyan Air Service; Avionics Division work order #71301 completed on October 4, 2006. A. Installed an AirCell Iridium Antenna P/N S67-1575-109 in accordance with DER Services drawing number 2006-173-1 approved per FAA form 8130-3 signed by Robert Belgau DERT designation number DERT-510024-CE. B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 3, paragraphs 43 & 44 and the aircraft's maintenance manual. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. D. Instructions for Continued Airworthiness is "on condition only." Additional Shies are Attached SDNY_GM_02759688 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246610 EFTA01331073 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE October 07,2006 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing 172731E TYPE Airplane mil e"*A•sw macww al N a AME nyan OF APPLICANT B Air Service LIST OF DATA IDENTIFICATION TITLE DER Services Drawing: 2006-173-1 . Rev. UR tr.:. Dtd. 27-Sep-06 END END ____ Effectivity: S/N: 20115, T/N: N908JE Iridium Antenna Installation STA 515 - BTWN S-2R & S-3R END END END END END END END END END END Note: This aircraft is effected by AD 98-11-03 RI. Certification to FAR 25.571, Damage - tolerance and fatigue evaluation of structure may be required. Per Advisory Circular 25.1529-I Instructions for Continued Airworthiness of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 4/11/2003. Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering design data and is not installation approval. (Ref. 8110.45 8/30/02 for more info) 2) This approval is valid for the aircraft model and aerial amber listed below 3) This approval is based on FAA Approved structural analysis on file at DER Services Office in Ft. Lauderdale, FL. or DER Services, Inc. office in Birmingham AL. Model No. 727-31 Serial No. 20115 PURPOSE Approve data for low profile antenna installation (structural aspects only, Stalls Analysis) OF DATA APPLICABLE REQUIREMENTS (LIST SPECIFIC SECTIONS) CAR 46.200, 46.201, 4b.202, 4b.260, 4b301, 46.302,46.303, 4L106 CERTIFICATION - trader antbotity vested by dirt-thee of the Administrator ad is accadaace with coadidos sod limitation of sppolatrant oder Part IS) of the Federal Mimics Repletion, data listed been tanated In accordance wltb established proudest sad toad to comply with applicable regainmeas of the Fatal Aviation Repletion O Reamstend approval of these data I (We) Therefore iril Approve these data SIGNATVRUS) Or DESIGNATED ENGINEERING REPRESENTWEW) DESIGNATION MAIDENS) CLASSIFICATIONS) -rid, esen---(•••-•- Robert J. Belgau DEBT-510024-CF. Structures IAA FORM II 14.311i.n)strrascou PittViOUS tOrrilXv DER SERVICES PROJECT NO. F2066-173 SDNY_GM_02759689 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246611 EFTA01331074 SDNY_GM_02759690 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002466 I 2 EFTA01331075 en •er Cg 8 7 6 5 4 3 I 2 D C 8 A GENERAL NOTES: 1. FABRICATE PART(s) AS SHOWN. 2. BEFORE INSTALLATION OF DOUBLER. ROLL TO MATCH AIRCRAFT MOLD UNE RADIUS. 3. BREAK AU. SHARP EDGES .020/.030 R. 4. TREAT ALL REWORKED AREAS USING ALODINE 1201S (PER MIL-C-5541. CLASS 1A) AND TWO (2) COATS OF EPDXY POLYAMIDE PRIMER (PER MIL-P-233377, TYPE I). 5. FINISH ALUMINUM PARTS USING ALODINE 120IS AND TWO (2) COATS OF EPDXY PRIMER. 6. MAINTAIN MINIMUM 2D • 1/16' EDGE DISTANCE FOR AU. FASTENERS ON DETAILS; MINIMUM 2D EDGE DISTANCE ON ASSEMBLY. 7. ALL FASTENERS ARE TO BE INSTALLED IN TRANSITION-FIT HOLES. HOLE TOLERANCE PER RAVINE 8. ALL FASTENER LENGTHS ARE TO BE VERIFIED FOR TOLERANCE PRIOR TO INSTALLATION. (REF) S - 3R --- STA 510 STA 515.00 S - 2R 9. INSTALL ALL PARTS AND THREADED FASTENERS WET USING PRIAM TYPE III SEALANT ON ALL FAYING SURFACES. 10. RESTORE ORIGINAL FINISH PER 9727 M.M. 51-21. 11. PROTECT REWORKED AREA AGAINST CORROSION PER 8727 SRM, CHAPTER 5140-2. 12. REFERENCE 8727 S.R.M. CHAPTER 51.30 FOR FASTENER REMOVAL AND INSTALLATION PROCEDURES. 13. REINSTALL ALL ADJACENT STRUCTURE REMOVED TO FACILITATE ANTENNA INSTALLATION. 14. BEAD SEAL ANTENNA WITH PRC 1422 SEALENT. 15. REVISE AIRCRAFT RECORDS TO REFLECT INSTALLATION. liitss scat NA EXISTING BONDED STRAPS VR DESCRIPTION INITIAL RELEASE 09-27-200T{(4,42az DATE APPROVED 50 COUNTERSUNK RIVET NAS I 097AD4 -2 EXISTING FUSELAGE SKIN (REF) FASTENER CODES ITEM DESCRIPTION saananstrel•Wa telASANOONAIPUN .--- STA 520 OP L OPL OPL OPL OPL OPL 8 4 4 1 RIVET - NUTPLATE SCREW NUTPLATE DOUBLER - INTERNAL LI CPS-IRIDIUM ANTENNA ITEM Ott ITS20426A03- 2 4 .3 2 MS24694C55 NAS1473A3 0.050" 2024-T3 00-A-25015 D C 4- 8 567-1575-109 PART NUMBER NAME MATERIAL MIL-SPEC VENDOR Ports List BANYAN AIR SERVICE SAMOA MANI 802bra MO P/SAY02 OCCJIDA SAAAAAN Al- ORAIVIC• OM Ns /anew an , WAYS —ft •••001......s • Ca losm•army @SSA A.600a. as a —AV we •PO I•al. WI OA••• S•••• ••••• .. NAAA/AAO Atari seorvic• ••• Poo era SY Fmoun AA amith Sr. re ...CMS_ gs'atiNINSEP UNSPEEISIED TOLERANCE LIT Mit orICHA 09-27 2006 a DER OW la tin ~SERVICESI 100 IRIDIUM ANTENNA INSTALLATION STA 515 SINN S-2R 8 S.3R FOLIOS NCLES !I/32 8 7 5 IECDIALS A Si t 43 Tu. t AI 4 MAW m W.D.OUVERI sacs IPA R.J.BELGAU miss to W.D.OUVERI ammo rn R.J.BELGAU Ait NT. BOEING stt w.. 727-3f us. w N902KIE stRAL IA .20115 r 2006-173-1 0. 3J g 2006-173 nt NA. no fir 3- 1 av !TR STRL INSTL 1 3 2 A N at C in I. Lri O ri z O vi • ri cri 0 R re <9 cc cc 0 EL 0 O cc o_ 0 V) EFTA01331076 SDNY_GM_02759692 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246614 EFTA01331077 8 7 6 5 4 3 2 C 4 a A STA 510 EXISTING FUSELAGE SKIN (REF) x4 STA 515 A 01.00 CONNECTOR CUTOUT IN SKIN 0 0 • 0 0 0 0 0 0 • •••• • o • • • r • • ° ea f a • • • • .. • • • • • it • 0_1_ • 0 • 0 • 0 • 0 A -I VIEW LOOKING UP SOME STRUCTURE REMOVED FOR CLARITY 4 STA 520 IRIDIUM ANTENNA INSTALLATION © STA 515.00 - BTWN S-2R 8 S-3R EXISTING BONDED STRAPS (REF) EXISTING BONDED STRAPS (REF) - S - 2R LBL 12 - S - 3R Tins roe... •CoW001.6.NOMPAIMICDOCCOMPThano. an AN OMR • 01111.... As. es se glea. Ow 6.. ..•••• • Ca *tan as, lie% saminitaarretwa frea. emeid Op talon on am man OM Wows Sauey wan an W ream.. is. gab ninimio•00.6,420 RAY no Om off miner% fa. manors shale...a/ de. •••••••••••3 IMMWA 8 I 7 5 4 EXISTING BONDED STRAPS (REF) EXISTING FUSELAGE SKIN (REF) SECTION A-A DER SERVICES ir 2006-173-1 rt lailiatia FL la •••••••• ONINSWHINO MIA B W.D.OUVERI OR swot or 20115 KA13•4 I, wit 2 If 3 3 I 2 1 D C 4- a A 8i r-r at E,4 C tn (13 ri c cri 00 r-: (n cc C9 cc CL LLI 0 0 w H U cc a_ 0 H U tn EFTA01331078 SDNY_GM_027596. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002466 I 6 EFTA01331079 a O a 0.75 O, 0.00 0.38 1.13 1.50 1.88 2.25 ! MINI i i iiiqi i .. il ii i i i 4.50 O I it " I I I 4.88 O 5.25 O O O O to Oft t tit. 5.83 O O O I. O .._ I j.! I iiti i 6.00 lit' .0, q, 1 i ri 1 ,:' ,.., z 0 Jo) 0 Ei OK% °WM (7 ill va 2.83 O 3.00 3.38 ---O 3.75 4.13 XV a 0, 4- O O SDNY_GM_02759695 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246617 EFTA01331080 , SDNY_GM_02759696 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002466 I8 EFTA01331081