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 4066[SSN REDACTED]). REINSTALLED REPAIRED I MODIFIED TCAS PROCESSOR P/N 4066010.913 (SIN 91050384) AFTER INCORPORATION OF ACSS ATA SB 4066[SSN REDACTED]. 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. [ADDRESS REDACTED] 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,[ADDRESS REDACTED] 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:[ADDRESS REDACTED]ates 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: [email protected] 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 [email protected] 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 0 ._ us Depactran MAJOR REPAIR AND ALTERATION or Trainecetarthe Faders (Airframe, Powerplant, Propeller, or Appliance) Awoke, MminIstnalon Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification So- re) Do - /7 INSTRUCTIONS: Print or type all enures. See FAR 43.9. FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions and C0SP0SIt0rl of this them. This report is required by law (49 U.S.C. 1421). Faure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act o(1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20155 Nationafity and Regisbabort Mark USA N908JE 2. Owner Name (As shown on registratlan cerfAkate) J.E.G.E. Inc. • Address (as shown on rogistrstion certificate) [ADDRESS REDACTED] Wimington, DE. 19803-3742 3. For FAA Use Only 4. Unit Identification s. Type Unit Make Model Serial No. Repair Alteration AIRFRAME """""•"'s(At 0. deserted Mir 1 above POWERPLANT PROPELLER APPLIANCE Type Manufacturer IL Conformity Statement A. Agency's 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 Cl SD4R514M ass 1,2,3 Limited Airframe Foreign Certificated Mechanic 0 Certifkated Repair Station Manufacturer D.1 certify that the repair andkit alteration made to the unit(s) lammed in Kern 4 above and described on the reverse or attachments hereto have been made in accordance %Nth the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is We and coned to the best of my knowledge. Date • 8 November 2004 Signature of Autheria2.3.1 .4 _,./2 : x i / et_ Zoe/ Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in Item 4 was Inspected In the manner prescnbed by the Administrator of the Federal Aviation Administration and is APPROVED O REJECTED BY FAA Fit. Standards inspector Manufacturer inspection Amthorlzabon Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Atheorthiness Group Date of App oval or Rejection 19 November 2004 Certificate or Designation No. 9D4R314M Signature of Authorized Individual d2l egit u t_ .... .... ) Steve Ouellette FAA Form 337 02-88) SOFIY_GM_02 759897 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246619 EFTA01331082 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 (II more space is required, attach additional sheets Identify with aircraft nationality end registration mark and date work completed) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing TDR-94 transponders P/N 622-9210-003 and routed to the manufacture for upgrade to P/N 6252-9210-007 to provide flight ID. System ground and flight checked good. B. The weight & balance is not affected and equipment list was updated. C. Instructions for continued airworthiness are "on condition only". END O Additional Sheets are Attached SDNY_GM_02759698 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246620 EFTA01331083 0 - - US Deponmem MAJOR REPAIR AND ALTERATION a Federal (Airframe, Powerplant, Propeller, or Appliance) A,&gon AdmiNstraban Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification f 1 50 •3/4 1451)6P-47 ! INSTRUCTIONS: Print or type all obits. See FAR 43,9, FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for Instructions a disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report Can result in a Civil penalty not to exceed 31.000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Boeing Model 727-100 Senal No. 20115 Natlonaity and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E, Inc. • Address (as shown on registrallon certificate) [ADDRESS REDACTED] Wilmingten, DE. 19803-3742 -- 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair il terabon • AIRFRAME •m1-----"(AS described in Item 1 abover--- --- el POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Confomilty Statement A Agency's Name and Address B. Kind Of Agency C. Certificate No. BANYAN AIR SERVICE u.S. Certificated Mechanic AVIONICS DIVISION Foreign Certificated Mechanic SD4R514M Radio Class 1.2,3 1635 NW 51st Place I81 Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer 0. I certify that the repair ancllor alteration made to the unit(s) identified In item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my knowledge. Date / ar A‘l/eifrilge? a '°‘71 signature of Author iduaadail. Steve Ouellette . 7. Approval for Return to Servile 1 Pursuant to the authority given persons Federal Aviation Administration and is cified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the APPROVED O REJECTED BY FAA Ft Standards Inspector Manufacturer inspection Authorization Other (Specify) FM Designee X Repair Station Pilsen Approved by Transport Canada Ainvorthiness Group Dale of Approval or Refection , /9 ferewisel_ace Certificate or Designation No. SD4R514M Signature win /* II '''''' Steve Ouellette FM Form 337 (12-83) SONY_GM_02 759699 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246621 EFTA01331084 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. O. Dinalotion of Work Accomplished (It more space is required, attach wititional sheets. Identity with aircraft flattened), and registration mark and date week completed.) The purpose of this 337 is for the work performed on N908JE under Banyan Air Service, Avionics Division work order #68062. A. Installed a Universal Avionics Systems Corp. Terrain Avoidance and Warning System in accordance with SIP Technical Services, Inc. data list 7280-DL-001-501, Rev. H dated December 5,2002 or later. (STC# ST09951SC) 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 2, paragraphs 24, 25, and 28, AC25-23 and the aircraft's maintenance manual. C. A functional test of the above equipment has been performed FAR25.1309 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. A weight & balance was calculated. An FAA approved flight manual supplement provided with the above STC, Document No. 7280-FM-001, dated December 13, 2002 or later E. Instructions for continued airworthiness provided by SIP Technical Services Report No. 7280-ICA-001 Rev. F dated June 6, 2002. END O Addilional Sheets are Attached SDNY_GM_02759700 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246622 EFTA01331085 !tuna ,tate• Of eetencriut ptpartment of Zaransparintion - gehrrnl cikbizition jktiministralion Supplemental Egpr aertifirate &-iftesah• award/0 ST09951SC SIP Technical Services, lac. 10107 McAllister Freeway San Antonio, TX 78216 era 4u ea or., b. a yr , .4.9.A. GMerowasis, sear assi sznetena4 ZZONA•aJ 44000S01 07,0r4 46 sabsbablefibeiki yerabiwaseisti ivegiwit 4b 1/c& Civil Air Sacjiaral.r. ektouregkv&e., .Fif/se KelOoszie ./Ifiest4e: A3wE ada.4.. Boeing -0 -4•441: 727-100 Series giosootavb ("rem atogw, War Installation of a Universal Avionics Systems Corporation Terrain Awareness and Warning System in accordance with SIP Technical Services, Data List 7280-DL-001-501, Revision H, dated December 5, 2002, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document Number 7280-FM-001, dated December 13, 2002, or later FAA approved revision is required. Siouratavw resireassia4nS. Compatibility of this design change with previously approved modifications must be determined by the installer. If the bolder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. 82.3 Kra // that" andh& JOISWee41, data rairket t‘t iftweVa.b syrbata-osvas:b 6. viren.a Jae...staved Ja4neneed nrchetaia, a knasinalien W.4 I cawrae intateW4. 44 aiiauh,:serato, 044 .3i.t4e,ae l../Sevialeys ../erkstoeVeciZievs. Sate cideesivs4Pbalebvs August 02, 2001 Sale oeisia4.44r :December 13, 2002 eee:i.kteae.- gek amended.. (ml.) Mr ai ion of this certificate is p bisbthla by s 1455 or not racemi,y Q. 000, or opt rower, PM Son 1110.3(10-4•I Paha l a 29 I fl air, or both. s certificate soy he traiarare0 to scnrdsacs with OA 22.57. SDNY_GM_02759701 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246623 EFTA01331086 SDNY_OM_02759702 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246624 EFTA01331087 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 FAA APPROVED • AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-100 WITH UNIVERSAL AVIONICS SYSTEMS CORPORATION DUAL MULTISENSOR UNS-ID+ FLIGHT MANAGEMENT SYSTEMS • REG IL N908TE SERIAL #. 20115 This supplement must be attached to the FM Approved Airplane Flight Manual when the Universal Avionics System Corporation UNS-1D+ Flight Manitgement System (FMS) is „installed in accordance with field approved 337 dated eV:: /la/ (21O(-)le . 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 basic Airplane Flight Manual. FAA APPROVED Gary Justice Principal Avionics Inspector Federal Aviation Administration Flight Standards District Office #17 Ft. Lauderdale, FL 33315 Date: NOV 8 2004 Rev. 0 VFilige 1 of 9 SDNY_GM_02759703 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002436625 EFTA01331088 4 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 Table of Content' SECTION PAGE GENERAL 3 LIMITATIONS 3 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 3 PERFORMANCE 8 Revision 0 Ail Date: NOY 8 2004 Pages RECORD OF REVISIONS Description Initlal Release Rev. 0 Approved . NOV 8 2001 *Et: O. Page 2 of 9 SDNY GM_02 759704 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246626 EFTA01331089 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D. FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION I - GENERAL 1. INSTALLATION DESCRIPTION. The Universal Avionics Systems Corporation dual FMS's use inputs from their integral GPS Receivers, Navigation Receivers and DME Transceivers to provide a blended position for navigation. Each FMS contains an Internal TSO C129a GPS sensor (GNSS 2400), which is cross-wired to the other FMS such that both systems have GPS 1 and GPS 2 data as inputs. The EMS's receive air data parameters from an Air Data Computer. A Data Transfer Unit (DTU100) is used to load periodic navigation data base updates via zip disks. The systems provide navigation and steering data to the flight director/autopilot system. Refer to the appropriate Operators Manuals as applicable. The FMS's contain software SCN 8021902 which provides capability for point-to-point navigation, as well as SIDs, STARs, holding patterns and GPS approaches. These SCN's comply with requirements of TSOs C115b and C129a Class Al when interfaced to the internal GPS sensors which are TSO C129a Class Al/B1/C1 certified The UNS- 1D+ FMS may contain either a GLONASS sensor or a GPS sensor, depending on hardware configuration. Lateral and Vertical deviations are provided for En Route, Terminal Area and Approach operations, including GPS overlay approaches. Approaches may be FCS coupled both laterally and vertically. Multi-Mission search patterns are available with SCN 902. 2. LATERAL NAVIGATION APPROVALS. Provided the FMS multi-sensor navigation system is receiving usable signals, it has been demonstrated capable of and has been shown to meet the accuracy specifications of: VER/IFR En Route domestic, Terminal and Instrument Approach (LOC, BC, GPS and GPS-overlay NDB, VOR, VOR-DME and RNAV) operations within the U.S.National Airspace System using the WGS-84 coordinate reference datum in accordance with the criteria of Advisory Circular AC 20-130A and AC 25-15. Satellite navigation data is based upon use of only the Global Positioning System (GPS) operated by the United States. Additionally, Russian GLONASS satellites provide increased accuracy but are not used for integrity or Receiver Autonomous Integrity Monitoring (RAIM) calculations or predictions. The dual FMS installation with dual internal GPS sensors, as installed, complies with the requirements of FM Notice 8110.60 for GPS primary means of Class II navigation in oceanic and remote airspace (including NAT MNPS in accordance with AC 120-33 and 91-49), when used in conjunction with the Universal Flight Planning Program, PN 10751 with SCN 24.0 or later FM approved version. This does not constitute an operational approval. Date: NOV 8 2004 Rev. 0 Page 3 of 9 SDNY_GM_02759705 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246627 EFTA01331090 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION I — GENERAL (cont.) Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 RNP- Approvals The dual multi-sentor FMS installation integrates dual GPS sensors and complies with equipage and accuracy requirements of FAA Order 8400.12A paragraph 12b(4), for operations in RNP-10 airspace. This does not constitute en operational approval. This installation also complies with equipage and accuracy requirements of AC 90- 96 paragraph 7b(1), 7d(3)(a) 2, 7d(3)(e) for BRNAV (RNP-5) when operating in Class I airspace, without time limits. The table details time limitations placed on RNP-10 and BRNAV operations with minimum sensors in NAV mode. Sensors Available RNP-10 Limitations RPN-5 (BRNAV) Limitations minimum dual FMS's required) (minimum single FMS required 1 GPS only N/A No time limitation when used in Conjunction with UFP VOR/DME only N/A No time limitation DME/DME only N/A No time limitation 3. VERTICAL NAVIGATION APPROVAL The dual Flight Management Systems, as installed, meet the requirements for VFR/IFR En Route, Terminal Area and Approach VNAV operations in accordance with the criteria of AC 20-129 and AC 90-97, paragraph 7.a (2). SECTION II — LIMITATIONS 1. The FMS Operator's Manual, Report Nos. 2423sv802/902 Dated 9/16/03 (or later revision) must be available to the flight crew whenever navigation is predicated upon the use of the Universal Avionics Flight Management System. 2. The system must utilize software version SCN 802/902.X, where X represents FAA approved minor changes. 4. IFR En Route and Terminal navigation are prohibited unless the pilot verifies the currency of the database or verifies each selected Waypoint for accuracy by reference to current approved data. Date: NOV 8 2004 Rev. 0 • Page 4 of 9 SDNY_GM_02759706 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246628 EFTA01331091 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908..IE BOEING 20115 Ft. Lauderdale. FL 33309 SECTION II - LIMITATIONS (cont) 4. Instrument approaches must be accomplished in accordance with approved instrument approach procedures that are retrieved from the FMS database. The FMS database must incorporate the current update cycle. a. Instrument approaches must be conducted in the Approach-mode, and GPS Integrity monitoring (when using GPS for approach guidance) must be available at the Final - Approach Fix, as indicated to the pilot by the 'GPS INTEG' amber annunciator being off. b. When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS navigation, the aircraft must have.. operational equipment capable of using that navigation aid, and the required navigation aid must be operational. c. GPS can only be used for approach guidance if the reference coordinate datum system for the approach is WGS-84 or NAD 83. d. GPS will remain selected for all GPS approaches and any approach with a 'G" suffix to the approach identifier in the navigation database. GPS will be deselected for any pilot-defined VOR or VOR/DME' RNAV approaches. e. Pilot-defined IFR approaches must be defined using Waypoint coordinates from FMS's navigation data base. f. The FMS's are approved for pilot-defined VFR approaches as a VFR pilot aid only. NOTE: All sensors remain selected for VFR approaches. 5. When operating in other than oceanic and remote regions, the aircraft must have other approved navigation equipment installed and operating appropriate for the route of flight. 6. Displayed FMS navigation parameters are referenced to Magnetic North, and operation of the aircraft is limited to latitudes between N730 and 860o, unless magnetic variation is manually entered by the flight crew. 7. When using VNAV, the Altimeter on each pilot's panel must be used as the altitude reference for all operations. 8. ' Fuel display parameters are advisory only and do not replace primary fuel quantity or fuel flow gauges for fuel load and range planning. SECTION III - EMERGENCY PROCEDURES NO CHANGE TO AFM. Date: NC V 8 2004 Rev. 0 7 4 Page 5 ors SDNY_GM_02759707 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246629 EFTA01331092 Banyan Alr Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 SECTION IIIA - ABNORMAL PROCEDURES 1. If 'GPS RAIM' becomes unavailable (as indicated by a Message and 'GPS INTEG' (amber annunciation), continue navigating using the GPS equipment or revert to an alternate means of navigation appropriate to the route and phase of flight, as necessary. When continuing to use GPS navigation, position should be verified every fifteen minutes using another IFR-approved navigation system. 2. Should an FMS system component fail, in most cases the CDU will go blank or the 'FMS MSG' light will flash. Depressing the MSG key will display the Message Page, which will indicate the component which has failed. 3. If sensor information is intermittent or lost, utilize remaining operational navigation equipment as required. 3. The FMS and associated components are protected by the following circuit breakers: C/B Name Amos Location Bus FMS No. 1 5 Pilot 28VDC Avionics Bus No. 1 (Triple-Fed) FMS No. 2 5 Copilot 28VDC Avionics Bus No. 2 (L GEN) FMS DTU 1 Pilot 28VDC Avionics Bus No. 1 (Triple-Fed) SECTION IV - NORMAL PROCEDURES 1. OPERATION Normal operating procedures are outlined in the FMS Operator's Manual, Report No. 2423sv802/902. 2. NAVIGATION DATABASE VERIFICATION. After power-on self tests have been completed, the INITIALIZATION page will appear. The term 'NAV DATABASE EXPIRES' followed by a date will be displayed. If the actual date is later than that which is displayed, the FMS will notify the pilot with a 'DATABASE EXPIRED'-message. Refer to the Operator's Manual for navigation database update instructions. 3. SYSTEM ANNUNCIATORS Each FMS has the following annunciations presented on the Universal Electronic Flight Instrument (EFI) displays (refer to the EFI Operator's Manual, as applicable) : MSG Illuminates and flashes in conjunction with the CDU to indicate a message is to be acknowledged on the MESSAGE page. SXTK Illuminates to indicate that selected crosstrack is active. FHDG Illuminates to indicate that the FMS is in Heading sub-mode. APPR Illuminates to indicate that an Approach has been activated. GPS INTEG Illuminates to indicate GPS Integrity is outside of the allowable limit for phase of flight (2.0nm En Route, 1.0 nm Terminal and Approach transition, and 0.3 nm Final Approach segment). NOV 8 2004 Date: Rev. 0 Page 6 of 9 SDNY_GM_02759708 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246630 EFTA01331093 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) 4. AIRCRAFT INTEGRATION a. Universal Avionics EFI display of FMS information Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 1) FMS information is displayed on the Universal Electronic Flight Instrument (ER) displays. The associated EFI Control Panel provides control of each display. See the appropriate Operator's Manual, as applicable, for each EFI display system. 2) Lateral deviation display scaling meets with requirements of TSO C129a and AC 20-130A (5.0 nm full scale for En Route, 1.0 nm for Terminal operations, and 0.3 nm for Approach operations). 3) b. En Route and Terminal Area Flight Control System Operation 1) With 'FMS'-mode selected by using the EFI Control Panel, the respective FMS information can be presented as Flight Director steering commands by pressing the [NAV] button of the FCP-65 Flight Control Panel. 2) With reasonable navigation data being displayed, the steering information can be Autopilot-coupled, to the pilot's or copilot's Flight Director system, by pressing the 'AP ENGAGE' - button on the APP-65A Autopilot Control Panel. c. Approach Operations NOTE: ILS approaches can be retrieved from the Jeppesen database and linked to the flight plan, but cannot be armed or activated as FMS approaches. The FMS can be used to provide navigation up to the final approach course, at which point the EFI must be changed to display raw ILS data which can be coupled to the Flight Control System (FCS). NOTE: GPS will remain selected for GPS and CPS-overlay approved approaches from the navigation database, as well as pilot-defined VFR approaches. Refer to Operator's Manual, Section V, Approach Procedures. Date: NOV 8 2000 Rev. 0 ):11Y, Page 7 of 9 SDNY GM 02759709 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024663 I EFTA01331094 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) c. Approach Operations (cont.) LOC, I3/C, GPS, NDB, RNAV, VOR, VOR/DME, and VFR approaches may be linked into the flight plan and then laterally and vertically coupled to the FCS as follows: 1) Approach Transition: When an entire approach transition (e.g., procedure turn, DME arc, etc.) is to be flown, first arm the approach on the FMS (ARM APPR). If the FMS is not armed manually it will arm automatically at 30nm from the airport. With the desired DIRECT TO or FROM/TO Waypoints selected, or the desired FMS Heading selected with INTERCEPT ACTIVE, select FCS 'NAY- mode by pressing the [NAV] button of the appropriate FCP-65 Flight Control Panel. When the FMS . has automatically activated the approach, denoted by the 'APPR' annunciator displayed in the associated EFI display, press the [APPR) button of the Flight Control Panel. When the FCS has captured the "APPR" — mode, a white "VNAV" will appear on the PFD and a white VN on the ADI signifying the 'arming' of the VNAV mode. The "VNAV- and 'VN" annunciation will turn to green in color when the FCS has captured the VNAV glideslope. See the EFI operator's manual for specific display annunciations. Continue monitoring both lateral and vertical deviations throughout the duration of the approach. If required, initiate 'Missed Approach Procedures' as described in the Universal Avionics Operator's Manual. 2) Heading Vectors: If given heading vectors by ATC to the final approach course, manually activate the approach on FMS NAV page 1/3. The FMS will enter the 'FHDG" mode, the EFI display will now display final approach course data, and the INTERCEPT prompt on Nav page 1/3 will be active. When cleared to intercept final, press the INTERCEPT line select key to intercept final. Ensure that commanded heading mode is canceled. Select [APPR) on the FCS Flight Control Panel to capture and track the final approach lateral and vertical information. NOTE: Guidance is provided to the runway threshold or missed approach point. It is the pilot's responsibility to level out at MDA if the runway environment is not in sight. Date: Rev. 0 NOV 8 2004 • Page 8 of 9 SDNY_GM_02759710 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246632 EFTA01331095 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale. FL 33309 SECTION IV - NORMAL PROCEDURES (cont) Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 3) Press the APP-65A Autopilot Control Panel [AP ENG]-button to couple the AP to the selected FD. The Autopilot will track pseudo-Localizer and pseudo-Glidesbpe signals from the FMS. b. Advanced Approach Operations 1) Advanced approaches may be identified in the data base by the prefix "A° to the approach listed in the 'ARRIVAL' page and in the navigation data base They are characterized by course changes on the final approach segment of greater than 6 degrees and/or having multiple flight path angles. To avoid excessive deviations from course and flight path, these approaches may need to be flown in FCS [NAV) mode until on the final leg of the approach. Select FCS (APPR] sequencing the final waypoint to engage vertically. c. Vertical Navigation 1) Vertical Navigation (VNAV) information is displayed on the EFI display and is available for enroute, terminal or approach descents. Pitch steering commands for enroute and terminal VNAV operations are not provided to the Flight Control System. SECTION V - PERFORMANCE DATA NO CHANGE TO AFM. Date: NOV 8 2004 Rev. 0 Rage 9 of 9 SONY_GM_02759711 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246633 EFTA01331096 coos SDNY_GM_02759712 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246634 EFTA01331097 C . US Department MAJOR REPAIR AND ALTERATION Ot Transportation Anon (Airframe, Powerplant, Propeller, or Appliance) kelaton AOrrinistration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identificabon INSTRUCTIONS: Print Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent evision thereof) for instructions and ...a i disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can resutt in a civil penally not to exceed 51.000 for each such. violation (Section 901 Federal Aviation Act of 1958} 1 -71 : 11. Alreraft Make Boeing Model 727-100 Serial No. 20115 Nationality and Registration Mark USA N908JE i i2. Owner Name (As shown on registration certificate) J.E.G.E. Inc. Address (as Mown on registration certificate) .. 103 Foulk Road STE 202 Wfirringlon, DE. 19803-3742 3. For FAA Use Only Tr, data denoted .x...24 tz, M ilt: rsortilints racluirement• il desentood real subfoct =Say bf • person wrerizea tr. FAR C. al. OCT I 9 7004 ,A, , 5° - Fs Do-17 ggMsnFMbUQS Os I 4. Unit Identify atb 5. Type Unit Make Model Serial No. Repak Alteration 1 . ? , AIRFRAME '"•"--'---(As described in Item 1 above)^•^•^---^rrear *"si POWERPLANT .i ffPROPELLER r APPLIANCE Type •• Manufacturer 8. Conformity Statement A. Agency's Name and Address B. Kind of AgenCY C. Certificate No. BANYAN AIR SERVICE u S Certificated Mechanic AVIONICS DIVISION Foreign Certificatedmechanic SD4R514M Ftadio Class 1,2,3 1635 NW 51st Place ra Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer D. I Certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been. made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best cdnY knoMedge. ' Date ty,) ; a vg. se ,..200 %zr frf die Signature of A=arral 6,2 zado, _ , .A. 'r-- .. Steve Gluellette• . 7. Approval for Return to Sera* • 'pursuant to the authority given persorts specified below, the unit identified in item 4 was Inspected in the manner prescribed by the Administrator or to& Federal Aviation Administration and is APPROVED O REJECTED :Ety FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) ..t- FAA Designee X Repair Stadal Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection /9 AA4,041/1"X. a ct / • Certificate or Designation No. SD4R314M Signature of Au U I ' I Stave Ousileili FAA Form 337 (124e) SDNY_GM_02759713 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246635 EFTA01331098 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be ...,ompatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. I ra. Description of Work Accomplished 1 id more space ls required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) The purpose of this 337 is for the work performed on N908JE undo Banyan Air Service, Avionics • Division work order #68062. A. Installed an Artex ELT406-2Hivl per Artex installation document number 570.5000, Rev. A, dated 12/10/02 mounted in unpressurized aft compartment. The antenna is mounted in the aft tail section. A remote switch is mounted in cockpit in the copilot's insrtument panel. An aural activation monitor is mount within the vacinity of the ELT per the installation document listed above. • B. The above installation WaikkiredinIceordancemith 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 2, paragraphs 24, 25, an—d78;76-C43:T3,-2ATChapter 3; paragraph 38 and the aircraft's maintenance manual. C. A functional test of the above equipment has been performed FAR25.1309 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. No Weight and balance was generated as the aircraft was weighed. E. Instructions for continued airworthiness is a battery due time change. This due date is reflected on the log book entry. Annual inspection is required per FAR 91-207 (d). END 0 Additional Sheets am Attached SDNY_GM_02759714 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246636 EFTA01331099 a us Drotirtintira MAJOR REPAIR AND ALTERATION or Trareportran (Airframe, Powerplant, Propeller, or Appliance) Fedani Artiftil Aterdnisinakm Form Approved OMB No. 2120-0020 For FAA Use Only office Idenb5cabon . INSTRUCTIONS: Print or type al entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent °vision thereof) for instructions and ;disposition of this tone. This report S required by law (49 U.S.C. 1421). Failure to report can result Ma civil penalty not to exceed 51.000 for each such. iiridation (Section 901 Federal Aviation Act of 1958). it. Aircraft Make Boeing Model 727-100 Serial No. 20155 Nationality and RegStration Mark ii USA N9081E • 2. Owner Name (As shown on legislation certificate) J.E.G.E. Inc. ' Address (as shown on ripiStration certificate) • 103 Fouls Road, Ste 202 Wilmington. OE. 19803-3742 3. For FAA Use Only Tn-, data elcnbatil canoes the Waage° at mammas is for the Move by • elniOn described Octet corionnity iri FAR 4.1, 43.T NO0uthar2004 -r-svo-f 7 Mee 4. Unit IdentifIcatc 5 Type Unit Make Model Serial No. Rep* AllareUdl .' 'AIRFRAME CI (As described In Item 1 above . POWERPLANT . i PROPELLER APPLIANCE Type Manufacturer t Conformity Statement A. Agency's 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 SOIR514M Radio Class 1,2.3 Foreign Certificated Mechanic 0 Certificated Repair Station Limited Aidrame Manufacturer 0.1certify that the repair and/or alteration made to the unit(s) identified in tern 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my knowtedge. Date I .44.05.466-4 ,,,,74/09- Signature of rodi c..._ Steve Ouellette 7. Approval for Return to Service Pursuant Feder to the authority given persons s I Aviation Administration and is below, the unit Identified in Item 4 was inspected in the manner prescribed by the Administrator of the APPROVED Q REJECTED BY FAA Flt. Standards inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Ainvorthiness Group Date cf Approval cc Rejection /9 j (4gs , see e e . - 2 2 , / Certificate or Designation No. SD4R514M Signature of Authorized Indi ' ual Steve Ouellette FAA Fenn 337 (12-88) SDNY_GM_02759715 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246637 EFTA01331100 NOTICE Weight and balance or operating limitation changes shell 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. 0. Description of Work Accomplished al more space is required, attach additional sheets. ideMily with aircraft nationality and registration mark and dale work completed) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing UNS-1D Flight Management System (FMS) control display/computer units and routed to the manufacture for upgrade to UNS-1D+. Reinstalled UNS-1D+ FMS CDU computers. System ground checked good. B. A flight manual supplement has been generated, approved and incorportated into the existing flight manual. A weight & balance and equipment list update are not required. END .z. vum 44.3 akcpc,A PIP i.S70 O Additional Sheets are Attached SDNY_GM_02759716 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 I EFTA_00246638 EFTA01331101 NOV. 8.2004 9:50AM PYKA AEROSPACE NO. 2146 P. 3 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TAWS System AFM Supplement for Boeing 727-100 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT UNIVERSAL AVIONICS TERRAIN AWARENESS WARNING SYSTEM (TAWS) AIRPLANE MAKE: BOEING AIRPLANE MODEL: 727-100 AIRPLANE SERIAL NO.: /1/7013—C REGISTRATION NO.: (-90 //6" This supplement must be attached to the FAA Approved Airplane Flight Manual when the airplane is modified by the installation of a Universal Avionics Terrain Awareness Warning System (TAWS) in accordance with FAA STC number ST09951SC. The information contained herein supplements or supersedes the basic Airplane Flight Manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic Airplane Flight Manuel APPROVED: 1--f-1,/gern yR S. Frances Cox, Manager Special Certification Office Federal Aviation Administration Ft. Worth, Texas 76193-0190 DATE October 25, 2004 Page 1 of 9 SDNY_GM_02759717 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246639 EFTA01331102 SDNY_GM_02759718 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246640 EFTA01331103 NOV. 14 4 Doc. No. 7280-FM-001, Rev A Issue 092401 Si.?. Technical Services Inc 10107 McAllister Freeway San Antonio, pc 76216 LOG OF REVISIONS TAWS System AFM Supplement for Boeing 727.100 REv, DESCRIPTION REVISED PAGES APPRD. By DATE IR New supplement All S. Frances Cox 12-13-2002 A Allow use of CDU or MFD display. Format and editorial corrections throughout. All See cover page 10.25.2004 FAA APPROVED Date: October 25, 2004 Page 2 of 9 SDNY_GM_02759719 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024664I EFTA01331104 i SDNY_GM_02759720 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246642 EFTA01331105 NOV. 8. t 4 9: 1A/1, 'YKA A A NI. i4 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TABLE OF CONTENTS SECTION PAGE SECTION I - GENERAL 4 SECTION II - LIMITATIONS 4 SECTION III — NORMAL PROCEDURES 5 1. Operation 2. Cold Temperature Operations 5 3. Systems Test S 4. Pop-Up Terrain Display 6 5. System Anntmciators 7 SECTION IV — EMERGENCY/ABNORMAL PROCEDURES 9 EMERGENCY PROCEDURES 9 ABNORMAL PROCEDURES 9 1. Circuit Breakers 9 2. Use of TERR INHIBIT switch 9 3. Response to TAWS Warnings 9 4. Response to Glideslope Deviation Alerts 9 5. Use of Flap Override Switch 10 SECTION V - PERFORMANCE 10 SECTION VI - WEIGHT AM) BALANCE 10 TAWS System AFM Supplement for Boeing 727-100 FAA APPROVED Date: October 25, 2004 Page 3 of 9 SDNY_GM_02759721 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFFA_00246643 EFTA01331106 SDNY_GM_02759722 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246644 EFTA01331107 MK 8.2004 0:514.M PYKA AEROSPACE h0. 2146 6 Doe. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 SECTION - GENERAL TAWS System AFM Supplement for Boeing 727-100 This Supplement provides general information for the Enhanced Ground Proximity Warning System installation. The aircraft is equipped with a Universal Avionics TAWS system. The system uses inputs from the air data computer No. 1, navigation receiver No. 1, radio altimeter, and the Universal Avionics UNS-1 Flight Management System (FMS) , and an internal terrain database to provide basic GPWS alerts and terrain alerts The TAWS alerts provide the crew with aural and visual indications of possible inadvertent flight into terrain. TAWS alerts are generated if one or a combination of the airplane's: 1) vertical speed, 2) rate of closure to terrain, 3) accumulated altitude loss, 4) airspeed, flap and /or gear configurations or 5) glideslope deviation is unsafe given the airplane's radar altitude and phase of flight. Terrain alerts are generated by comparing aircraft position and altitude to the EGPWS terrain database. This system also provides "Flight Plan Look Ahead" terrain alerts and warnings by comparing the FMS flight plan to the terrain database SECTION II — LIMITATIONS The TAWS display will be used for situational awareness only. Navigation must not be predicated upon the use of the TAWS. The 3-D view provides no amuck information. To avoid giving unwanted terrain alerts, the TAWS terrain alerts must be inhibited by pressing the TERR INHIEI switch when landing at airports that are not included in the airport database or when landing at an airport other than the airport in the FMS flight plan. Deviation from Aix Traffic Control Clearances is authorized to the extent necessary to comply with TAWS warning. The use of terrain awareness warning and terrain display function is prohibited during QFE operations. The current local altimeter setting must be entered in the pilot's altimeter for proper terrain alerting. The TAWS database and alerting algorithms do not account for man made obstructions FAA APPROVED Date: October 25, 2004 Page 4 of 9 SDNY_GM_02759723 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246645 EFTA01331108 SDNY_GM_02759724 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246646 EFTA01331109 NOY. 8.2004 3'514M PYKA AEROSPACE NO. 214 6 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TAWS System AFM Supplement for Boeing 727-100 SECTION III — NORMAL PROCEDURES I. Operation All aircraft crew interface is conducted through the Universal Avionics display, either multi- function display (MFD) or FMS control display unit (CD11), end system annunciator switches. TAWS terrain information may be presented on either an MTID or a CDU. The TAWS requires inputs from the following systems, radio altimeter, air data computer, VHF navigation receiver, FMS, gear position and flap position. 2. Cold Temperature Operations TAWS uses baro-corrected altitude as the reference for Fonvansd Looking Terrain Alerts (FLTA). TAWS does NOT compensate the baro altitude input for non-standard temperature lapse rates that may be encountered in extreme cold conditions, causing degraded FLTA operation. Basic ground proximity warning modes (1 through 6), as well as Premature Descent Alen (PDA), are radio altitude based and not affected. In extreme cold conditions, the aircraft will be operating at a lower altitude than indicated, thus resulting in TAWS alerts being delayed or missing. The color-banding on the TAWS display will be offset by the cold temperature altitude error. When operating into and out of airports where cold temperatures exist, the aew should be aware of the difference between the indicated baro altitude and the true altitude and the effect this has on FLTA and the terrain display. To determine the effect on FLTA warnings consult the Airman's information Manual Chapter 7 paragraphs 7.2.3d and 7-2-3e. 3. System Tests BUILT IN TEST TAWS has a Built-In-Test (BIT) function which includes Power-Up Self Tests, Initiated Tests and Continuous Tests. Where there has been degradation in capabilities that result in TAWS being unavailable, BIT annunciates the fact to the flight crew via a GPWS FAR. or TERR MOP Lamp. PRE-FLIGHT TESTS A TAWS Self Test should be conducted prior to each flight. Momentarily press the GPWS TEST annunciator. The following indications confirm proper TAWS operation: PULL-UP Annunciator Illuminated TERR Annunciator ➢luminated BELOW G/S Annunciator ➢luminated G/S INHIBIT Annunciator Illuminated TERR INHIBIT Annunciator Illuminated FAA APPROVED Date: October 25, 2004 Page 5 of 9 SDNY_GM_02759725 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246647 EFTA01331110 SDNY_GM_02759726 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246648 EFTA01331111 hil4. 4.2404 • PYKA AEROSih.E Doc. No. 7280-1 (it , Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 SECTION IIT — NORMAL PROCEDURES iCcatinuedi GPWS FAIL Annunciator GPWS TFST Annunciator illuminated Illuminated NO.2146 P. 8 TAWS Terrain Display Test Image (Colored Bars) Awe! Amtunciarions "TERRAIN, TERRAIN" "PULL UP, PULL UP" "DON'T SThlE" "SINK RATE" "GUDESLOPE" "TOO LOW TERRAIN" "TOO LOW GEAR" "TOO LOW FLAPS" "ME HUNDRED" TAWS System AFM Supplement for Boeing 727-100 Once the test is complete, TAWS will reboot During this time the Greys FAIL and TERR INOP annunciators will remain lit and a TAWS FAIL message will be generated on the MFD until the system is operational. (approx one min) NOTE: As a result of pressing the GPWS TEST annunciator again within five seconds of initiating this test, the test will canal and the TAWS computer will continue to operate without rebooting. 4. Pop-Up Terrain Display In the event of terrain alert, the map view of the TAWS display will "pop-up" on the MFD or CD1J. Pressing any function key on the display will remove the pop-up and revert to the selected display function. Prospective terrain conflicts are depicted by a star shaped Terrain Threat Symbol. Both Warnings and Cautions are annunciate(' with this symbol. Terrain warnings are a flashing red symbol while Terrain cautions are depicted by a flashing yellow symbol. Terrain threats along the flight plan are depicted by a white symbol and represent the predicted first point of conflict between the flight plan and terrain RED threat "stars" on the TAWS display indicate a Terrain Alert (30-second wanting). YELLOW threat "stars" on the TAWS display indicate a Terrain Caution(60-second waning). FAA APPROVED Date: October 25, 2004 Page 6 of 9 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 91101 SONY_GkL02759727 15, and 17 EFTA_00246640 EFTA01331112 sj SDNYGM02759728 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246650 EFTA01331113 NOV. 8.2004 9:52AM PYKA AEROSPACE ti0 2146—P. 9 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc 10107 McAllister Freeway San Antonio, TX 78216 sEall)N III - NORMAL PROCEDURES1Coneinaedi TAWS System AFM Supplement for Boeing 727.100 WHITE advisory alert " stars" on the TAWS display indicate a flight plan terrain conflict. These alerts are annunciated by a "star" on the display shortly after a VNAV altitude is entered into the flight plan or when a procedure (STAR or approach) containing altitudes is linked to the flight plan Flight plan terrain advisories do not require immediate action but indicate that adhering to the flight plan as entered will cause a future terrain alert. Waypoints and altitudes should be checked for accuracy. 5. System Annunciators The following system annunciators are provided for the system; A. PULL UP Red PULL UP annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates whenever TAWS has detected terrain in the aircraft's immediate flight path The annunciator will remain illuminated until the terrain has been cleared. Aural annunciations of "TERRAIN, TERRAIN, PULL UP" or "PULL UP, PULL UP" are also provided whenever the red PULL UP annunciator illuminates. B. BELOW GS Amber BELOW GS annunciators are located on the Captain's and First Officer's instrument panel. This armtmciator illuminates on approach whenever the TAWS has detected that the aircraft is at least 1.3 dots below the glideslope. This annunciator remains illuminated until the aircraft has returned to within less than one dot of the glideslope. Aural warnings of "GLIDESLOPE-GLIDESLOPE-GLIDESLOPE" sound until the aircraft has returned to within less than one dot below the glidepath The aural annunciation may be canceled by pressing the BELOW GS anntraciator/switch. However, the BELOW GS annunciators will remain illuminated. If the aircraft goes below the glideslope after the aural warning and light annunciation has gone out, the light and aural warning will again sound. C. GPWS FAIL Amber GPWS FAIL annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates if the TAWS has failed. FAA APPROVED Date: October 25, 2004 Page 7 of 9 SONY GM_027 59729 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFM_00246651 EFTA01331114 SDNY_GM_02759730 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246652 EFTA01331115 NOV. 8.2004 9:53AM PYKA AEROSPACE NO. 2146 P. 10 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 SECTIONH7 - NORMAL PROCEDURESiContinuedi D. GPWS TEST TAWS System AFM Supplement for Boeing 727-100 GPWS TEST switches are located on the Captain's and First Officer's instrument panel shared with the GPWS FAIL annunciator. This switch is utilized to perform a self-test of the TAWS system. E. TERR Amber TERR annunciators are located on the Captain's and First Officer's instrument panel. The "TERRAIN, TERRAIN" aural warning paired with a visual alert is indication of reduced terrain clearance. F. TERR INOP Amber TERR LNOP annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates when the terrain function is inhibited by TERR INHIB switch, terrain datah.lte is invalid or failed, terrain alert function is inoperative due to hardware failure or lack of a required input such as position or altitude. G. TERR LNILIB Blue TERR INHIB annunciator/switch is located on the Captain's instrument panel adjacent to the TERR INOP annunicator. This annunciator/switch is illuminated white visible only when the TERR INHIB is active. FAA APPROVED Date: October 25, 2004 Page 8 of 9 SDNY_GM_02759731 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246653 EFTA01331116 SDNY_GM_02759732 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246654 EFTA01331117 NOv. 8.2004 9:530. PYKA AEROSPACE NO. 2146—P. 11 Doc. No. 7280-FM-001, Rev A Issue 092401 S.1.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 SECTION IV -EMERGENCY/ABNORMAL PROCEDURES EMERGENCY PROCEDURES No change to basic Airplane Flight Manual ABNORMAL PROCEDURES TAWS System AFM Supplement for Boeing 727-100 1. Circuit Breakers The TAWS system is protected by the following trip-free circuit breakers: NAME JACATION AMPS BUS GPWS P-18 5 28 VDC Ess. 2. Use of TERR INB1B switch. The Terrain Awareness Display inhibit switch (TERR WHIR) must be placed in the INHIB position in the following conditions: 1-Whenever the FMS in the Dead Reckoning (DR) mode 2-Within 15 nrn of approach or landing at an airport not contained in the TAWS database. NOTE: When an off airport landing is required the FLTA and PDA functions should be inhibited by activation of the TEAR INHIB switch. 3. Response to TAWS Warnings When an aural 'TERRAIN, TERRAIN, PULL UP" or a red PULL UP warning light annunciates, execute a positive pull up maneuver, apply maximum rated thrust, and ascend to at least the best climb angle until the warning ceases. Notify ATC if action requires deviation of ATC cleared flight plan. When an aural "CAUTION TERRAIN", "TOO LOW TERRAIN," "SINICRATE" "DONT SINK," "'TOO LOW FLAPS" or 'TOO LOW GEAR" caution annunciates, initiate corrective action to remove the cause of the warning. 4. Response to Glideslope Deviation Alerts When the BELOW GS annunciator illuminates and an aural "GLIDESLOPE" annunciation alert occurs, initiate corrective action to fly the airplane back to the glideslope centerline. To inhibit the "GLIDESLOPE" annunciation on back course approaches, select the BELOW GS warning light/switch. The glideslope inhibit function is only available below 2000 ft AOL when the BELOW GS annunciator illuminates. FAA APPROVED Date: October 25, 2004 Page 9 of 9 SDNYGPA02759733 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246655 EFTA01331118 SDNY_GM_02759734 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246656 EFTA01331119 NOV. 8. 2004 9:530 FYKA AF.;O5:1ACi. NC. [ <16 12 Doc. No. 728O-FM-OO1, Rev A Issue O924O1 S.I.F. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TAWS System AFM Supplement for Boeing 727-1OO SECTION IV — EMERGENCY/ABNORMAL PROCEDURES (Continued) 5. Use of Flap Override Switch When landing with less than normal flaps, the FLAP OVERRIDE switch should be usesd to prevent the `TOO LOW FLAPS" turn] annunciation. SECTION V - PERFORMANCE No change to basic Airplane Flight Manual. SECTION VT - WEIGHT AND BALANCE Refer to applicable weight and balance document. FAA APPROVED Date: October 25, 2OO4 Page 10 of 9 SDNY_GM_02759735 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246657 EFTA01331120 SDNY GM 02759736 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246658 EFTA01331121 0 MAJOR REPAIR AND ALTERATION al instsatiktn (Airframe, Powerplant, Propeller, or Appliance) resew mtrallOn emo AtImbilll Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification .51, - r-s pc, - /7 INSTRUCTIONS: and disposition 81.000for each Rim or type all entries. See FAR 43.9 Appendix B, and AC 419-1 (or subsequent revision thereof) tor' 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 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. N908.1E 2. Owner Name (As shown on registration certificate) JEGE INC Address (As shown on registration certificate) [ADDRESS REDACTED] 3. For FAA Use Only 4. Unit Identification 5. Type UM Make Model Serial No. Repair Alteration AIRFRAME As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A Agency& Name and Address B. Kmd of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. [ADDRESS REDACTED] 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 T i c Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unh( ) idenfilied in item 4 above and have been made in accordance with the requirements of Pan 43 of tine and that e U.S. Federal Aviation on 11! reverse A \attachments hereto ' information furnished herein is (rue and correct to the best of my knotiledge. Date 6/12/02 Signature of Authorized Individual 1 Christoptia Hoeseuorth Inspector. , 7. Approval for Return to Service \ Pursuant Admini BY . to the authority given persons specified below, the unit dentilied in item 4 was inst3ected m the bY6 trator of the Federal Aviation Administration and is 0 APPROVED 0 REJECTED FAA R. Standards Inspector Manufacturer Inspection Authorization Other (Spear) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Refection 6/12/02 Certificate or Designation No. EYKR782D Signature of Authorized Individual k ' John K. Urso. Inspector., -;l" , -: L us` I ' 6 FAA Form 337 risen / SDNY_GM_027 59737 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246659 EFTA01331122 rr NOTICE Weight and balance or operating lirritation donor* shall be entered in the appropriate aircraft record. An alteration must be soaped :de with all previous alterations to assure continued conformity wIth the applicable altwortNness requirements. 8. Description of Work Accomplished (If more space Is required. attach additional sheers, Identify with aircraft nationality and registratim mark and date work accomplished) N9081E. BOEING 727-31, S/N 20115. W.O. 18046 REFERENCE F.A.A. FORM 337 DATED 7/2A)1 INSTALLING A UNIVERSAL AVIONICS CORP. UNS-I 19 FLIGHT MANAGEMENT SYSTEMS (FMS) WITH INTEGRAL GPS SENSORS. RECONFIGURED AIRCRAFT WIRING TO PROVIDE V-NAV DISPLAY INFORMATION ONLY. FROM THE EXISTING a 1 AND it 2 UNS-I D FLIGHT MANAGEMENT SYSTEMS. MS MODIFICATION AS ACCOMPLISHED PER THE FOLLOWING JET AVIATION DRAWINGS. WHICH ARE SUBSTANTIATED BY FAA FROM 8110-3 RESPECTIVELY: WIRING DRAWINGS. • BM-16236-410, REV A. DATEDawe SHEETS I THRU 5. TITLED - NO. I FLIGHT MANAGEMENT SYSTEM. • B727-16236.411. REV A, DATED/1/16/0Z SHEETS I THEW 5.1TfLED - NO. 2 FLIGHT MANAGEMENT SYSTEM. REFERENCE F.A.A. FORM 8110-3 DATED 4/19/02 BY SYSTEMS AND EQUIPMENT DER NO. DERT510087-NM. ACCOMPLISHED OPERATIONAL CHECKS PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21. DATED 19 MARCH 200) writ NO DISCREPANCIES NOTED. AN EMI TEST. REPORT NO.: 8727.16236-080 REV IR. SHEETS I OF 5. DATED 06/19/2001. WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY CANER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13- I II, CHAPTER 12. SECTION 3, PARAGRAPH 12- 37 AND AC 43.I3-2A. CHAPTER 2 PARAGRAPH 23f. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER FAR. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236100, REV A. SHEETS 1 THRU 9. DATED 5/8/02 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL END K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 SDNY_GM_02759738 - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246660 EFTA01331123 Apr -19-02 08:08A N 3 Curran 352 243 1011 P . 02 DEPARTMENT OF 11LAREP0RTAT ION FEDERAL AVIATION ADMDFISTRATI0N STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Apri119, 2002 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane. Radio. NA:copier. <IC) Airplane NAMEOF APPLICANT Jet Aviation Associates West Palm Beach, FL UST OF DATA IDENTIFICATION TITLE 8727.16236410, Revision A, dated April 16, 2002 0727.16236.411, Revision A. dated April 16, 2002 NO. 1 FLIGHT MANAGEMENT SYSTEM NO. 2 FLIGHT MANAGEMENT SYSTEM PURPOSE OF DATA in support of major alteration to Boeing 727-31. serial number 20115, registration number N9OSJE. APPLICABLE REQUIREMENTS (List specific sections) CFR TITLE 14. CHAPTER 1, SUBCHAPTER C FAR 25.681 (a)(b)(1) FAR 26.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581 (a)(b)(d) FAR 25.1301 (a)(b)(c)(d) FAR 25.1367 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 26.1381 (a)(b) FAR 26.1322 (b)(c) FAR 25.1431 (aKb)(c) CERTIFICATION - u..........rn ........ st feecciWe tia WM ant ad co sinthed YIN enacted NOM In. dd. A4LE.L.ARRER4 inconte...eD ...s• L no I...RR. RE oflacasto ...D.P." bin ma'am' is monism. Rub alablitbed procedens obiCowed ft amply' nii animal. dem & Eq.Ipmat REPK0'. DaliK APPreval thily. Dom NM COMOIDR Me( 41. Fete A..... 141.4 .••••• retektanet day rs., Afloat. lesiollAtios Appretsh KflaaAn 0 Rwomtnegid appnwsl .thew I W) Therefore ILI Appnn that data (Spleen tiGNAT1nt 'MGM CO EI RIPIRESOCCAlinai OCSIGNATIOM HUMIICINCCI CLASSOICATI0Nis• L. _ie./A__ DERT-510087-NIYI Systems & Equipment No an J. an FAA Form /*P0) sun/LS/DES PRZYIOUSEDmoN GP0001-433FIENAME30727414CREYADOC SDNY_GM_02759739 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024()661 EFTA01331124 SDNY_GM_02759740 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246662 EFTA01331125 Jet Aviation Associates Ltd. Bldg. 1515 Perimeter Rd. Palm Beach Intel Airport West Palm Beach, FL 33406 FAA CRS EYKR782D Document No. B727-16236-100 AFM Supplement to The Boeing Company 727-31 Serial No. 20115 FAA Form 337 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N9013JB SERIAL NO.: 20115 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 VORIDME from the Collins No. 1 and No. 2 VORIDME systems in accordance with manufacture's InstalatIon and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or later approved revision and FAA Form 337, dated ,f une 26, 2001. The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FAA Approved: 'Or c7 . ' Cif, Federal Aviation Administration Flight Standard District Office -17 1050 Lee Wegener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: June ;1.2001 Revision A. Dated: 5/3 ,:.n> Page 1 of 9 SDNY_GM_02759741 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246663 EFTA01331126 SDNY_GM_027.742 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246664 EFTA01331127 f i g , US Orartrnre of Tansp3rwlon Federal Fede AdenletIstrallon MAJOR REPAIR AND ALTERATION . (Airframe, Powerplant, Propeller, or Appliance) Aviation Form Approved OMB No. 2120-0020 For FAA Use Only Officeldenlifisation , . Eri-k- 1.3U^37 INSTRUCTIONS: and disposition $1,000 Print or type all entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subseque t revision thereof) for Instructions of this form. This report is required by law (49 U.S.C. 1421). Failure to report can re ult in a civil penalty not to exceed for each such violation (Scotian 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 shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOIE-ICRD. STE 2O2 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 6. TYPO Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer . 6. Conformity Statement A. Moneys Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. [ADDRESS REDACTED] WEST PALM BEACH. FL 33406 U.S. Certified Mechanic CRS EVICR782D AIRFRAME O. RADIO 1,2,3. i METED A/F It ENG Foreign Certified Mechanic x Certificated Repair Station Manufacturer D. I certify have furnished that the repair and/or alteration made to the wafts) 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 COrTett to the best of my knowledge. Date Signature of Authorized Individual 1/14/02 John K. Ursa. Inspector. L44 114.— 7. Approval for Return to Sera Pursuant Administrator BY to the authority given of the Federal Aviation persons specified below, the unit dentilied in item 4 As inspected In the manner prescribed by the Administration and is ig) APPROVED DI REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Sadly) FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 1/14/02 Certificate or Designation No. EVICR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance. FAA Form 337 (1288) SDNY_GM_02759743 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O246665 EFTA01331128 NOTICE Weashland balance or operating amitalion changes shall be entered in the appropriate aircraft record An alteration must be compatacfir With al:previous alterations to assure continued contumely with the applicable ainvorthiness requirements. 8. Description of Work Accomplished (If more space is requited, attach adirdonal sheets, Identify with aircraft nationality and mgistration MEM and date note accomplished.) BOEING 727-31, S/N 20115. N908.1E: W/O 17454. ACCOMPLISHED AN ALTERATION TO THE CABIN INTERIOR FURNISHING ARRANGEMENT PREVIOUSLY INSTALLED UNDER PAGE AVJET STC SA3137S0, DATED 1/17/92, BY REMOVING THE FOLLOWING INTERIOR FURNISHINGS: DESCRIPTION POSMON P/N S/N F.S. WIT 0/B AFT FACING SEAT. FORWARD SALON 303413-2 4350 401.94 R/H VB AFT FACING SEAT. FORWARD SALON 303413-10 4351 401.94 FORWARD RAI TABLE AND PEDESTAL FORWARD SALON A727-2531-001 NSN 438.50 LH AFT FACING SEAT CENTER LOUNGE 3034131 4354 73200 COFFEE TABLE AND PEDESTAL CENTER LOUNGE 727-2535-003 NSN 772.50 THIS ALTERATION WAS ACCOMPLISHED PER JET AVIATION DRAWING B727-17454-200, REV IR, DATED 1/2102, SHEETS I & 2, TITLED - MINOR DEVIATION TO STC SA3137S0, THE LIMITED 727-100 GENERAL ARRANGEMENT. REFERENCE F.A.A. FORM 8110 DATED 1/6/[ADDRESS REDACTED]RUCTURES D.E.R. NO. DERT-810028-NE. 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. I3-1B, CHAPTER TO, SECTION 2 AND AC 43.I3-2A, CHAPTER 1 PARAGRAPH 9. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS ALTERATION. END O Additional Shoots Am AttaOhod * U.S. G.P.O 1990.781.753 SDNY_GM_02759744 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246666 EFTA01331129 le MAJOR REPAIR AND ALTERATION US T Otp.vtraceni (Airframe, Powerplant, Propeller, or Appliance) olranoccetabca Federal Minion AderisisbaGen Form Approved OMB No. 2120-0020 For FAA Use Only Office IVtifictlion INSTRUCTIONS:' Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 72731 Serial No. 20115 Nationality and Registration Mark N908JE 2. Owner Name (As shown on registration certificate) JEGE Inc. Address (As shown on registration certificate) [ADDRESS REDACTED]4742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME As descnbed in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type / f I Manufacturer 6! Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Gary K Palmer [ADDRESS REDACTED] X U.S. Certified Mechanic #84544584AP Foreign Certified Mechanic Certificated Repair Station Manufacturer D. I certify Nat the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 08/01/01 Signature of Authorized Gary K Palmer Individual 7. App oval for Return to Service 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 ID REJECTED FAA Ft Standards Inspector Manufacturer X Inspection Authorization Other (Snooty) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Dale of Approval or Rejection 08/01/01 Certificate or Designation No. 84544584W of Authorized Individual x , Gary K Palmer ----Y.-42i Gary ern' 331 (12438) SDNY_GM_02759745 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246667 EFTA01331130 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. B. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration math and date work accomplished.) Firebtocked and upholstered existing, one (1) cabin single chair (Erda SIN 4359) in Townsend: Leather Lambskin Pads Alligator Embossed/Tipped Gold/Black, leather and two (2) cabin chairs (Erda S/N 4357 and 4358) in Clarence House: 1037901S-37 Velours Mohair, fabric. D.E.R. Identification 62326-01. Fireblocked and upholstered existing, two (2) cabin single chair (Erda SIN 4360 and 4361) in Old World Weavers: Edmond Petit FMPOO 10004 Zoom, fabric. D.E.R. Identification 64318-01. Fireblocked and upholstered existing, one (1) cabin single seat (Erda 5/14 4354) and one (1) three section divan (Dettmers S/N 520, 521, and 522) in Gellman Ind.: Tiburon TWeed, fabric and one (1) divan (Deitmer SIN 516) in Clarence House: 10379MS-37 Velours Mohair, fabric. D.E.R Identification 65624-01. Fireblocked and upholstered existing six (6) single cabin seats (Erda SIN 4350, 4351, 4352, 4353, 4355, 4356), one (1) LH forward sidefacing divan (Dettmers SIN 517), and two (2) 3-place reclining divans (Detainers S/N 518 and 519) in Old Weavers: EA81340013 Alfa Check, fabric and ETS J. Tessin SA.: Mastic #19075, leather. D.E.R. Identification 65059- 01. All materials meet FAR 25.853(a) Appendix F, Part l(aX1)(ifi. Aircraft seat cushions have been fireblocked as per the requirements of FAR 25.853(c) Appendix F, Part II. Amendment 25 - 83. Results of sample bum tests are documented on SAL's Test Plan #7428, #7617, #7722, and #7759 and on attached DER approved 8110-3, Identification 62326-01, 64318-01, 65624-01, and 66059-01. Seat cushions have been tagged as being in comp5ance with the applicable regulatory requirements. Aircraft seatbelts were sent to Aircraft Belts. Inc. Repair Station YB1R632K for rewebbing, work order number 0046395 and reinstalled on the seats and divans. Replaced 19 each P.L. Porter 5102300-28 seat recline Hydrolok and 6 each P.L Porter 5102300-21 divan recline Hydrolok. Hydroloks were replaced using standard interior practices. Installed Erda Hydro Legrest PIN 302617-3 and mechanical control single P/N MC15-36 on two (2) cabin single seats Erda seat SIN 4360 and 4361 in accordance with Erda drawing 302617 Rev B. Attached: FAA approved Townsend: Leather Lambskin Paris Alligator Embossed/ Tipped Gold/Black, leather and Clarence House: 10379015-37 Velours Mohair, fabric. Test Plan #7428, form FM 8110-3 dated 04/16/01, Judy Boggs, DERY-405020-CE. Identification 62326-01. Attached: FAA approved Old World Weavers: Edmond Petit FMPOO 10004 Zoom, fabric. D.E.R. Identification 64318-01. Test Plan #7617, form FM 8110-3 dated 06/20/01, Judy Johnson, DERY-405020-CE. Identification 64318-01. Attached: FM approved Gellman Ind.: Tiburon Tweed, fabric and Clarence House: 10379BIS-37 Velours Mohair, fabric. Test Plan #7722. form FM 8110.3 dated 07/12/01, Donna J. Parrish, DERY-410100-CE. Identification 65624-01. Attached: FAA approved Oki World Weavers: EA81340013 Alfa Check, fabric and ETS J. Tessin SA: Mastic #19075, leather. Test Plan #7759, fowl FM 8110-3 dated 07/24/01, Donna J. Parish, DERY-410100-CE. Identification 66059-01. Attached: Aircraft Belts, Inc.: CertificalloniPaddng List, work order number 0046395 consisting of 11 sheets. Attached: FAA form 8130-3 from P.L. Porter Controls, Inc.: 5102300-21 and 5102300-28 Hydrolocs tracking number 7723, 6751, 7176. 6759, 9495, 7367, 7368, and 9292. Pertinent data on file at International Jet Interiors, Inc. under W.0.#: 01119. Customer to install seats and divans In aircraft. Log entry has been made. EN 0 Additional Sheets Are Attached * U.S. G.P.O 1990461453 SDNY_GM_02759746 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246668 EFTA01331131 ()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) [ADDRESS REDACTED]E 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 [ADDRESS REDACTED] 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. [ADDRESS REDACTED] 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 [PHONE REDACTED] 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) [ADDRESS REDACTED] 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 [ADDRESS REDACTED] 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) [ADDRESS REDACTED] 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. [ADDRESS REDACTED] 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) [ADDRESS REDACTED] 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 [ADDRESS REDACTED] 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) [ADDRESS REDACTED] 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 [ADDRESS REDACTED] 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 [PHONE REDACTED] 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) [ADDRESS REDACTED] 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. [ADDRESS REDACTED] 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 [ADDRESS REDACTED]eil 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) [ADDRESS REDACTED] 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 [ADDRESS REDACTED] 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) [ADDRESS REDACTED] 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 [ADDRESS REDACTED] 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 [PHONE REDACTED] 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 WI= $7.41TSCC MENG DIPIAILDIT 11V403PORIAT0441:004AL "M1104 ACIYOUSTRAllat STANDARD AIRWORTHINESS CERTIFICATE I 10713114.01.4:0 istoewarce wow N90/JE PS•getrOGRAMIIMOISOOIL BOEING 727-31 • Alialair *Slat Mlle( 20115 • 4 OuliKAY TRANSPORT ♦ 14/0111/4.44404kUS Sat WILAUCC. dmilliinitoliailalmo4 past•14144/444•IMINNOM41011 Bawl ofilain Etna nil* lima r ha 1•44011 14•4.44•••••••••••44,02444ninillOwlit 411•114••••••••••••••••••• 1•4104•40 41•••••••••••••••emsbutelinik4 alma am• pmid•Whaill•144COvellobaliagesICIMMOS.441141.4 lad leek Calsolls NOT • OWS , Na COMM,/ WY* •••••• ••••••••t .4404.414 almsp••••••man* ••••••• .4•404,44.4111.14 ma NM NI IMMO/ Ir=r 4 R May 17 2001 • Imikee MS Is Sea aPeOhn bp Fav/s/fra ••••••••• altallnlin milin4•1 Mae 04.4101431:014011.11 S017 senalarrittilare awl s vIa:errs "'l emma It . FM taialC04111.1 wibila Splis4•Am Pens SD NY_GM_0275984 3 CT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, E EFTA_00246765 EFTA01331228 SDNY_GM_02759844 CT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, a EFTA_00246766 EFTA01331229 . • towymeomo.a. cowmen or........otnno..-rom...“..w..somanura. STANDARD AIRWORTHINESS CERTIFICATE • . ....,..=... SSOSLS ..........era DOSING 72741 . :=7..... 20115 • wow ?PASSPORT • ...........".................. . ..... ... .... • NOSH ... '0 .7:77-90 " S zu)A JA /-., x.4_1,7,47 .............. ...b.. FAA Fore 01004.... ....... ....... 7 TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00246767 EFTA01331230 SDNY 02/b9866 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 0024676% EFTA01331231 0 MAJOR REPAIR AND ALTERATION ILE- DtPD4449191. (Airframe, Powerplant, Propeller, or Appliance) Transportation • Federal Aviation Administration - Forts, Approved OMB No. 2120.0020 For FAA Use Only Office Montifuntion / 5 6... rt• 49 -10-... •9 / INSTRUCTIONS: Print a all entries. See FAR 43.9, FAR 43 Ardis B, and AC.43.9. I (or subsequent revision thereof for instniaions and deposition *Antis form This report is requ law (49 U.S.C. 142 I), Failure to repo rota in anion penalty not to exceed $1,000 for rucksack violation (Section 901 Federal Aviation At of I9$4 I. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N505LS 2. Owner Name (As shown on registration certificate) NORTHWEST DELAWARE CORP Address (as Amon on registration certificate) 1105 N. MARKET ST WILMINGTON DE 19899 • 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model _I Serial No. . Repair Alteration AIRFRAME --- (As deseribed in ikon I above) ••---•-•----•—••-- XX POWERPLANT PROPELLER APPLIANCE 1.4' ' 4 Manufacturer 6. Conformity Statement A. AgeneYs Name and Address R Kind of Agency C. Catifrcate Na TIMCO . Lake City Municipal Airport Lake City, FL 32025 US. Certificated Mechanic DU4R141M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. Irani& that the repair and/or alteration made to the units identified in item 4 above and dmaibed on the raven* or attachments hereto have been made in accordance with requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information Punished herein is true and carat to the beta of my knowledge. Date August 23, 1999 Signature of Authorized Individual Arthur E. Saylor 7. Approval for Return To seniadlit4e ce Pursuant Administrator BY to the authority given persons specified below, the unit identified in item of the Federal Aviation Administration and is El APPROVED 4 was inspected in the manner prescribed by the REJECTED • FAA Flt. Standards Inspector Manufactora Inspection Authorization Other (Spann.) FAA Daiftwe X Repair Station Person *woad by Tampon Canada Ainnethintss Group Date of Approval or Rejection August 23, 1999 Certificate or De:0vation No. DU4R141M Signature of Scott L. Authorized ividest Palm FAA Form 337 (12-88) This 337 supersedes 337 dated August 7, 1999 SDNY_GM_02759847 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246769 EFTA01331232 NOTICE j freight 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 Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) Boeing 727-31 Reg. No. N505LS S/N 20015 August 23, 1999 Page 1 The following major repairs were accomplished: I. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 56 IAW TIMCO E.O. 99-1190 Rev. PR dated 12 JUL 99 Approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delmainated skin above #2 engine pylon L/H side at stations 1342.4, I371.5 and 1387.85 IAW TIMCO E.O. 99-1191 Rev. lilt dated 23 Jul 99 approved per FAA Form 8110-3 by DER D. Joynes DER #DERY-635317-NM dated 21 July 99. 3. 060H I-0027 Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR Engineering Repair Data Sheet and FAA Form 8110-3 by DER Jeffrey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished IAW TIMCO E.O.'s, ROHR Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished is on file at this repair station under work order 060/T-361. --end- 0 Additional Sheets Are Attached us.00wormarridonnia onyx ien.resoivout SDNY_GM_02759848 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246770 EFTA01331233 ft) MAJOR REPAIR AND ALTERATION US. Depannum of (Airframe, Powerplant, Propeller, or Appliance) Transportation e Federal Aviation Admbdstradon Pam Approved monk. 21204020 For FAA Use Only Office Identification .4OO'—ear 7/ INSTRUCTIONS: Print r twee all nitrite See FAR 43.9, FAR 43 midix B sad AC.43.9.I (or subsequent revision thtreof for inskucticas and ffisporaion °PM form. This repro is requiredby Mae (49 U.S.C. 1421). Endure to rep m tan In 4 C1•11 penalty nee to exceed 11,000 for esch such violation (Section 901 Federal Aviation Act of ISIS) I. Aircraft Make Boeing Model 727-31 Said No. 20115 Nationality and Registration Mask N505LS 2. owner Name (As shown on regittration«rtificato) NORTHWEST DELAWARE CORP Address (u shown on registration cobra:ate) 1105 N. MARKET ST WILMINGTON DE 19899 3. For FAA Um Only 4. Unit Identification 5. Type - Unit Make Model I Serial No. Repair Alteration AIRFRAME XX GU described titan I above) POWERPLANT PROPELLER APPLIANCE TY,. Manufacturer 6. Conformity Statement A. Agway's Name and Addams B. Kind of Agency C. Certificate No. TIMCO • Lake City Municipal Airport Lake City, FL 32025 US. Certificated Mechanic DU4R141M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair ancVor alteration made to the units identified in item 4 above and desaibed on the male or attachments hereto have been made in moord.uwe with requirements of Rut 43 of the V.S. Federal Aviation Regulations and Out the information famished herein is we and coirect to tiro tent of my anossIcdgc. Dale August 7, 1999 Signature otAuthorized Gregory A Christman,/ FTh 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below, the unit identified in item 4 was inspected in the prescribed by the of the Federal Aviation Administration and is Z APPROVED O REJECTED FAA Fit Standards inspector Manufacturer . Impaction Anthorization Other (SpeeiM FAA Designee X Repair Station Person Approved by TransprtCuada Airworthiness Ciro Dale of Approval or Rejection August 7, 1999 Certificate or Daignation Nn DU4R141M Signature of ottL am FAA Form 337 (12-88) SDNY_Gh4_02759849 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246771 EFTA01331234 . 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 confonnisy with the applicable airworthiness requirements. S. Description of Work Accomplished (If more spaces required, attach additional sheets. Identify with aircraft nationality and registration mask and date work completed.) Boeing 727-31 Reg. No. N505LS S/N 20115 August 7, 1999 Page 1 The following major repairs were accomplished: I. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 45.5 TAW TIMCO E.O. 99-1190 Rev. PR dated 12 JUL 99 approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delaminated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 JAW TIMCO E.O. 99-1191 Rev. YR dated 23 Jul 99 approved per FAA form 8110-3 by DER D. Jaynes DER #DRRY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbanded #2 engine upper skin on aft fairing assembly JAW ROHR Engineering Repair Data Sheetand FAA Form 8110-3 by DER Jeffrey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished TAW TIMCO E.O.'s , ROHA Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished are on file at this repair station under work order 060/T361. end El Additional Sheets Are Attached * us. oovaionrirrinterremoenct IM449419,40U7 SDNY_GM_02759850 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246772 EFTA01331235 1u1.21. 1999, 22:06 PDT MegNum': CPZ-LR1C-99-00014H Page 2 of 2 67/Z1/99 RED IS :08 FAX 9 @Oat U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE ZZL.1 tic; 159C AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727 TYPE Glirydone, Radio. Heliconer. err.) Airplane NAME OF APPLICANT • Boeing Commercial Airplane Group LIST OF DATA IDENTIFICATION TITLE. • • CPZ-LRier89.0204-'112 Dated-9.1cl 1999 - ' CM-Lk/09-00006H Dated- /21u1.1999 • ' . • CS...ER(699-0208TR .. Dated 191ul f999 ' . . — . . . Subject Center Engine Support Side Panel Corrosion, Deb/ideation Requestor: 'HMCO (CP2) for The Limited (LH) Part Number/Serial Number. 65-17556 Model No.: 727-100 Serial No.: 20115 Basic No.: E22I8 Registry No.: N50014 Variable No.: E3704 Line No.: 735 Flight Cycles: 21643 Howl: 31835 Service Bulletin/AD: N/A . . • • . . 'HMCO telex with description of blindant end doubler repairs to corrosion and • deltunination areas at Station* /3711S: 13S7:85, and 1342.4. " Boeing reply that repairs aiditeuthiall)lideaciey With preiyefions. ...,. • : - ' ''•••• -.?.t• c. '. v. .. • ' . • . :•1Th4C0 telex witlisiaiemehtiliatiepafeliisi ()tea ChiliPleeeei Pei disieltition•aisitresjMesi' ' - ' • ' for form. • • • • . . ., . ; . ' • • PURPOSE OF DATA Structural Substantiation of Repair Plan • APPUCABLEREOUIREMENTS (List spec* naiatu) CAR 4b • Subpart C: 46200 through 46.202, 41).270 Subpart D 46.300 through 4b.304(a),46.306(a)44(b) tEFITIRCATION - Hofer of appoimment under Part 183 i have authority vested by (Erection of the Atbrdnistralor and In accordance with.condldoac of the Federal Regulations, data listed above and on attached sheets numbered been Guunined in accordancewith esmblished procedures and fouod to comply Regulations. Recommend approval of these data Approve these data and limitarions with applicable requirements of the Peden° Aviation I We) Tterefore O . elf SIGNATURFIs) OF DESIGNATED ENGIN NG FtEPRESENTATIVE(s) DESIGNATION NUMBER(s) CLASSIFICATION(s) 1). Joyner . DERY-635317-NM Structures FAA Form Form 81103 1-70) SUPERSEDES PREVIOUS EDITION Page 1 of SDNY_GM_02759551 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246773 EFTA01331236 SDNY_GM_02759852 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246774 EFTA01331237 07/15/89 15:54 FAX TURCO ENGINEERING • LAKE CITY Q002 US. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE July 12, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. . 727 TYPE (S7Fanas Rada HaFxtder. eta) Airplane NAME OF AppucANT TIMCO LIST OF DATA TIMCO E.O. 99-1190, Rev. l/R, Dated 12 JUL 99 TIMCO REPORT NO. S.A. 99-1190. Rev. VR, Dated 12 JULY 99 B727; SEAT TRACK: STATION 662. ROL 56 CORROSION BLENDOUT REPAIR. STRESS ANALYSIS; SEAT TRACK CORROSION REPAIR AT STA 663 RBL 54 END • NOTES: 1. This approval is for Northwest Delaware aircraft N505LS, S/N 20115 only. PURPOSE OF OATH In support of a Major Repair accomplished on aircraft S/N 20115. This approval is for design and static analysis only and is not Installation approval. APPLICABLE REQUIREMENTS rya *sae satiorte) FAR 25.301. 25.305, 25.601, 25.603, 25.605. 25.609 and 26.613. CERTIFICATION - Under authority vested by direction of dm Adrrirlistralce Part NM of the Federal Won Regulations. data Wad above and an wilt; estabeshed procedures and rend to comply van applicable requirements 0 Recommend approval adieu data I pm Planta* 0 Approve Mese data and In at:Cadence with conditions and Seed shoals numbered WA nave Ernitadcos ciappOintrnant inlet been examined In accordance • of Um Federal Aviation Reputations. MOROI/REM OF DESIGNATED EN&MEERING REPRESENTATIVE) DESIGNATIONsnatasts(al CLASSIFICATION(S) ti -)C3-- Wayne Fink DERT-510117-CE STRUCTURES en A Can.. 1111&L1 /.1.2.110i beaten ELECTRONIC FORMAT (449) SCNT_GM_02759853 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246775 EFTA01331238 SDNY_GM_02759854 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246776 EFTA01331239 a- J-UK 4.00 F$ ;bliedli. Z1 FKUUKAM 2/ U.S. DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTFtATiON STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE August 3, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727 _ TYPE (4apitme. Radio. lielicopeas dm) Airplane NAME OF APPLICANT Rohr, Inc. LIST OF DATA IDENTIFICATION TITLE ERDS Cl 036 dated August 3, 1999 -. B.. Cox Stress Analysis Dated August 3, 1999 • • Engineering Repair Data Sheet, Definition of discrepancy and VA545300-1 (AR Skin - Upper Skin Assembly) . Skin Disband VA545300-1 (Ref. ERDS C1036) repair design for P/N PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS (Ubisstific scams) (1) FAR 25.301 (1) FAR 25.307(a) (1) FAR 25.605(a) (1) FAR 25.619 (1) FAR 25.303 . (1) FAR 25.801(a) (1) FAR 25.609(a) (1) FAR 25.305(a)(b) (1) FAR 25.603 (1) FAR 25.613(a)-(d) .; • CERTIFICATION — Under authority appointment under Part 183 of Me NONE have been vested by direction of Pedant Aviation Regulations, examinee in accordance Regulations. ❑Recommend approval the Administrator and in accordance with conditions and limitations of data listed above and on attached sheets numbered with established procedures and found to comply with appreable of these data • requirements of the Fedaml Aviation I (We) Therefore Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING E ENTATNES DESIGNATION NUmeen(3) CLASMFICKnON(S) Structures (1) Jeffrey D.Shutrump DERY-805628-NM FAA onn 8110 11-70) SUPERSEDES PREVIOUS EDITION (rammer Serlostad try Rohr. inc.) SDNY_GM_02759855 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246777 EFTA01331240 SDNY_GM_02759856 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246778 EFTA01331241 RC/IMMO. ' ENGINEERING REPAIR DATA SHEET (ERDS) FORM 81103 REQUIRED cuiss Dux* M- al WSW. ci 036 PEV. PACE I OF 2 nIr n nu n tisnagantom Odavict.catirca otIn • me en ra WA REV. PART NO. VA545300-1 `.ART SERIAL NO. N/A SCOEL V727RE r liT kPONt AFT FAIRING -UPPER SKIN ASSY sERVCCE /CURS UNK S CUTOMER THE LIMITED REPAIR: OISCFtEPANCY: (8E SPEOFIC • PR WT CLEARLY) ITEM A. Repar. ITEM A. The upper skin on the AFT faring assembly, PIN .MA545300-1, on the #1 Engine position shows a disbonded UPPER SKIN REPAIR condition on approxknately 50% of the AFT surface, Including 1. Remove discrepant upper skh from any. Care should be two crescent shaged cracks on an existing repair (fiben2lass?). taken not to disband the lower skin of the easy. On this same are'on the lower surface of the panel, an area of 2. Fabricate anew upper skin from .032 gauge 202443 per QQ- material is also missing and fated as above. The lower reps& A-250/5. stops before transitioning to pan down of honeycomb. 3. Remove lower surface Clad (bonding side). Do not thin below See page 2 for sketch of location and description. .029. 4. Make sure all remaining "old" adhesive Is removed from core. MATERIALS: Clean and prep sldn (using PM or Pasa-Jefl 105) and exposed Upper Skin .032 2024-T3 CIO-A-250/5 core (using Pasa-Jell 105) on panel. Clean repair area per 727' Lower Skin .016 2024-0 QQ-A-250/5 SRM 51-40-6, Par. G(2) (SRM 5140-5). Heat treated to —T42 per MIL-H-6088 5. Pane bond side of skin and core with BR-127 adhesive Honeycomb .3103/16-10(5052) MIL-C-7438 primer, per manufacturer specifications. 6. Apply two coats of FM-73 adhesive material, per manufacturer specifications. 7. Bond replacement upper skin to core and tower skin per 727 SRM 51.40-6, paragraphs E, J & K 8. Perform Post Bond inspection by visually Inspection of periphery for evidence of adhesive bead, and tap test the whole panel for voids. ORnitiGailtaiAl annals' Is land Ink IP CW I 'REPASS) SY DATE AIRWORTKNESS APPROVAL ..7----.._ CATE Don Adams 8-02-99 sT £ fr,A.r4c .P-_7 - ? 7 FORIINO SOW SDNY_GM_02759857 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 co g -a EFTA_00246779 EFTA01331242 SDNY_GM_02759858 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246780 EFTA01331243 R0HR.ING. 1.11) Won Whe oda VW CM* Mir-z» ENGINEERING REPAIR DATA SHEET (EROS) SUPPLEMENT SHEET RCS NO. C1036 &v. S.0. NO. NIA PAGE 2 OF 2 (brscerniver covriferea) (DISPOSMON CONIIUNUED) LOWER SKIN REPAIR 1. Remove existing repair (fiberglass) from discrepant area on lower surface. . - 2. Cut filler to size of discrepant area from .016 gauge 202443 per QQ-A-250/5. 3. Fabricate doubler from .020 gauge 2024-0, per DO-A- 250/5 to cove finer. Doubler to overlap filler periphery by 1.50 min. Optional to use 202443, no heat treatment required. 4. Form doubler to match lower skin contour per BAC 5300. Heat treat to -T42 per BAC 5602 or MIL-H-6083. Verify hardness per SRM requirements. 5. Inboard and outboard edges of doubler to be tapered to. .010 min. Care should be taken so the edges of the doubler land mid spaced between existing assembly fasteners. 6. Install doubler using steps 3 through 8 above. 7. Install new panel, filler & doubler using BIP fasteners to complete assembly. Apply sealant to edge of logo fight cut out . and sea all gaps at assembly. 8. Clear Abdine all external clad surfaces per MIL-C-5541, Class 3. hatred Ink When Ibis Steam ORIGINAL! DMILIET.... E EOM MI E7913.11 SDNY_GM_02759859 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246781 EFTA01331244 SDNY_GM_02759860 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246782 EFTA01331245 8- 3-99 4:55 PM ;SUPRA 27 PROGRAM • , BY B. COX DATE 08/02/99 enK131-5frefgrATE EROS cioss DOOM =El ROHR ROHR, INC. ; 5/ 8 PAGE 1 of 4 TITLE Skin Disbond VA545300-1 Us or d rc of chi: infonration ts subject to the Tottrietion on the utle. 3.0 or on the lint• of This document Super 27 I. Discropancy: Tho outer akin of the upper skin assembly of the aft fairing is disbanded and the aft edge of the outer skin has two cracks. See sketch below from ERDS. II. Proposed Disposition: Remove the outer skin of the upper skin assembly and bond on a new outer skin using FM 73 adhesive and BR 127 adhesive primer. The cracks at the aft odge have been reported to be along a previous repair that was filled with a fiberglass patch repair. The fiberglass patch will be removed and replaced with a metallic patch and doubler. All metallic materials will be the same as BP materials. III. Static Analysis: The aft faking is analyzed in section 10 of Reference 1. In section 10 of Reference the substructure has been analyzed to withstand all the aerodynamic loading without using any of the skin as affective. Therefore, this analysis will only investigate the capability of the adhesive to carry the shear stress to the core conservatively assuming that the skin will carry the aerodynamic loading. Strut Stress Analysis (VA-CR154 Rev. C) SDNY_GM_02759861 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246783 EFTA01331246 SDNY_GM_02759862 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246784 EFTA01331247 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 8/ 8 BY B. COX DATE 08/02/99 CHK13 DATE EROS c1036 ❑❑❑1J KKKK ROHR ROHR, INC. PAGE 2 of 4 TITLE. Skin Disband VA545300-1 the or disclosure of this infant-stain ts subject to the restriction on the htle Age ce- 071 the stint page of this clxument The noted adhesive primer is compatible with the adhesive as shown in the excerpt of MIL-HDDK-337 at the end of this analysis. Conservatively assume all the aerodynamic load is reacted by a 1.0-Inch wide by 30 inches long beam that is simply supported between the fuselage and outboard edge. The core shear stress (L) is expressed by f c = V / hb where V is the vertical load being reacted at the supported end h is the centroid distance of the sandwich panel h = t/2 + to/2 + t b is the beam width From page 10.7 of Reference', the aerodynamic pressure (P) on the aft fairing Is .5 psi limit (.75 psi ult). Therefore the ultimate vertical load at one end of a simply supported beam is V = .75(30)(1.0)/2 = 11.25 lbs (ult). From VA545300, t = .016, to = .032 and t, = .30. h = .016/2 + .032/2 + .30 = .324 in f c = V / hb = 11.25 / .324(1.0) = 34.7 lbs/in2 From the certification sheet shown at the end of this analysis, the allowable lap shear for the FM 73 adhesive is 6.523 psi at 75° F. Since there is nu test data readily available for this adhesive system for core bond, a comparison of this adhesive system will be made to EA9649R (RMS 058). From figure 3.3.2 of Reference 2, aluminum core and face sheet with EA9649R adhesive has an allowable of 220 psi for the BP core configuration. Since the lap shear for the repair adhesive is significantly higher than EA9649R (2,838 psi at 75° F), it is reasonable to assume that 34.7 psi core shear Is acceptable for this adhesive system. The repair at the aft end of the faking is acceptable by inspection since the aerodynamic load is very little to nil at this location. IV_ Fatigue Analysis: Repair is acceptable for fatigue strength by inspection since the ultimate margin is high and there are no additional stress concentrations compared to the type design. Meth anIcal Design Allmables (RI IR 85 -013) SDNY_GM_02759863 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246785 EFTA01331248 SDNY_GM_02759864 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246786 EFTA01331249 8- 3-99 4:55 PM • ;SUPER 27 PROGRAM DODO 7/ BY B. COX DATE 08/02/99 DODO PAGE 3 of 4 cHXD DATE ROHR ROHR, INC. Tine Skin DIsbond EROS C1036 VA545300-1 disckme iefenurtton Ie HAdeci A, Me =Waft OA the thic OeMW on dlefintrast Of lath domanant j 44 812D4058K-337 1 Ammmber 2882 I III lit 1 i Ji I Si l € 4 E - . , 1 . i i, . .. 1 11 it 11 ill ... H i 1 1 g g :1 si 4 A i gx 1- I 1 s 1 I i 0 .z g li I- 0 i a # 2 i • -, 1 ; i i 8 i ri n 9. in k ii LIE iss , 1 i . I i 1 — = .-•-•. ≥ i 1 z • SDNYGivl_02759865 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246787 EFTA01331250 SDNY_GM_02759866 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246788 EFTA01331251 8- 3-99 4:55 PM ;SUPER 27 PROGRAM ; 8/8 av E. COX DATE 08/02/99 CHICO ERDS C1036 DATE DOM ROHR ROHR, INC. PAGE 4 of 4 TITLE Skin Disbond VA545300-1 use Qf nisch:num omit InnermatIon s rublect to the rowletIon on the tie. Pluto or on the Bntpax. of document = Willi am's saws Men S R akalg CBRTKrrewom COLD •111400-LARD CITY TO P.O. BOX 1909 LANK Clry YL. 32026 sale TIMC0-1.14102 CITY To =GMAT 90 EAST Zat.,TAZ =Ma 20uTE 19, NOR 1029 OOR ORDER IA= CITY 0023439/001 FL 32026 CUSTOMER DArm SHIpPRD ORDER 690376 06/17/99 pRoDucr BMW* 28CEIPTION . mix 49132 MS00101202 RECOOLMENDED GTORA23-- SWIM AT oR DZZOW rig 7111 .06 rSV 3 • ASR Flaw 12 Nouth0 FROM maw OP BETEMENT 0 negrsoo P --------....... 5 .00 ET7 DEA5 BATOR/OBIT MID BATCH// TIT DATE NUMBER NUMB= fratiljTACMXW (=WITT am 2742-037 aVS.13,1000 300.00 SF in 27402 TOTAL 1. WATCH OTT - sou.00 k TOTAL-, Ise TOTAL OTT 600.00 4.* ISIS CgRTIP2a4 TES DUITNRIA4 AT tD or 0131/e/0252 001052900; To APPLICABLE: MOT= USLOW. • P CROW 3 PR2/092 MOTES AS PART OF CYST2m- TUR-1 WITH TNS OR PIXTFEMX TD Aliti SEE CYTEC FOR I I? trgg DRNMINGS AND BectIFICATIOU3 SPECIFICATTOBg: MW-Ar/32 RSV B. TrAW-2 ran I CLASS 2 FORK 6747a 21132BEaVii OR ALv4EXPTANC72 PBSKIIRM2012 3 a Clic PART XDP2CIVII AE3 cemy TO BR USED mATC22K40 Arcarvt WADI CESTIPICAT/ON. 42928TM:ice.* 76 F LAP 9KRAR [iRs.9. stag, VTBIC:tir .061, .061, 9 /C : .-40224-Nalflal TEST A A 40 180 F 6704. 6622, 6122 Psx 4s3R, 4370, lave. 4260, Rsxs Pai .062 Par OA ADTKORI2RD SIgZIA.TORS e1/224ljl e/$2r 4r lAng7JVcr LZ )1gdng: Pid fre:C eg-C -g SONY_GM_02759867 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246789 EFTA01331252 • SDNY_GM_02759868 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246790 EFTA01331253 Work Order 43736. IfIII US Dopitimontol T importation wwwkoriwa idailalsin00. . MAJOR REPAIR AND ALTERATION"' 'a'. • "'"• " • ' • • (Airframe, Powerplant, Propeller or Appliance) - " " ' ' • • • - • • • . .... .. , Fonn Approved i . , 4. . OMB No. 2120-0020 ' • t •• For FAA Use Only Office Id ratification U % ot . T -; I ap'--.. • • ‘.. • INSTRUCTIONS: Print or type al entries. See FAR 43.9, FAR43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for InstrucUons and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penally not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1858). • • . 1. Aircraft Make / 1 r"'Ir .. Boeing Model •• . . •- • ..'.:. .. ,r: I N 727-31 j• 1• 1 • l • ” I Serial No. •4 : 20115 Nationality and Registration Mark •. N505LS 2. Owner Name (As shown on registration certificate) . j i., :4 Northwest Delaware Corporation. Address (As shown on registration certificate) .., . . , 1105 N Market St . • " Wilmington, DE 19899 3. For FAA Use Only -The data identified herein complies with the applicable airworthiness requirements and Is approved only for the above described aircraft, ••. subject to conformity Inspection by a person authorized In FAR 43, s Ion . 43.7 20fr %deaf / GL-CMH FSDO aura of FAA Ins cler fJetsus Zubia - Unit Identification 5. Type Unit Brake '. "a" h ' . 1‘ I. • Model . . , Seder NO. ' . Repair Alteration AIRFRAME ....... ..................... . Jetta:dee:We Kem 1 above)A.ri ,,,., , , c.o., ,„.....,. ? . . .. . . ... X POWERPLANT • • ' • - ' ••••. • • PROPELLER . . • • "..f P! 'n tr ;,. f ' • ". I . .. i i AI An.. • r.•:•' ":" ' • -rintsx,;• . A' ' 'IV • • APPLIANCE Typo ,. ' ' I • Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Cedificate No. ElectroSonkS • • 4391 International Gateway Port Columbus International Airport Cotentin, OHIO 43219 U. S. Certificated Mechanic Repair Station AE1R005K. Radio Class 1.2 8 3: Instrument Class 3, Accessory Class 3 Limited Altimeter Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair andfix alteration made to the unit(s) Identified in item 4 above and described on the reverse or attachment; 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 hue and correct to the best of my knowledge. Dale April 28, 1999 Signature of Authorized indi • - • • - - • - • •-- - • • - 7. Appro al Rot Service l I - ' 4 Pursuant to the authority given persons specified below, unit id n item 4 was I spelled In the manner presented by the Administrator of the Federal Aviation Administration and is ID APPROVED 0 REJECTED i'.: ' I • BY FAA Fit SLindards InSpectot Manufacturer Inspection Authorization . rtz:: Other (Specify? . .... - • 1 FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group 1• . • I .1 ii. e • • 1 .• Date of Approval or Rejection q -di -"I i - - • - --- Certificate or Designation No. AE1R005K Signature (Authorized Ind hi I . — ' . , r • SDNY_GM_02759869 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024679 I EFTA01331254 NOTICE V. 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 shoots. Identify with aircraft nallonakty and registration mark and date work completed.) • . • 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKEJMODEUDE.SCRIPTION STATION INSTALLATION DATA 622-7203-101 3 Collins VHF-422b Comm 2. The following equipment was Installed In the aircraft. PART NUMBER QTY MAIEJMODEUDESCFtIPTIoN C37c, C38c TSO 450.0 • STATION 822-1115-001 3 Collins VHF-422c Comm C37c, C38c 450.0 523-0772719 3. The above work was accomplished IAW FAA Advisory Circular AC 43.13-16, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. 4. This work has been accomplished under ElectroSonics Work Order 43736. •. 5. Removed existing Collins VHF-422b corn's to accomplish 8.33lan modifications Collins S.8.17. Following modification, reinstalled as VHF-422c and performed a complete operational check. 6. A complete test of the installation of the modified unite has been conducted to confirm that other aircraft systems are free of interference as a result of this Installation. All tests found to be satisfactory. 7. Collins does not specify any new continued airworthiness instructions for the above equipment The owner/operator should consult the Boeing maintenance manuals for general avionics continued airworthiness requirements. 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued airworthiness any time the above equipment Is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded JAW the prescribed loading' Information from the manufacturer. END • 04 ti-Iffil 54 {4 C-2 A4 04 134 I *4 04 storm A3 AeR 2 8 1999 04 1 1A 04 34 4e 0-6 ..,..,s. COIULI10ON . 04 C-9 i C4 I65 1A41 11410 A-9 1,7 - 0-t A-/ 0-3 II-1 2 54 3-0 C-1 C.4 £4 44 . vans, . 7 .,Ni — 31999 . Al r i; 0-41 ii.f. kieto SC , ci,„ ,,„„ commas es 1-7 C-3 I C-4 C-S 311 A40 A-8 .A.7 04 All 0 Additional Sheds Are Attached r • U.S. GPO:1991-0-568-012/40035 SDNY_Glvl_02759870 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246792 EFTA01331255 vo• :•16 r.., : Work Order 43736. 01 MAJOR REPAIR AND ALTERATION''' •• • 1 , Form Appmved . • : r. •Ir • :. OMB No. 2120-0020 For FAA up Only ' US Departrnoce el (Airframe, Powerplant, Propeller or Appliance) , Pampa, Ike foams 440444 4eninfoneen • • • e.' . 27: -. GL07 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43Append& B, and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). ' • .... • " • . .. • • -, • • • • 1. Aircraft Make • 1 1.•1 . Boeing . Model : ' t -4I' , ''..1 :k i. ‘11 . . . 727-31 Serial No. 20115 Natrona fty and Registration Mark • • N505LS 2. owner' Name (As shown on registration certificate) ::., Northwest Delaware Corporation.. . Address (As shown on registration credilicale) . . ..1105 N Ilarket St 111/11n4nOpp, DE19899 ' . .. • 7 . :: : c .. 3. For FAA Use orgy • • I" i :7 -The data Idenktred herein complies with the applicable airworthiness requirements and is approved only for tho above described aircraft,..., .. . ...,, subject to conformity Inspection by a person authorized In FAR 43, section 43.7 / 4 17 4 07 • did/ GL-Clitti FSDO . Dale tura , r Jesus Zubla • • • ' • ;,'• 4; Unit Identification S. WIN Unit . .,,.. Make ,:., .• .: f. •.,'• • r. ol . 4. :. - Model •.;i:i:.:. .StnialNo. Ntecation AIRFRAME . , . . . , • a deSeriberd ill lien, t above). et .17•I7..arr.”, .rr f • • ! , • . ; X POWERPLANT . .,,,gur•r• •••• .4 e 't ".' 1 PROPELLER APPLIANCE Type • .' '.• *. • • •• r• - '• Or • .. . • Manufacturer 6. Conformity Statement A. Agency's Name and Address. : B. Kind of Agency • • • - '' ''• t 1. ' • C. Certificate No. - • EledroSonics 4391 International Gateway Port Columbus International Airport Columbus, OHIO 43219 U. S. Certificated Mechanic Repair Station AE1R005K . Radio Class 1,2 & 3: Instrument Class 3. Accessory Class 3 Limited Altimeter Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I candy that the repair *miler alteration made to the nit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my knondedge. Date April 28, 1999 Signature of Au orized Ind i ; . r.1 , .. ....> .—• / .. i N i i :. *c.-- . 7. Approval or turn o nice : Pursuant to the authority given persons specified below, the un Idea In m4 was inspected in the manner preacnted by the Administrator of the Federal Aviation Administration and is CIAPPROvED 0 REJECT® ?. i ()poi :.) c BY FAA Fl Stanclaxis leSpectof Manufacturer Inspection Authorization Other , Other (S • ..; \ ; FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Lt- I Date of Approval or Rejection Li - 11 - 99 Certificates Designation No. AE1R005K Signa r of Authorized ' ual • -- - - --- - 'BM SDNY_GM_02759871 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246793 EFTA01331256 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 Conformfty 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.) 1. The following equipment was removed from the aircraft: PART NUMBER CITY MAKEJMODELJDESCRIPTION STATION 622-6520-005 2 Collins CTL-22 200.0 622-6520-005 '1 Collins CTL-22 • 259.5 2. The following equipment was Installed In the aircraft. PART NUMBER OTY MAKEJMODEUDESCRIPTID4 ill:) . . STATION. INSTALLATION DATA 822-1120-005 2 Collins CTL-22c • : 822-1120-005 1 Collins CTL-22c I i _ . . • The above work was accomplished IAW FAA Advisory Circular AC 43.13-1B, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. ' • • • ' ' 4. This work has been accomplished under EiectrOSonics Work Order 43736. . 5. Removed existing CTL-22 to accomplish the 8.33KHZ spacing modifications Collins S.B. 31. Following modification, reinstalled units'and performed a complete operational check. 6. A complete test of the installation of the modified unite has been conducted to confirm that other aircraft • systems are free of interference as a result of this installation. All tests found to be satisfactory. 7. Collins does not specify any new continued airworthiness instructions for the above equipment The owner/operator should consult the Boeing maintenance mahuais for general avionics continued airworthiness requirements. 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued ; airworthiness any time the above equipment is removed and/or repaired and reinstalled. I . 9. . The aircraft Weight and Balance is unchanged and Equipment List has been amended. _ . • 10. The aircraft must be loaded lAW the prescribed loading information from the manufacturer. END C37c, C38c 200.0 523-0072719 C37c, C38c, 259.5 2.1.p 34 C-1I C.4 04 I 1S-0 I A-2 A-1 6 1 ctcf RI 0 A-3 Alit( 28099 A.4 0 . le5 0 ) A-7 ii, o J ..,„ 1500 COLO:ABU 014 0 ) C-3 I C-4 I C411.41 I A.I0 1.-9 0 1 A4 0-1 41-1 2 S•A S•0 C-1 C-2 A4 0-2 A-2 0-9 - SCW* .A.3 :•iiii ''' 3 ' A .- • GIN SDO• • •FOill. A ,, 4.. c.-a e-e, C4 A4I -1.-10ii.-9 it' , 0-7 1 04 i . • . O Additional Sheets Are Attached . U.S. GP0:1991.0-568-012140035 SDNY_GM_02759872 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246794 EFTA01331257 r MAJOR REPAIR AND ALTERATION Form Apprrsed OMB No. 2120-0020 uS OeParencs (Airframe, Powerplant, Propeller, or Appliance) For FM Use Only d Transportaion Federal Aviation AdmInIstreUen Oftioe Identification .e44. Asto-o INSTRUCTIONS: Print or type all entries. See FAR 43,9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disco:Won of this foot This form is required by lay (49 U.S.C. 1421). Failure to report can mutt in a civi penalty not to exceed $1,000 for each such volition (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Mom Boeing 72741 Serial No. 20115 Nationality and Registration Mark N505LS 2. Owner Name (As shown on regStra0an certificate) Northwest Delaware Corp. Address (As 5/10W77 on registration cettiatte) 1105 N Pdaltit atrii .. WilmIngin, 98 1. 4 3. For FAA Use Only Alki 1 0 1C93 CM-DALLAS SW05 4. Unit Identification 5. Type Unit Make Mo0el Serial No. Repel( Altera= AIRFRAME described in item 1 X X (As above) POWERPLANT PROPELLER • APPLIANCE Type Manufacturer 6. Conformity Statement A. Agencys Name and Address B. Kind ofAgency C. Certificate No. Associated Air Center [ADDRESS REDACTED] Dallas, Texas 75220 V.S. Castrated methane TX2Ft203L Airframe Class 3 & 4 Radio Class 1, 2 & 3 Foreign Certificated mechanic X C,ertifcated Repair Staten Menvfackuer a i certify that the repair an/or alteration made to the unit(s) Identified in hem 4 above and described on the reverse or attachments hereto have been made in accords= with the requirements of Pal 43 of the U.S. Federal Aviation Regulatory% and that the information furnished herein is true and correct to the best <limy knomedge. Date 8/4/98 Signature of Authorized IndMdual ›rionjA 1141 O °— 7. Approval for Return to Service Pursuant to the authoritygiven persons specified bele", the unit Identified in item 4 a inspected m the reamer prescated by the Administrator of the Federal Aviation Administration and is ®APPROVED 0 REJECTED BY FAA Ft Standards Inspector Manufacturer insponionAuthorizarlon Other (Specify) FM Designee x Rent Station Person Apfund ly Transpal Canadian Ainvalhmess Group Date of Aquae' a Rejection 814/98 Certificate or Designate No. TX2R203L Signature cfAuthatted IndiAdu.al 71i,a- 4/ 40 141.4rdler—• orrn 337 (1248) SDNY_GM_02759873 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246795 EFTA01331258 NOTICE Weight and balance oropereting 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 al more space is require; attach addoxial sheet& meow wen aircraft nationality and leglerallco mark and Ode work completed.) Aircraft: Boeing 727-31 Registration #: N505LS Serial #: 20115 Aircraft Total Time: 31,675.6 Aircraft Total Cycles: 21,567 August 4, 1998 The following alteration was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Mode "S" Transponder ICAO Code Strapping Change in accordance with AAC Drawing 1565-001 Rev A dated July 28, 1998, 8110-3 approved by D.E.R. SW-997, David A. ICimbrell July 29, 1998. The following repair was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Repair - L/H Horizontal Stabilizer Trailing Edge Beam at Elevator Station 156 in accordance with AAC Repair Drawing 1565-002 dated July --, 1998, 8110-3 approved by D.E.R. SW-810, Robert IV Manashi August 4, 1998. **************************END************************** K Additional Sheets Am Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60167 SDNY_GM_02759874 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246796 EFTA01331259 DAK-98-089 OrlArnewr OF TautaPORTATION FEDERAL AVIATioN ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JULY 29, 1998 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE ( 41Irplano, Radio, Holleoptist, eta.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER DALLAS, TEXAS LIST OF DATA IDENTIFICATION 1TTLE 1565-001 REV. A 07/28198 MODE S TRANSPONDER ICAO CODE STRAPPING CHANGE ' I ... NOTES: TC DATA SHEET A3WE. ELECTRICAL DESIGN ASPECTS OF THIS THIS APPROVAL APPLICABLE TO B727-31 THIS 8110-3 FORM IS IN SUPPORT OF FAA : • iikl. DATA IS APPROVED. Sits; 20115 ONLY. FORM 337. PURPOSE OF DATA TO SUPPORT THE AVIONICS/ELECTRICAL MODIFICATIONS. APPLICABLE REQUIREMENTS (List specific sactrons) FAR 25.1301 (a)(b)(c) CERTIFICATION - Under authority appointment under Part 183 of 0 have vested by direction of the Administrator and In accordance with the Federal Aviation Regulations, data listed above and on attached been examined In accordance with established procedures and found Regulations. approval of these data these data conditions and limitations of sheets numbered to comply with applicable requirements of the Federal Aviation M Recommend I OM Therefore Approve SIGNA\URE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE/Si DESIGNATION NUMBER(S) CLASSIFICATION(S) DAVID A. KIMBRELL 7 SW-997 AVIONICS/ELECTRICAL i i a 7 -1:71/../ SYSTEMS ylo ... /L.-/e2ezber FAA Form 8110-3 0140) s. ‘FTIFS ',Remus Ecmom( COMPUTER GENERATED) GPO 1,01413 SDNY_Gtv1_02 759875 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246797 EFTA01331260 SDNY_GM_02759876 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246798 EFTA01331261 AUG-04-1999 10:39 ASSOC AIR [PHONE REDACTED] [PHONE REDACTED] P.01 U.S.OEPARTmENTOFTPANsPoRTATION GEDERALAVIATIONADMINI8TRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE #98421 AtIO03T Oil, 1992 _ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARE 307.1NO MODEL NO. 727-31 TYPE (seats. was en) AIRPLANE (N5001.3) NAME OF APPLICANT A280CIATZI1 Alit - CENTER LIST OF DATA IDENTIFICATION TITLE ASIOCIATrD ALA Car= DUNI= NO. 1565-002 ASV. "IR', DATIO 07-29-1928 REPAIR - L/H HatazzoNTAL STAB:LIZ= T/t OPFER SIM - SLEW STA 136. (Slat 1, 2 AND 3 or 3). 140725: 1. THE STRUCTURAL A3PiCTS ONLY Or TEE ABOVE LISIID RATA ARP arrimmoo tronasn. suss APPROVAL 28 roil ens ENGIUMMIro DESZON DATA ONLY. 2. THIS APPROVAL 13 VA.= ONLY FOR HOEING MODAL NO. 727-31, AIRCRAFT 2/N 20125 AND Is ism= IN St719PCCRT Or A MAJOR REPAIR Or THY SUBJECT AIRCRAST. PURPOSE OF DATA IN SUPPORT OF A WAJOA AMUR ON HOEING )DOLL NO. 727-31, AERCFATI 3/N 20115. APPLICAELE REQUIREMENTS as %vox sae CAR 41).200 (a) , (b) , 41).201 (11) , (b) , (e) , tb.202, 4b.300, tb.301, 4b. 302, 417.903, 4b.304 (al , (b), 4b.308 (a) , (b), (d) • CERTIFICATION - Under authority vested by &U MW of limitations of appointment under Part 183 of Ma Federal sheets numbered ,J00C0000000000CCOOL have been found to comply w*h appliCable requirnmentS of the Federal the AdmIntStrator and in accordance Aviation Regulations, data listed examined in accordance with Aviation Reaulelions. data with conditions anti above and on attached establithad procachuta and INI Recommend Approval et these I (WI) THEREFORE o Approve these data aloNtrauRgiinoro ENGINEERINGREe 6EWATIMS) 0664NATIONNUMWM) cutiSSIFICATION(8) a t 8W-910 ariUnEvara Rama KAI i. ze 0 /.7C)10.1ZUZINS1 PASYLOP1 ISIM0N c_ri A -• r)e.e5 . TOTAL P.01 SONv_GIvi_02759877 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246799 EFTA01331262 SDNY_GM_02759878 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024680() EFTA01331263 • • 00...••••1 OP IIIMMOSTA.M= "aal...1•IMMUIONI STANDARD AIRY/00711MM C10111FICA72 • ••••••••••••./0 •••• =ten.. Weee•••• MOM BOUM 727-31 20115 122112PORS •••••••Pkir..0 0.10••••••4 B 07-23-90 cum FAA form 81004 oah T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00246801 EFTA01331264 SONY_GM_02759880 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA _00246802 EFTA01331265 • MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) of Transpartation Federal Aviation Administration FOOT, Approved Om% or se nly PAAGONLLAS A., MO; r \ (A/C- INSTRUCTIONS: Print or type ell entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of this form. This form is required bylaw (49 U.S.C. 1421). Failure to report can result in a cm penalty not to taceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Boeing Model 72741 SCSI No. 20115 Nationality and Registration Mark N500LS 2. Owner Name (As shown on regisfration certificate) Northwest Delaware Corp. Address (As shown on registratbr: cofttecate) 1105 N Market St. Wilmington, DE 19899 3. For FAA Use Only 1. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteralion AIRFRAME described in item 1 X X (As above) POVVERPLAfT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A Agencys Name and Address B. Kind of Agency C..Certificree Nor- • Associated Air Center [ADDRESS REDACTED] Dallas, Texas 75220 U.S. Certificated Mechanic •• TX2R203L., .. • • • Class 3 & 4 Foreign Certificated Mechanic X Certificates Repair Stason Manufacturer D. I certify that the roper and/or alteration made to the wigs) identified in item 4 above and described on the remise or attachments hereto have been made In accordance with the requirements ci Part 43 of the U.S. Federal Aviation Regulations and that the inforrrigion furnished herein is true and correct to the test of my knowledge. Date 812197 Sig of Authorized kern OW . fi 7. Approval for Re Service Pursuant o the authoritygiven persons specified below, the unit identified tern 4 was inspected in the manner prescrited by the Administrator of the Federal Aviation Administrtmen and is (J APPROVED QREJECTED BY FAA FN. Standards Inspector Manufacturer Inspection Authortzation Other (Specify) FAA Detente X Repair Station Person Approved hy Transport Canadian Akworthmess Group Dale of Approval a Relection 8/2/97 - - - --- Certificate or Designation Na TX2R203L Signalise Individual S iore. .e_____ SDNY_GIvl_02759881 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246803 EFTA01331266 NOTICE • Weight and balance or operiling limitation changes shall be entered in the appropriate aitraft record. An alteration must be compatible with all previous alterations to assure continued contort:lily with the applicable airworthiness requirements. 8. Description of Work Accomplished Itl mere spice is rtio.iised attach adational sheets kin** with aitaart amount), and regiStatiOn mark and date work corn#eted) Aircraft: Boeing: 727-31 Registration #: N500LS Serial #: 20115 Aircraft Total Time:31,471.2 Aircraft Total Cycles: 21,468 August 2, 1997 The following work was accomplished at Associated Air Center, Dallas, Texas under Work Order 1476. 1)Repair - Airstair Door Actuator Attach Clip in accordance with AAC Repair Drawing 1476-001 IR dated July 16, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 2) Repair - #1 & #3 Pylon Corrosion on Forward Engine Mounts in accordance with AAC Repair Drawing 1476-002 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW- 916, Jim Martin July 22, 1997. 3) Repair - #8 Leading Edge Slat Crack at 1/B Slat Guide in accordance with AAC Repair Drawing 1476-003 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 4) Repair - Corrosion on R/H Wing Upper Surface at WBL 70.5 Between Str. 1 - 14 in accordance with AAC Repair Drawing 1476-004 IR dated July 21, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 5) Repair - Floor Beam BS 600, RBL 25 Figure $ Hole in accordance with AAC Repair Drawing 1476-005 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 6) Repair - Aft B/B Door Interior Structure Cracked in accordance with AAC Repair Drawing 1476-006 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22. 1997. 7) Repair - Wing to Body Fairing Damaged Dome Nut in accordance with AAC Repair Drawing 1476-007 IR dated July 25, 1997. 8110-3 approved by D.E.R. SW-916, Jim Martin July 25, 1997. 8) Repair of Center Engine Exhaust Nozzle in accordance with Rohr, Inc. Engineering Repair Data Sheet No. C0625 Rev. A dated July 23, 1007, 8110-3 approved by D.E.R.(s) NM-2731, Jeffrey D. Shutrump for Structures, NM-738, Tony Bradlaugh-Dredge for Powerplant and NM-2182, Michael August for Special Administrative July 23, 1997 and AAC Repair Drawing 1476-008 IR dated July 25. 1997. 8110-3 approved by D.E.R. SW- 916, Jim Martin July 25. 1997. S eAddsonal SIvrais Are AlleNte0 U.S. GOVERNMENT PRINTING OFFICE: 1992.769-012/80157 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SDNY 027591382 15, and 17 EFTA 00246804 EFTA01331267 Aircraft: Boeing: 727-31 Registration #: N500LS Serial #: 20115 Aircraft Total Time:31,471.2 Aircraft Total Cycles: 21,468 August 2, 1997 9) Autopilot Interface Unit Modification in accordance with AAC Drawing 97-2211- 210 IR dated July 28, 1997, 8110-3 approved by D.E.R. SW-880, John W. Goswick July 28, 1997. END SDNYGlvl_02759883 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246805 EFTA01331268 SDNY_GM_02759884 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246806 EFTA01331269 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22J97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Alrotene, Radio, Helicopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-001 4-- REV. IR 7-16-97 REPAIR - AIRSTAIR DOOR ACTUATOR ATTACH CLIP THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 ..303 .307(c) .300 .304 CERTIFICATION • Under authority vested under Part 183 of the Federal Medico Regulations, exemined In accordance lab established procedures by direction of the Administrator and In accordance data listed atom and al attached sheets and found to comply vAib applicable Recommend approval of these data Approve these data with conditions and britallons of appoirtment numbered el oe oC have been requirements of the Federal Aviation Regulations. MI I ) Therefore .00 I= SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 57.: . ._..., JIM MARTIN SW-916 STRUCTURES _.. _ GPO 901-613 SDNY_GM_027598B5 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246807 EFTA01331270 SDNY_GM_0275.386 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246808 EFTA01331271 ARC.11.IS1 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane. Radio. Helicopter. etc.) AIRPLANE NAME OF APPUCANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-0021" REV. IR 7-17-97 REPAIR - # 1 & # 3 PYLON CORROSION ON FWD ENGINE MOUNTS THE ABOVE DATA IS APPROVED ONLY. FOR AIRCRAFT S/N INSPECTION FOR THE STRUCTURAL DESIGN ASPECT 20115 PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrate' and In accordance with conditions and ambitions of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered te. se 41 have been panned In accordance se established procedures and found to comply with applicable requirements lathe Federal Aviation Regulations. Recommend approval of these data BEI I Therefore Ve4 rXi Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) 7r -76 JIM MARTIN SW-916 STRUCTURES _.. _ ...._ _ ... _ GPO 901.813 SDNYGIvl_02759887 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246809 EFTA01331272 SDNY_GM_02759888 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246810 EFTA01331273 AitiC•17. ISE U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-00317 REV. IR 7-17-97 REPAIR - # 8 UE SLAT CRACK AT I/B SLAT GUIDE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECT\ ON PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .308 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance under Part 183 of the Fedora/ Aviation Regulations, data listed above and on attached sheets comined in accordance wilts established procedures and found to comply vieh applicable (=Recommend approval of these data I 20) Therefore Approve these data with conditions and Imitalims of appointment numbered re 44. re have been requirements of the Federal Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 7 : JIM MARTIN SW-916 STRUCTURES _.. _ can (11-70 EDITION) GPO 9014313 SDNY_GM_02759889 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246811 EFTA01331274 SDNY_GM_02759890 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246812 EFTA01331275 RAC•c11.15 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane. Radio, Hetcopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-004 L." REV. IR 7-21-97 REPAIR CORROSION ON R/H WING UPPER SURFACE AT WBL 70.5 BETWEEN STIR. 1 - 14 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INS? ECT ION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 -.303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Reptile/king, examined in accordance with established by direction of the AdmInkstrator and In accordance data listed above and on attached sheets procedures and found to comply vett appdcable Recommend approval of these data Approve these dela with conditions and riflery; of appointment numbered SC. at re( have been requirements of the Federal Aviation Regulatiors. NM I Therefore (Wic) II 9 SIONATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) " -e JIM MARTIN SW-916 STRUCTURES -- - - -- -- - -- - GPO 901413 SDNYGlvl02759891 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 3 EFTA01331276 SDNY_GM_02759892 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246814 EFTA01331277 ARc•ii. lac] U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1478-005v REV. IR 7-22-97 • REPORT NO. 1478-005 (.--- REV. IR 7-22-97 REPAIR - FLOOR BEAM STA. 600 RBL 25 FIGURE 8 HOLE STRUCTURAL SUBSTANTIATION - REPAIR - FLOOR BEAM STA. 600 RBL 25 FIGURE 8 HOLE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL ONLY. FOR AIRCRAFT S/N 20115 INSPE CTION DESIGN ASPECT PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REOUIREMENTS (Ust swift sections) CAR 4b.200 .301 .305 .201 .302 .308 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Pad 183 of the Federal Aviation Regulations, ermined h accordance %Nth estabEshed by direction of the Admiresbator and in accordance data fisted above and on attached sheets procedures and found to complyWM applicable Recommend approval of these data Approve these data wilh cations and limeations of appointment numbered are ex" al have been requirements of the Federal Aviation Regulations. MN () I Therefore 9,0 I l SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) f.1 7e JIM MARTIN SW-918 STRUCTURES arm 81103 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901413 SDNYGIvl_02759893 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246815 EFTA01331278 SDNY_GM_02759894 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 6 EFTA01331279 lifiC•il• Ito I U.S. DEPARTMENT OF TRANSPORTATION • FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Ratio Helicopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476.006 4-- REV. IR 7-22-97 REPORT NO. 1476-006 4, REV. IR 7-22-97 REPAIR - AFT B/B DOOR INTERIOR STRUCTURE CRACKED SRUCTURAL SUBSTANTIATION - REPAIR - AFT B/B DOOR INTERIOR STRUCTURE CRACKED THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List spectfto sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 .303 .307(c) .300 .304 CERTIFICATION - Under authorfty vested under Part 183 of the Federal Aviation Regulations, examined In accordance with established by direction of the Administrator and In accordance data listed above and on attached sheets procedures and found to comply %Oh applicable Recommend approval of these data Approve these data web conditions and ImIted:res of appointment numbered 60/ ree d have been requirements able Federal Aviation Regulations. No I 0 Therefore 0 a) SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) g 7.—te JIM MARTIN SW-916 STRUCTURES orm 81103 (1 • EDITION) GPO 901-613 SDNYGivl_02759895 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246817 EFTA01331280 SDNY_GM_02759896 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 8 EFTA01331281 fIRC.97, IL. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/25/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio. Helicopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-007 •-• REV. IR 7-25-97 .---- REPAIR - WING TO BODY FAIRING DAMAGED DOME NUT THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust specific sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authonly vested under Pea 183 of the Federal Aviation Regulations, earnined in accordance vats established by drecdon of the Administrator and In accordance data listed above and on attached sheets procedures and found to comply vith applicable Recommend approval of these data Approve these data HIM anditions and limitations of appoinbnent numbered o 44 mr- harm been requirements of the Federal Aviation Regulations. MI I Therefore Opfi; Ui SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTAT1VE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) f -al JIM MARTIN SW-916 STRUCTURES FAA Farm 8110-3 (11-70 SUPERSEDES PREVIOUS EDMON) GPO 901413 SDNYGlvl_02759897 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246819 EFTA01331282 SDNY_GM_02759898 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246820 EFTA01331283 RAC-J(11. 1CA) . U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/25/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Ain:sane Radio. Helicopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-008 (---- REV. IR 7-25-97 REPAIR - OUTER SKIN NOZZLE CENTER ENGINE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 Mic l f^, , , ;,..- c-• PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust speak sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established by direction of the Adminislratce and In accordanoe dab fisted above and on stincned sheets procedures and found to comply all applicable Reconmend approval of these date Amon, dust data with conditions and lirnitathns of appohtment numbered De t‘ d have been requirements of the Federal Aviation Regulations. imi I We) Therefore 12g) SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES FAA Fonn 8110-3 (11.70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 SDNYGtvl02759899 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246821 EFTA01331284 SDNY_GM_02759900 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246822 EFTA01331285 JWG 97.084 U.S. DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JULY 28, 1997 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. I 727-100 TYPE (Airplane. Nolan. Helicopter. etc.; Airplane NAME OF APPLICANT Associated Air Center UST OF DATA IDENTIFICATION TITLE Drawing No. Autopilot Interface Unit Modification W/D. ----------------------- Note: (1) The above data is approved for the electrical/ electronic avionics design aspects only. 97-2211-210 ,---e" Rev -- Date: 7/28/97 and PURPOSE OF DATA To Support Major Alteration on S/N 20115 Only. APPLICABLE REQUIRLAIhNTS (Dot specific sections) FAR 25.869(a), 25.1301, 25.1431(c). CERTIFICATION - Under of appointment under Part 183 X X X X X X X XX have been authority vested by direction of the administrator and in accordance with conditions and limitations of the Federal Aviation Regulations, data listed above and on attached sheets numbered examined in accordance with established procedures and (mind to comply with applicable Regulation,. Recommend approval of these data Approve these data requirement, 01 the Federal Aviation I (MIS) Therefore tEl sionATune(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMSER(S) CLASSIFICATIONS) 94 -rA r—L"—C SW-880 Systems & Equipment ' John W. Goswick SDNY_Givl_02759901 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246523 EFTA01331286 SDNY_GM_02759902 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246824 EFTA01331287 7-23-S7 3:19 PM ;SUPER 27 PROGRAM -• • [PHONE REDACTED];e 2/ 5 U.8. DEPARTMENT OF TRANSPORTATION PEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE July 23, 1997 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Altplam, AMA liellcopor. et) Airplane NAME OP APPLICANT Rohr, InC. LIST OF DATA IDENTIFICATION TITLE Rohr Inc., EROS C0825 l/ Revision A dated July 23, 1997 • Engineering Repair Data Sheet INSPEU n TI CIN PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS gmrspeotosectody (1)(3) FAR 25.301 (2)(3) FAR 25.805 (a) (1)(3) FAR 25.303 (2)(3) FAR 25.609 (1)(3) FAR 25.305 (a)(b) CERTIFICATION — Under authority appointment under part 153 of NONE have been vested by direction of the Administrator and In accordance vAth conditions and limitations of the Federal Aviation Regulations, data listed aDove and on attached sheets numbered examined In accordance with established procedures and found to comply with applicable Regulations. Recommend approval of these data Approve those data requirements of the Federal Aviation I (We) Therefore SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTATIVES DESIGNATION NUMBER(S) GLASSIFICATION(S) (1) Jeffrey D. Shutrump NM-2731 structures ifite (2) Tony Bredlaugh-Dredge NM-738 Powerplant (3) Michael August NM-2182 Special Administrative to O•Mfatee br RotV, a a, SDNY_GM_02759903 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246825 EFTA01331288 SDNY_GM_02759904 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246826 EFTA01331289 .4 44,0•44404.440144.4 INIPAMOR C4,14416•04./10 ,4—MPOW. .4.4440.114.114:44 STANDARD PiRWORTHINEES CERTIFICATE 44.0414044.44001.014. 4. 4 G41,40044 05001.3 DODD 727-31 20115 ?DISPORT 4.4 ROa • ,...9•Nocagor.• tll rI•reaut) 07-23-90 LEE R. TR 7 0107 mn ra DM .....04 ./I 4M/P 44, Cm, to. 4144.4.0014= 4.14:4414[0.4444424* FAA Ferro D00.2 ow, o.., ••••••• SONY_GM_0275990.5 TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA _00246827 EFTA01331290 i SDNY_GM_02759906 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00246828 EFTA01331291 • ge • MAJOR REPAIR AND ALTERATION CS Onrcsttrco Powerplant, Propeller, or Appliance) • Form Approved OMB No. 2120-0020 For FAA Use Only Office(dentification ,4 ?7 CA 0 a sovccomon (Airframe, hews sewn= . e areUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequ nt revision thereof) torinstructions and disposition of this form.This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Modes 727-100RE Serial No. 20115 Nationality and Registration Mark NSOOLS 2. Owner Name (As shown on registration certificate) NORTHWEST DELAWARE CORPORATION Address (As shown on registration certificate) Mig ign i,DE. 1;899; 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 r PROPOSER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. THE LIMITED INC. 4387 INTERNATIONAL GATEWAY COLUMBUS, OHIO 43219 X U.S. Certificated Mechanic /A301541619 Foreign Certificated Mechanic cenificated hermit Station Manufacturer 0. I certify that the repairand/or alteration made to the un't(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 rAdigion Regulations and that the information furnished herein is true and correct to theaat.ot my. nowledge. . 9:1) 1.11.‘ Date L>, I.- ( s March 11, 1998 ! Signature • 'z IA al . . . Richard R Cady II 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is • GI APPROVED 0 E TED FAA Fit. Standards Inspector Manufacturer X • Inspection Authorization er (Specify) 40 FAA Designee Repair Station Person Approved Cana by Transport -worthiness Grou Date of Approval or Rejection Certificate or Designation No. Si natu of onzed I vld..al • March 13, 1998 IA2185934 . T.W. RITCHIE FAA Form 337 riz-sei SDNYGivi02759907 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246829 EFTA01331292 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirement& 8. Description of Work Accomplished (If more space is required, &trash addltionatsheals. Identify with aircraft nationality and registration mark and date work completed.) REMOVED THE FOLLOWING EQUIPMENT: 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 7000700-962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STATIC SOURCE ERROR CORRECTION CURVE INSTALLED IN ACCORDANCE WITH AES DRAWING .LIST NO. 97-727-500 REV. B, DATED NOVEMBER 3, 1997 PER SUPPLEMENTAL TYPE• CERTIFICATE ST09364sc. FAA APPROVED FLIGHT MANUAL SUPPLEMENT, DATED OCTOBER 27, 1997 IS REQUIRED AND INSTALLED ON THIS AIRCRAFT. WEIGHT S BALANCE NEGLIBLE. COPY OF STC ST09364SC AND MASTER DRAWING LIST ATTACHED. CONTINUED MAINTENANCE PRACTICES INCLUDED IN THIS PACKAGE. END Additional Sheets Are Attached •U.SGsemeet0665Cnalsa035 SDNY_GM_02759908 • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246830 EFTA01331293 THE LIMITED UR0859 RECEIVED U.S.IDepartment of Ttansportation Federal Aviation Admlnistradon -• - MAJOR REPAIR AND ALTERATION (Aidrame, Powerplant,Propeller, or Appliance) Form O AP M8 Int .05;1996 For -AA Use Only °"grIA.001)2k141iiki.S SWO5 /Ctr..- C- INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9.1 lor subsequent revision thereol) for !omwallens and disposition of this form. This report Is required by law (49 U.S.C. 14211. Faiture to repen con result Ina dvil i penalty not to exceed 01,000 for each toch violatIon (Station 901 Federal Aviation Act of 1958). _ . .4. 1. Aircraft Make Boeis g Model 727-81 Seniel No. 20115 NS/3~4y end Registration Mark N50015 2. owner Name (As shown on registration conilicate) Northwest Datawire Corp Address OM shown on registration certilicatot 1105 N. Market St Nilmington, DE 19899 3. For FAA Lise Only 4. Unit Identifieadon 5. T pe Unit Makt. Model &dal No. Repelt' Altaration ~FRAME -------- -----(As descnbad In Item 1 above) POWERPLANT PRATT & WHITNEY Turbo Fan Engine JT8C-7B P654373 X PROPELLER APPLIANCE rype Manufacturier 6. Confornity Statement A. Agenty's Name and Address 8. Kind of Agency C. Certiflcate No. Greenwich Air Services - Texas, LP [ADDRESS REDACTED] Dallas, Texas 75235 U.S. Cartificated Mechanic • RA1R445K . Powerplant Class 3 Accessory Class 1,2 and 3 Foreign Certineated Mechanic X Cenificated Repair Station . Manufacturer D. I certily that the maak endnor alteration made to the unit( ) identified in Item 4 above and described on the reverse or attachments hereto have been made in accordence with the rei:lui:amens of Part 43 of the U.S. Federal Aviation Regulations and that the Informatica furnIshed heroin is true and correct to the best of my knowledge. Date /c) - 3 .0-7 Sin I, Authorized Individual 24,47,1--- 7. APoroval Return To Service Pursuant to the authorlty given persons specified be w, the unit identified in item 4 was inspected in the menner prescribed by the Administrator of the Federal Aviation Administration and is Exil APPROVED n REJECTED BV MA Rh st-evas mouw« aterstessw asmoren Aulhonvelen orer Iltmayl , MA gedane* x filIPM• §. uilen ~os isoweed °T Truien Canada Afrwereeent Onno Dato of Approval or Rejection / O-30 -fr i.‘ Certilicate or Designation No. Signa f Authothed in ividsal RA1 R445K .---- de' • SDNY_GM_02 759909 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024683I EFTA01331294 ZE89N:00- Vin LT Pue 'ST 'OT '6 '8 7. SHdV2IDV2:1Vd 8302:10 3ALLD31021d 011J3f8fS 01.66SLZ01^/0ANOS 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 Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) • Engine S/N P654373 was removed due to "SERVICE BULLETIN COMPLIANCE." • Engine was disaSsembled, inspected, repaired as required in accordance with Pratt & Whitney JT8D Engine Manual (P/N 481672), and Greenwich Specialized Unit Repair Workscope which are data approved by the Administrator. Inspected/reinstalled Combustion Chamber Outer Case P/N 542155, S/N 243, T.T. & T.C. Unknown, in accordance with P&W Alert S/B 6228, Part I and Part II and AD's 87.11.07 & 95.08-15. Ps4/Drain bosses require reinspection within 6000 cycles and at each Engine shop visit. Rear flange requires reinspection within 12000 cycles and at each Engine shop visit. Case meets inspection requirements of Part III of P&W AS8 6228. Continue timed combustion chambers. Complied with P&W Alert S/B 5729R2 and AD 87-14-01R1; immersion ultrasonic inspect C2 fan blades. Complied with P&W Alert 6038R5 and AD 94-20-01; corrosion inspect high pressure compressor disks. Complied with Pratt & Whitney Alert 5/8 6196R5; #5 bearing seal assembly. Improved oil return & compartment sealing configuration. Complied with P&W Alert S/B 6110 and Alert S/B 6131, AD 94-20.08. This terminates -reinspection requirements for P&W Alert S/B 5913R6, AD 93-06-05. Engine was preserved forshort term storage IAW Pratt & Whitney JT8D Engine Manual (P/N 481672). Engine was subjected to a test run; a post-test borescope inspection was performed and Engine was accepted as serviceable. Engine TT: 32939.0, TC: 22557, TSR 00:00 CSR 0000. Pertinent details of this repair are on file at this Agency under W.O. UR0859 .2 n ADDITIONAL SHEETS ARE ATTACHED FAA AC 72-4906 EFTA01331295 Og, MAJOR REPAIR AND ALTERATION us Demmer* ClbetzgaMen (Airframe, Powerplant, Propeller, or Appliance) Iredsoviitelellat AdmitMilan Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification SO.FSDO-°9 INSTRUCTIONS: Print or typeall entries. See FAR 43.9, FAR 43Appendix B.endAC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49U.S.C. 1421). Fadure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 8727-31 Serial No. 20115 Nationality and Registration Mark N500LS 2. Ovmer Name (As show,, on registration certificate) Northwest Delaware Corporation Address As shown on registration certificate) 1105 N. Market Street Wilmington, DE 19899 3. For FAA Use Only 4. Unll Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME *(As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. ST Mobile Aerospace Engineering, Inc 2100 9th. Street, Brookley Complex Mobile, AL 36615 U.S. COMM:Sled Mediank MZAR013L Airframe Limited Foreign Cenifiatee mechanic X Calif kated Repair StallOn Manufacturer D. I certify that the repairand/or alteration made tothe un t(s) identified in item4 aboveanddescribed on the reverse orattachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my knowledge. Date November 25, 1995 Signature of Authorized IndivId Clarence Spencer im.......______ 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is SO APPROVED 0 REJECTED BY FAA Rt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection November 25, 1995 Certificate or Designation No. MZAR013L Signature of Authorized Individual ---.. Christopher J. Hil • FAA Form 337'1245) SDNY_GM_02759911 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246833 EFTA01331296 • 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.) Installed DeVore Aviation Corporation tail flood light installation in engine pylons in accordance with De Vore STC ST09113AC dated 26 May 95. DeVore Top Drawing List #72700003DL Rev "A" dated 5-30-95. Installed Valsan Wmglet Modification in Accordance with Valsan Master Drawing List #VA000007, Rev "N" dated 17 April 1995. STC SA59381%1M. Aircraft Inboard and Outboard Aft Flaps and Ailerons rigged to endure fimctionality and conformity. Aircraft weighed after modification. Weight and balance data provided to customer. Aircraft total time = 31,197 hours. Total cycles = 21,345. END'. O Additional Sheets Are Attached •USGPO:199OO4011-012/400O4 SDNY_GNI_02759912 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246834 EFTA01331297 O AND ALTERATION Fs.", APPrOved OMB No. 2,20.0020 MAJOR REPAIR vlosemen Fot FAA the endy Olicreasso. (Airframe, Powerplanl, Propeller, or Appliance) 11141•6111fill•••• iilleil•MISI, 15472 ,11:flo i INSTRUCTIOIRt Plint CWIY00 tutentriet Sn FAR OA FAR 43 Append.. B. and AC43.9-1 (Ortubsequient nnision thereof) tor instroctkons Ona 014.01.06on ol Mai loin. T ho rop0,11•18.410nln bylaw (401.1.S.C. 14213 Fe luntIO report Canmolt i • cml palony not io oliaila $1.003 kw Mól SKI% allabOa (Section 901 Faleni Aelobon Act ol )9:43 T. lee eaCiA/6- Yodel 237.r7 - leb Seed Mt r; o H s••••••• Nosionety end Reoisliotion Mark A/52 , 04. 5 2. Oa Nas (As *Own on tivairgn cartitIcS) 4 4" ha tata /401..D/445. . . , - Si (As shown on regettrollon catraltalit) r.O. ?ok 1138 aii.sverifinv 31e. /9A3 S. For MA URI Olik - • . '..' ":. •:;•4\3, .N.3.;4-34 N:O ..tib4.!`7':•. • ' , . . 3,4 A ','. ,, \..r,e tr.'34. •.• St .7!, ...r. : t .. . 3. • ' • — 4. llell Idiellsellso • '''' ' e. 'TYPO Unit Melee Rend Mention . —.., • (As in ban I 4000VJ AdiFRAUE tbactited '.. . • POWERMANT r • -.1.4. . :-.*„"..- , ..... • PROPELS r !... .\".. , -`2."09,16 ...C!.:., • . - MMMCI 9brs . epOtt iOret' /IYA, 4406 OW 49 V (ATA 160 '1106 173 e ? X la ri lryea CCOnlornilly 414ffileard A. Agency* Moe and Adding * . t Kind of Arony C. Condlcolo No. -gr Zatirefaisti . • • us c........ mowne ,...............c . 1 :V3e2 s/a.. ........... s.. .2,7 ..) Je 593 5 ari-4393uś ofĄ0 4132 /t ..,..,.,,„. D. lennon‚ aha %hemom ondier alletetIon made w the tainl(s)idonlilOP3 him boon ~Je in occortlance 4/41. the niqUinlonntsb Ismonvd Iwon 4 eve ona correct to UV 0•01 01 toy In ItOfn 4 •00•• woO °flatbed on OW rOvIna• of anocnnwonungrolo ol Pen 43 of de U.S. Popersi Anaben asouleeone ano Inst IM vuoimation ..._.... • . De onW 71779 (i .. Ind, - Apr *epilog RetuniNo Softies . PUMAMI. 10 Ule solne/ay gnom poisons sooplied bolos. the r identiliain kun 4 was inloo0441 in the manno/ plesenbod by Ow Assmovonnoo eino Fas Anilan AdnIOWal N. lOn end. APPROVED O REJECTED PAA Ell.Slenderds illvaiponbr MOnolOant" X InKfOCOOn Aillh041/MiON Oltor (SPOIW BY • FAA Delligre• Ropier &OCR Pelson pea by TunsOon real. Awto one i auta O•uperArrernereasposon 7 /9/ 9 Cił Grafitowe/ Dronation No. _1.4-a iss.-crw . mew um fled :non. ... - . .. • ........... .... __ . , I i i. o. ...Je m, ba. ... '••••• anKaisi".••antaflahDealtataelefaagialikraggvi , 1• 01hal SDNY_GM_02759913 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246835 EFTA01331298 FAA AIRCRAFI REGISTRY CMIEIU R0. 3 DATE: je/r/i NOTICE Weight and balance or °fleeting limitation changes shill be entered in the appropriate 'bore t record. An alteration must be compatible with alt preyiOus alberstoons to assure continued conformity with the apPfloalg• allwOrthatods redulremenld 0. Description of WO* Accomdlisned (II more space teound. attach addaronat sheet Identity wen aircraft nalOneary end reaustralson matt snd ale work COmSdritd -rev 9,04,4,bio—ri -kierhse.39--Ar alvise.,4-oet• 72) A- 74, 10660/0.- 964 (Roza.) 3y••:;9—: -. zugatotrestnver • Mmc- yevetz_ c4:2462;m5-.544-1. 4..--‘ atirGefre-D Ai INC fririctIle2> /1/4 44Xtralbvar 23e 4)/ 7VP. A.Z. Grit -0 /-041 t . • - .Sys77W a 345) oPerOrieWhia, Cifeezetzn SS. *Sow -34-Seat• 'rev 1 mere) ..1747/984. 440e.hg- nov.focc.Av hearrAte" la-v2...05 awely 27.9,4). ?A .M4' or AD 90-eil-osi dew. 59 -8784.:. "Ok.14,4400,9- 23422.-er 11,46" ihraelle 4.7). 317-/illgaTt. Aveat-Penem-Ver: einoy. .ofi 755s. AD. n 774,- Aay.4.rr- reisor Afthink_ SIAlatoar. egnade 17e- .177-4e- web r407- c6rrez. Affiedyrami6 I II:1' APPArtall_ or Agent•Wer mews err" CeilPtionvete • i i... • Oaf ' I t-:.• . tn. Alt Fit.) e j l , • • )' " LING.es\ \,-••, %)"O1\1:\ -7" Te1/4 Se t' • 031'•••• ••• • '<Irv, • •* t.o to...eh/v.101 no tetiliC irdpoe ront • moil . ::(ti "aIdot sbora CyilOvl ervoibro rt. • nrns mil 1. I4In tnnItInn41* i• i In St nn,' stilt" I roil Alio minas, , obits. ' sr-S`c‘o: yvi to Roe frL PI 13411:0 . el tin...mi.. i .it • SI\ t Of yd lortlioolovi Winos yeti toniiitgrol µw p NO .v Die;g1tt wit v soss..0 711 .11.7/1 Lt Ont'Oliqua is• a WIC driloiltbeilIDS 1I *VA p.atn - • "- 7. I X ; tooii AM tm { .11Wrt. ri1C;TPi 6131.1• • n;s its..„„,"0 . I...mm. 4 Ain •• Oberon entoiAiSioo4J .0.7y-oz o nit to;ii..;;;Col Or nom SWAM dakalidnrisQ4 Sri • " ‘• 1n., • SDNY_GM_02759974 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246836 EFTA01331299 FAA AtitteAFT REGISTat CAMERA No . ,3 DATE t y/r/fr TRANSPORT AIRPLANE DIRECTORATE AIRCRAFT CERTIFICATION SERVICE 1.04iANSELES AIRCRAFT CERTIFICATION OFFICE f. • A229 EAST SPRING STREET LONG SEAM CALIFORNIA 40006-242.3 Honeywell Inc. Air Transport Systems Division ATTN: Mr. F. W. (Will) Lynch " 21111 North 19th Avenue Phoenix, Arizona 85021 References: a) Honeywell letter, dated Fe5hary 17, 1994 b) Honeywell letter, dated March 1, 1994 • Approval of an Alternate Means of Compliance • ig response to your letter of March 1. 1994, our review of.the data submitted fh'support of a proposed alternate means of compliance with paragraph C. of AD 94-01-04 regarding Conversion of Honeywell TCAS II part No. 4066010-901, -902 and -903 (My Mod) to part No. 4066010-904 (Mos G), has been completed. We concur that method and procedures outlined in your revised Service Bulletin 4066010-34-SW16 Revision 1, dated February 17, 1994 provides an acceptable level of safety in accordance with paragraph C. of AD 94-01-04 Docket No. 93- MA-68-AD; Amendment 39-8786. further question, please contact Mr. Abby Alan Y. Shinseki Manager, Systems and Equipment Branch 1.% SDNV_GM_02759915 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246837 EFTA01331300 FAA AIRCRAFT REGISTRY . CAMERA NO. 3 -. DATE; -90,/f/ir IT01264Ili 331V*2 V.O/T477.1CH.1:1 ;:!;:7.:51;f4 :!1.31.144 tfLt DItTr.M.:" 771S-a01:;;' .1O".39 A:10.1 • • W.t. r VxvaI.1;41PU • re..?".noli14. • nonotrAlo^lh'i nri0cm::-rtn:A. .': II:fit A: . CS2C! •srioshr. ... .. • v•Hon- r: /0 Ltig';.!* :74.scrtnlifit.bpiooll. 5 to .71tc,!ur ;Cr ‘• ;0:4 a9)1! II WI II:4rcsr.O1:1.6 'notroinoT ottirzgrr : .bn,nIcco? notqi fl.d uel)':•912-0103":". .cr-hng (1123‘a10_,:cr:- • atiurruti nty-H2 betl..401.iuoi nt nnntf;uq zvinnzinicf•iiisiboil/Orn indf :Own ofgetqq”c 1t flasittil( Mir Klcrviv% b1sb :f .r171 III.12-'+C-0100itC) •••:?•.on neteutr.o-ttr fil, nt •••.,,,t/.... 10 fi v9! • • F ,7;1!I.V.: .1 ".t.C!, bns SDNY:NA02759916 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246838 EFTA01331301 • dew. FAA AIRCRAFT ltGISTZT CAMERA MO. ,3 DATtt "6/9/11 5- sit -; : anitwoRTfitiiEss DIRECTIVE FLIGHTSTANDARDS SERVICE REGULATORY SUPPORT DPASION olTransportMon P.O. BOX 26460 Federal Adage° • OKLAHOMA an. OKLAHOMA 73126003 Admits's:n*6On •••••••... 0•••••••••111. Ow /SS *OS Mkeittet aisSio• a s•r ar r 0.1./SAMmak•Paosea 0 . 0 ,m•••• • ...i.e. sea bass mow we as IlkeSts dolmans". es•Snip•••• sialeaussl i•••• •••••••v__ amt... IP. PO pawl WIMP mai bluer milemo••••••0•••••••••••••••• ••••••••••••••••••4 es sq.•••••a0kahm 0••••••• Mary 94-o1434 HONEYWELL: Aniersdnicist 39-8786. Docket 9$411.1.68-AD. Applicability: Traffic Alert and Collision Avoidance Speen (TCASHI computer units: pert numbers 4066010.901. -OM. and -003i as installed on, but not limited to, the goliowtragittrpiiia testthested m an category: • Airbus Induatrie Model A3OO-6OO. A31O-2OO. A31O-3OO. A32O4.OO. and A34O Maim Mrptusees Boeing Model '727.100 and -200: 737-100. -200. 400. -400. and -500: 747-100. -200. 400. -400 and 747SP 757.200: and 767-200 and -300 aeries enplanes: Cessna Citation Model 0550 end 0560 eerie, airplanes. and Omens Citation Ell and VU series airplanes: Canadair Challenger Model a-800.2516 and -2.0112 saics airplanes: British Aerospace Model 125-8OOA: OM/stream Model GIL 0 LLB. CIO. and GEV Genes airplanes: -:• • 2r47, Lockheed Model 4101 l series airplanes: McDonnell Douglas Model DC-9-1O. -20. -30-. -40 and -50: DC./ 0-10. -15.30. and -40;.,,:4 MD-11: and DC-9-8O series airplane& and Model MD-88 airplanes: . . • Dassault Aviation Model Mystere•Paloon 50 and 900 arias airplanes: . i I • Short Brothers Model 603-60 series airplanes: de Havilland Model DHC-8-1OO and DEIC-7 series airplanes; iiti f Fokker Model F27 series airplanes: and Corporate Jets ]lotted Model BAe 125.8OOA and Brio 125-1OOOA series airplanes. —••••• • Compliance: Required as indicated. unless accomplished previously. • To prevent collision, or near misses caused by isionnpatibility between the TCAS U prooraeors and the current au name control system- accomplish the plowing: (s) Before December 31. 1994. accomplish the requirements of paragraph, latilnuad • . al(2) of this AD in accordance with Henri/ell Service Bulletin 4O66O1O-34-SWI6. -dated 3. December 20. 1993. • Iii Remove ranting Honeywell TCAS U computer units. part numbers 4066010-901. -902. and .903. and replace those units with new units that incorporate updated CoMskin avoidance system ICAS) logic, kleuttiled es Version 6.O4A in Mitre letter FO46-1.4O69.id dated September 21. 1993. • • L21 Modify the computersuricIllance {ogle on Honeywell TCAS II computer units, • 1 put numbers 4066010.901. -902. and -903, to ensure that these units accommodate Mode C • altitude input o( 1OO-foot increments and that the system will be tracked and coordinated by Intruding aircraft when the Mode S transponder CA field Is act at CA•7. • (bl-WPrtor to Anther' flight 'after accompUshin,i the requinneents- otperageapir (eat this?. -.W.—nrylle di/ ittinrie. night -Maittlitl"ant) 'ol'AFM- Suppleoient. hing'dthees l °Obit paragraph (bX II or (On) of this AD: (1) Revue the Normal Procedures Section of the AIM to include the tiFiroPelete TCAS operating ellaniCtertst1C relative to the modifications required by paragraph (al of this AD. In acconianee with a method approved by the Manager. Los Angeles Aircraft Certification OOIce (iCO). FAA. Transport Airplane Directorate. Or 12) Revise the Normal Procedure Section of the AFM. to include the following! TCAS operating ellaineterbtle relative to the modification rundrod by paragraph (a) of this AD. This nay be seem:mit/had by Inierting a-copy of this AD in the AFM or AIM Vi e: • 1' . F 5. SDNY GM_O2759917 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246839 EFTA01331302 )3. • .• . . • • . l',',4 1,3 .4'istg;141r3totA!anizailaaas;y: . : It • T...., fx • • . ' 'All Resolution Advisory (RAI and Traffic Advisory (TM aural asesstallea arc Inhibited at altitude of less than 1.100 feet above ground Iced (Mal daubing. and leas than 900 fed AGL deweealing er1 An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used If approved by the Manager. Los Angeles Aircraft Certifleatiota Office IACOL FAA. Transpert AlrpLaae Directorate. °pennon shall submit their requests through an appropriate FAA Principal Avionics Inspector. who may add commenta and then send it to the Manager. Los Angeles ACO. NOTE: Information coneenang the cdretosce of approved alternative methods of compliance with this AD. If any. may be obtained from the Los Angeles ACO. (dl Special flight permits may be bowed in accordance with PAR 21.107 and 21.199 to operate the airplane teaks:an= what the requatments of this AD tan be earorepliaD•A • (el The replacement and modification shall be demo in accordance with Ploneywell Service Suntan 4068010.34-5W16, dated December 20. 1993. This Lacorparalloa by MkSIZEkte was approved by the Director of the Federal Register is accozdano: with 5 US.C. 5521a) and I CM Part 51. Copies may be obtathed hem lioneywell Inc. Commercial Flight Systems Group. Mr, Transport Systems Division. P.O. Box 21111. Phoenix. Ancona 85038. Copies may be inspected at — the FAA. Transpen Airplane Directiemtc. 1601 Lind Avenue. SW.. Renton. Washington: at an FAA. Transport Aftplarie Directorate. Lee Angeles Marna Certification 01110t. 3229 ,East Spring Street. • Loos Beach. California: or at the Ofnce of the Federal Register. 800 North Capitol Street. NW.. suitc 700. Washington. DC. (0 This amendment becomes effective on February 4. 1994. FOR FURTHER INFORMATION CONTACT: Abby Melina. Aerospace ringloo•e. Systems and Equipment Branch. Mitsi-l= FAA. Transport Airplane Directorate. Los Angeles Aircraft Certification Ocoee. 3229 East Spring Stmt. Long Beach California 90808.2425: telephone (31019M-5351; fax (310/988-5210. Tall No. Prod. No. Aircraft/APO Hours • Aircraft Fligftts Date CJCe %O. MI . GI GI I Gill MX. . . • . - NOT APPLICABLE - COMPLIED WITH - DEFERRED UNTIL .,, - . THE ABOVE ITEM IS DUE ON PLEASE COMPLETE THIS FORM MO SE1O IT IN WHEN THE ITEM IS COMPLIED WITH. . N sammum • • 14. 4 1 1 S4 7;* - • - 'off /1•1.fttr:ill pat t • t - • •-• I • •i, • • Tr.e` . :Anil ' al bt , ;:4kini., WI Ha' . 44 ••• • —876/0.4-ffg§ar --- S UBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,o and 17 EFTA 00244Z:1n EFTA01331303 •IAA AERCEAET RECISTRT CAMERA NO. DATE 8 a- - 0 MAJOR REPAIR AND ALTERATION . Oanoweni ohmomowv (AMrame, Powell:4ml, Propeller, or Appliance) Nowntrateiten m........ - Fenn eaneveg OMB No. 2120.0CE0 Per FAA Lem Only °tilt...V:14'9110-15 INSTRUCTIONS:Print or late eat entries. See FAR43.9. FAR 43 Appendix EL end AC43.9-1 for suissequent revision thereof) for instruction and disposition of the form. This moon is moulted by law (49U.S.C. 1421). Failursto reportcan resort in aciriNnalty no110exceed $1.000 for each such violation (Section 901 Federal Aviation Act of 1958). , 1. Altar Make BOEING Model N. 727-31 : I Soma No. 20115 Nationality end Rsoesustion MW NSOOLS 2. Owiwor Marne (As mown on tegISNIAIOn artflkika) NORTHWEST HOLDING CORP. Address (As shown an migration cortzikats) 1105 N. MARKET STREET WILMINGTON, DE 19899 3. Far FAA Use ofty 4. Unit identification 5. Type Unit WM Modal Serif No. Repair Alterman AM RUNE (AS described in hem I share) . X PCNIERPLANT • PROPELLER . • APPLIANCE Type • Mansdalurer IL Ceniareity Itatemme A Agency's Herne and Acklins O. lid A Agency C. Cirtificade No. PAGE AVJET CORPORATION 9809 TRADEPORT DRIVE ORLANDO, FLORIDA 32827 U.S.Cesiikated easchame ' OSORA25M Foreign Ceslareo sfecherde X Consume Am.' Slay. Menuleconer D. I certify that the few and/or alteration made to the un't(s) 'dent,' ied in item 4 above and des< ' me reverse or attachments hereto have been infra in accordance with the requirements of Pan 43 of Ow U.S Federal Ana egeta end information furnished herein is use end correct to ihe heel of my memos.. Date • • 20 79) err /9944 Signature of Authorized Indi --..„, e.i....iragmbge- va.,,,) • 7 Approval ler Ran To Sereloe Kaye 1 to the authority Oren persons specinsa below. the It identified in kern 4 was. Inepeeled in the monster proectibed by Bp Apronistnnor or he Fothemi Ayisnion Administration end le I APPROVED 0 REJECTED - FAA Ft Standards Inspector MSnufsctunor Inspection MAhorizetion Cam (wry) BY FAA Desiree X Repair 51.1105 Person Approved.by Transport Carod y rross Group ... Retention Cenamtte Strew. Author:LS DM* of royal o 0 g / C/ - g or Ossigneho- No. 0S4R4251( geedrictms as ) C „ •-•• SDNY_GM_02759919 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024684 I EFTA01331304 CAA NO. 2/1 DATE: !U-/h2- yr.[ I FAA AIRCRAFT REGISTRY NOTICE Weight and balance or opera NV limitation changes shall be entered in the apPlaCdiste Wiesen secede:. Satirisation must be compatible with all previous ShOhniCteNrro assure continued conformity with the applicable airworthiness reptanaments. & Deoctiption of Mot Amontplehed mote space is requited attach Additional sheets. hawses with circlet naliOnelay ens 1 registration mw* end date work completed.) 127-31 S 20115 peas 1. INSTALLED A DOANE 6 MARGOLIN EMERGENCY LOCATION TRANSMITTER (ELT) SYSTEM IN ACCORDANCE WITH PAGE AVJET REPORT. PR 41-22 REV. A, DATED 8/15/94 AND ISDI. - 91 -02 REV. 8, DATED 8/10/94 AHD APPROVED PER 8110-3 BY DER MARION SHIN, SCE-339, DATED AUGUST 16, 1994. SUMMARY: 1. PROVIDED WEIGHT E. BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINET DETAILS OF WORK ACCOMPLISHED ARE ON PILE AT THIS REPAIR STATION' 0S4R425M UNDER WORK ORDER 60298, DATED SEIMMNBER 2, 1994. • - - END-- a Addlibrolli MOMS IWAIIIChed 0.0041•61-044•01..:03: SONY GM 02759920 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246842 EFTA01331305 -FAA AIRCRAFT IEGISTRT CAMERA NO. DATE: - 4:, . MAJOR REPAIR AND ALTERATION 0 mwmmon wanes- w .• (Airframe, Powerptant, Propeller, or Appliance) • '---Si Miniywow. FormAproosi O1W No. 2120-0020 Few FAA Use Oaly McletePIDO -15 MSTRUCnONSMmt or type all me Mc Sn FAR Alt FAR 43 Anendia & and AC 43 94 Or submmuent mean thateW kw Malmmtims and dimmsitim 0 Mis Wm. T his mpon is maMted bylaw (49 US.C.1421), dims to mph um remit In a WM pmelty ma te encmW WAX kw sun such violation Mecum 901 Envoi Aviation Act 04 1WW. 1. Minna Maim Boeing WWI • - 727-31 Serial No. 20115 Nationality and RegisUstion Mork NSOOLS ' 2. Chimer Nwrie Ms shown on mgoVehon Vindicate) , NORTHWEST HOLDING CORP. Andress (As aeon OM SO 9Wa rtOn ceninhan'n • , 1105 N. -Market Street , Wilmington, DE 19899 1 For FAA Use 4. Unit iderellowdm S. Type ...-, Um Man Model Sabi Nlo. Week Alleinikin AIRFRAME described ,n hem 1 anon) x (As P0WERPLANT MOPELUM APPLIANCE Tam Mensdettwor S. Onsformity StMetnerd A. Arnall Neer and Sam B. Kind of Agency C. Ovulate NO. Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 ti.S.Ceniecattecl tAichank 08,18425M , Foreln Certinuted klechanie X n Swa Cetered nape. im , Merhttectutet D. I certify that ham been furnished the repair and/or in etwation made to the UMW identilied in item 4 above and den with the tectioliennliti oiPanOot the US. Feder& AN collect to the best 0 my noolnew. mode accordance het0n Is true end Date 2, StPrEivIaa 1993/4 Signature 0 AvenorM0 MOM eaellegre-LAAUT el) L Awmowl kw Rolum To Swaim SICAI Pursuant ACIMM4tistor BY o R. wAnollY Onin persona kinifin Wow, the unit WentilM0 in AM' 4 was Inspect In the manner prescribed by the el 1M Federal Aviation Administration AM is CI APPROVED 0 REJECTED FAA n Standards Mrprct d lor Mmolonum Mg*CtionAulterOWNm aver Minivy) . FAA Desire* I X Rep* Station Cmwda Werair= Date 01Appeoval Or Rejection 2 SEPT: 93/4 toniticoto Or .. Designation No. CoS4R425M SPriat el AO In . A a-- .1 i .esoc÷gL e fr om ... rit1 41 01 ! SDNY_GM_02759921 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246843 EFTA01331306 -FAA AIRCRAFT REGISTRY CAMERA N0.3,:/ DATE: /0.-Ig.-/I4 a. NOTICE Weight and balanceat Oporatind lineation changasShall be entered in the &uproot's"( t advertise-owl An aneiation must be compatible with all previous alunanons to assure continued conformity with the +Placable airworrhonas mammon's. • bescrIption el Work Accomplished Or more space le toptinad. Minh OddrtiOnal shNn. identify with waren nationality and rogweration maw and are work compiled.) • 727-1k SIN 2011 psoor.s. 1. REPAIRED CORROSION ON THE LOWER FORWARD CORNER OF THE AFT CARGO DOOR BEAR STRAP IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-30- 02838 DATED 8/11/9a AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339,' DATED AUGUST 22, 1994. 2. REPAIRED DOUBLE DRILLED HOLES IN B.S. 940 MOD KIT BRACKET IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-10-02839 DATED 8/10/94 AND APPROVED PER'8110-3 BY ORR MARION SHIN, 50-339 DATED AUGUST 22, 1994. SUMMARY • 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION 054R425M reIDER WORK ORDER 60298, DATED SA Pr. cit. END 0 Additional Shafts Are Allhched cadwadieleModiavOU --- MbNyaoffcg9i2 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246844 EFTA01331307 -FAA AtSCRAFT REGISTAr tahERA No.,W DATE: jogg-,44 fr • 0 MAJOR REPAIR AND ALTERATION scaraienes a bresenceot (Airf faille. Powerplant, Propellor, or Appliance) leasemensis• •••••••••140 Form ApprOved 01•13 No 21204020 For FAA Use Only OffiASIOn DO— 15 INSTRUCTIONS. Pnnt Or fee ail envies. Sae FAR N.Y. FAR 43 Appendix ELandAC43.9d (or subsequent tension thipreog frif irsiruclIons anthespositionol Mb tarn. The report is rewired by law leg U.S.C. t421). Failure bravest can result in a civil penalty not to emceed Et .000 for Nen such vielellan Mattoon 901 Fedorel Armen Act al 19581. • was Boeing Nodal 727-31 Ertel NO. 20115 NatIonelity end Alma?. 2. Owner Nan* (AI Mown on registration aveldicata) 'NOR1MWEST HOLDING CORP. MIdnissIt iftrrIgginrInteE Wilmington, DE 19899 . • t Far FAA Us • Owls • .. .: A Unit Ideallikellee 5- Ins Unit Make Model Wet NO. Etna Mango' IJAPPAME denuded ... in flare I - X (As abere) POWEIIPLAPIT • PROPELLER • V ANUANCE Type . d 0 • Manuesturer • • 11..Cegforolef Illeleibeed A. Agency's Name and Ades . 8. KIM Of Arty C. Cartillosla No. • Page Avjet Corporation , 9809 Tradeport Drive Orlando, Florida 32827 A U.S. Caretcara keer sic OS4R425H . F Cerliscased aschank X Carriatanto Pup it t s andart lianulacktor 0. Id0r1Ity that 1.00 mink and/rmIllt010000m04010 the yogis) klentilied in item 42Snenddescribed have teen nets in &cordon:* with the requirenteints of Pan 43 of the U E. 44410•1Aylati futnished hadan A Ind and correct to the Wee aity luta...WSW on the revere. or Miedunents hereto. Ind that m ion ' .e - DOI ; 2. 6 EP7E/raile. 14; 9 3‘ egnelura of Authoring' Inevid 4,3,6€21"7.4.0>2 ei 4.,/ "it L Award for Ran To Bake Natu011110 Administrator SY IN 1011001117 of the Federal persons specified Administration below. Vie unit Mobbed in item 4 was I Win 100 manned prescribed by Ma Xl APPROVED O REJECTED rat Aviation and 'e ' . FAA Ft Standards Inipscior Manulecturet . leveler. Autharialien Othe (Specify) FAA FAA Desiree. X Ramie SeliOn Person by Transport Canada Group Dee of Approval or Refection [2. SEPT 90 Cordlivile or Designation No. OS4R425M Signal ol Auth, 4" gew7i-itn "4 • FAA Ions 337 Ma, SDNY_GM_02759923 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246845 EFTA01331308 •PAA A&'CRAFT REG/SERI CAMERA .:n, ?Ai NOTICE Weight and Mattel or operating limitation changes shall be entered in the appropriate aircraft record. An alteration "lust be corneal:We with elf previous alterations to assure continued conlormily with the applicable airworthiness requirements. a. Owalption of Work AccoorpWhof I mote *KO Pi required. Sank addolsOnal SAM. Identity wan akentt nalkallety and iaglaustion mark and data work compered.) 727-31 S/N 20115 N5001 1. RELOCATED ACCESS PANEL FROM B.S. 1183 TO B.S. 1350 LH AND RH BETWEEN STRINGERS S4 TO S7 IN ORDER TO FACILITATE ACCESS FOR FREQUENT INSPECTION TO TERMINAL FITTING IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-30-02837 DATED 7/428/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339 DATED AUGUST 22, 1994. SUMMARY 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION OS4R425M UNDER WORK ORDER 60298, DATED .2.S.6Pri744 •♦ O Additional Shoots Are Matted eflOPW.9010-61WWilaWDS • • SONY GM 02759924 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246846 EFTA01331309 FAA AIRCRAFT REGISTRY CAMERA DATE: /- 93 0 MAJOR REPAIR AND ALTERATION us innmi alemo Otis demn (Airframe, Powerplant, Propeller, or Appliance) nersammaaa miammatin Fore Amend OMS No. 2120-0020 For FAA Use Only Office Identification 51-ISB0-15 meittiOn ImallO) lor insmmtions a CivilPenalty not to exceed S! WC INSTRUCTIONS: Print ortype all•MnesiSee FARM.% FAR 43Appandk B. and AC 4.19-I (Or subsequent end dig osit on ol MO Ner This mport ra requited by law (41I U.S.C. I421). Falleml0 moon can result i tor sect such violation (Section 901 Federal Aviation Act Ol 19540. d ,ASR Make Boeing Model 727-31 Sera' No. 20115 Netionauty and Registration Math N5001.5 A Owner Name (As shown on cogiartarknarPfloa) NORTHWEST HOLDING CORP. Addrena (AI Shown on respitnnion ['Waken') 1105 N. Market Strut Wilmington, DE 19899 a. For FAA Use &Ay I. tha IderAlkatlen : Unit Make Meal Serial No. Repair Alteration AIRFRAME • • fitadretliddlamie ',teen R '-«, POWERPIANT , PROPELLER APPLIANCE Type -Manulecturer liy.eneerealty 9~ A. Agency's Plante and Address & Kind ot Agency C. CerlAket• No. Page Avjet Corporation 9809 Tradeport Drive Orlando, FL 32827 us. cee~ hum« OSeR425M • Fame/ Ceninesma Immune g Ceramic., name Saloon limulson D. I Certify inn thermal/ and/or iil ttttt ion msd• to the un tO) identified in dem 4 above and insonom on the reverie of attachment* hereto hove been made in eteoidente with the requirement* 04 Pest 43 of the U.S. Federal Aviation Regulations and AN the hrikanation !tarnished herein is IAN end correct to the bath el my nowledge. Date • g l i /S 3 Signature eked Individual /Pbenflt.my V. etc.,,' Y iei‘0 04-; • % 7. Ice serww , Pursuant ' AdmIMstrator Dy tc. the authority given persons awaked below, the unit Identified in hem 4 was InsO/cled In the manner prescribed by the of the Federal Aviation Administration and a 10 APPROVED 0 RE ECTED FAA Flt Standards klepeClor Mainulachow InsORCHOn niAreillizenOn own (Spurr/ , Mk glengen x Repel( SUNK _ Peon AppriAM ini by TranSpen Carsnnes «Mm Gram Date.' royal w emection r.25-/f3 7 CortIlkete or DesIgnellon No. 0S4R425/1 Signal sol Authorised / r oat IC*" di gmea, A -A./Pot vi . '3 FAA Fom 337 Fiat, RDNY_Ohl_O2759925 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246847 EFTA01331310 FAA AIRCRAFT REGISTRY CAMERA NO. IN DATE: 1,9* NOTICE WeightandbalanceOr Operating limitation Changes shall be entered in the appropriate aircraft record. An alteration must be compatible, with all previous alteration: (0 assure continuery conformity with the applicable airworthinest requirements. .5Z 0 U. DeseMpt ono R. Acconosbed (If more space is required. attach echlaionar sneers. Wady with aircraft nationaufrand regatranon mark and dare wore comp...4dd B727-31 • 'SIN 20115 - .N5OOLS 1. INSTALLED HONEYWELL SCAM II SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA309450. • SUMMIT: AIRCRAFT WEIGHT AND BALANCE UPDATED ACCORDINGLY. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS INSTALLED OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. 4. ALL ENGINEERING AND WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION UNDER WORK ORDERS 7492, 8112 AND 9301. 5. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. • • M • '!4!.)21.!:, ' AdeNioneu shateswintaine *US PRINTING orncc, inl-ali-.01210117' MONYMA4_0 926 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246848 EFTA01331311 FAA AIRCRAFT acCISTAT CAMARA ND. 2,r4DATZA 1/ - 4 - 9a • • .- 74% , • MAJOR REPAIR AND ALTERATION vs waine's .. o bovecnoinn (Airframe, Powerplanl, Propeller, or Appliance)`' ' ...•• 4.4,4•4 • ...../........ . Form Approved OMB NO. 2120-0020 For FAA Um Only Office mantill as lc • HP INS trivet IONS: NMI or type all entries. See FAA 43.9. FAR 43Appentli, Band AC 43.9-I (Or subsenuentralsIon thereof) Mr instrucdons and cintioseion oldds Iona This Minn Is required by law (49 U S.C. /42n. Failure to report an coattail a civil penally not toeaceed 31.000 loi tact' such violation (Section 901 Federal.A.Sation AO ol ISM. I. Newel mote . Boeing Model 727-31 _- Serial No. - 20115 Nationality and Registration Mark N5OOLS 2. OsnWI Name (At gammon isolAitallOnnellikalo) r. I Northwest Holding Corporation Address (As shown on rooISItallon OnlificolO) P.O. Box 7138 Wilmington. DE 19803 - 3. For FAA Use Only 4. Unit identification L Type Unit Mae Model Soria No. Rep, Alletstion AIRFRAME (A 0 0 0 I 442, X / POWEILPI.ANI roproun APPLIANCE l ype • • emdochnel 4 CORIOS IllalaiM•II __.., RA ' ,.. A AyusiErs. Mane Mid &Muni. El Kind of AElencY C. Cadilitlite No. u s Caner-nee mown Page Avjut Corporation tent. cmainared meehanic 9009 TY a tItfiius' I. I)i. i VI3 3 entm‘neennmustam • 0S4R425M Orlando, Florida 223327 . - hilmw4clumw • I) I curio, mai 4i..c.4-)Mei aalign ..IIV.400.5 MOO PO Rig imill(4)6026Itilmed ri...e wen ...Jo k a...no... e anis he rectuliammla is....t.Ai swop'. ib buy aid 4.4.0:l to die WM ol my - In item 4 moon and doomedon Int ieverse or allachmentahmoo or Pon 430 Me U S Fmmerd Aviation Regulations and that U.. 4404414H011 knuelcd(le • . ineiv . „5_11LAICr ) •i+ 1 2 17? Sly, owe Le A. i hs...duel 4 met, .KWrigiti- • 7 al km Rouen To Service ewe., to Inc 4,4,....., Ione pqa...4.4 sprcilkad Wen'. the RINI adetiliblia in Awn 4 *es anpacred in ma manner gultricribed by the Adinnisti.oei or the I ouni.a An Iwo AdmInialrallon and Es . ft .AFINSOI/ED 0 Mt EC I 30 az. I AA I II $4440444I. lowalul M.Rlielatluott InilputIANI Aull'OMMICIO °V14, ISPOC.4) LP? I- AA llestonw X !grime Station NOM, AIIPIIned Or IlltinPart Canada Ait *tinniness Grove Vole LA A. Iluvalut Ihneconsit ..:11 NfilLeSt lillip- CcitthCalt Of Demenation No. '0548425H Skilialuly Of AillA00110 Individual fN/ .. a.o.:O hi aer--nant--1 51.0.0 it Lfrnni-sr SDNY_GM_02759927 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246849 EFTA01331312 FAA A/ RCRAPI REGISTIE CAKEIA NO. 3PATZ4 //-4-4a • NOTICE Weight and balance or operating limitation Menges shall be entered in the appropiiale aircraft record. An alteiatron must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness reutorements. g n arl) et Watt Acceenollshed &pee et neutral attach edehloOnia Sheets. Identity with *heist: naloOnahly and reeilltelopn milli and dale were teingthled B723-31 ' 5/N 20115 1. MODIFIED SECOND BATTERY SYSTEM PER PAGE AVJET CORPORATION STC SA309250, MASTER DRAWING LIST PIDL-91.-37, REV. A. 2. MODIFIED ED 805 EFIS PER PAGE,AVJET CORPORATION STC MASTER DRAWING LIST MDL-91-44, REV: A. 45001,5 SA3085S0, • 3. MODIFIED FMS-800 FLIGHT MANAGEMENT SYSTEM PER PAGE AVJET CORPORATION STC SA3089SO, MASTER DRAWING LIST MDL-91-43, REV. A (NZ-9112 SOFTWARE). SUMMARY: 1. PROVIDED WEIGHT AND BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINENT DETAILS.Opk. WORK ACCOMPLISHED ARE ON FILE AT PAGE AVJET CORPORATION UNDER. WORK ORDER 9286, DATED AUGUST 31, 1992. END 0 Additional StoatsAte Attached O •• SDNY GM_02759928 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246850 EFTA01331313 PAK-AIRCRAFT REGISTRY CAMERA no. Zit DATES q- 9a, • 0 " MAJOR REPAIR AND ALTERATION . uSOwaserate atoracarron (Airframe, Powerplant, Propeller, or Appliance) Newt smarim AdwatIvann Form Approved OMS No. 2120-0O20 For FAA tfoe Only 011ice Idenolicauon 30-fS00-15 _ INSTRUCTIONS:Printer rye el entries. See FAR 419.FARA3Apkodis ill. and AC43.9.1 (or subsequent revision Memo() lot insloudions end Oisposnion Of thi4 (atm.This report 4requited by law (49 US.C.14211. Failure IC NOON can topsoil❑in spoilpenalty not lo escood 61.000 for each such viola6on (Section 901 Federal Aviation Act o119541, I. Aircraaal Mee Boeing Model 727-31 Serial No 20115 Notionalily and Registration NW N5OOLS 2. 0•044 Name (Al shawl on rogisitanencerrificon. • ' Northwest Bolding Corporation • - • A4Onass (As shown on enistestion calif aft) , •P.O. Box 7138• - -. - • Wilmington, DE 19803 ... Fee PAA Mee Ord/ - • . ' . . . 4. UnR Identilicalion S. Try. Model swim Met' mention AIRFRAME • -, (Asa bad I I fl own • X ROPtrotAsir . . - • Menem& . APPLIANCE Type WNW B. Conlon ally Slalemeni A A or 4 NOM and &Mem B Kind of Agency C. Conflict,' No. Page Avjet Corporation 9809 Tradeport Drive Orlando Florida 32827 U S Catainataa mautente O54R425M rw«gn Catoicatto hlecninc X Cott/caw Roam stalwn leNectiov D. I Gently Owl Ube tepair andfot alteration made to IN un li at idenithed in ileni A altrotli And deMeibed On UN (erne Or •INCliments Nnolo hate been mod* In eccenwice with iho taqvleornenla of P 11 43 tat Ina U.S Fecletat Aviation RintulaboM and that IN sat ininiOn • Banished baton is his and cot tool to the INN of my nuatledge Dole , •-.-:- 2- SIgnelwe e JOH., 1- at all Nir 7. Ann, Retro To Souk* Pu want to Inn authatity Oven persons IIPICIPod below. In ml Al•ntilta0 in nem 4 was inspected In the manner YeelKbbei by let ib Adauflealat of the Fedei al Ac onion Administration and a (1, APPROVED 0 RE ECTED FAA Fit Standards ilitspuder anulacturer Inapoc000 YonlObiaben BY /AA Charm I Repair Shallots Pet son stormed by rtansoon Cam& AlretifINness GIOIA r ISpOeligi Dale al Apµ Oval et RegicUon Zt JA ), $2 N Cot IbiCed• 04 Designation No. 03411425N SI lure of Aulhonzed I - Ad ak..4.- _MOM H I-frill-tat • AA Fenn la/ •• me . • ' SDNY_GM_02759929 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024685 I EFTA01331314 NOTICE Weight end balance or Operetta g limitation changes shall be entered in Ms appropriate aircra If record. An aneration moil M compatible with ell previous alterations ro enure continued conformity with (he applicable airworthiness requimments. a. Oneripoon of won iktemopoolloo qt mom space is required. attar, eddilionsl sheets. kleatty with arced, nationally and regiataion m✓t and dew wort comolearil E727-31. LAN 2n1li 1. INSTALLED SUNDSTRAND MARK VII WINDSHEAR DETECTION/GROUND PROXIMITY WARNING SYSTEM (GPWS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA311350. SUMMARY: 1. AIRCRAFT WEIGHED AND NEW WEIGHT AND BALANCE COMPUTED. 2. EQUIPMENT FURNISHING LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS INSTALLED. OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. 4. ALL WORX ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. 5. AIRCRAFT TEST FLOWN BY CUSTOMER AND ALL SYSTEMS CHECKED NORMAL. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. 0 Addition& Shims No AMC'S SDNY GM 02759930 OleneefltieeleIVIII SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246852 EFTA01331315 FAA AIRCRAFT REGISTRT CANCRA NO. iv DAM _ 9 07_ I 0 MAJOR REPAIR AND ALTERATION , usosonses wkwasavown (Airframe, Powerplant, Propeller. Or Appliance) tedani Mamas mi.... Form FIPProved OMB 51).21204Xr20 FAA Only F LNG " or Onkel rhilicsiion 90:1100 -15 . INSTRUCTIONS:PARof type ellantries.Se1FAR 411 FARbAppercla 0. and AC 419-1 (or Subsequent owision thereoll Tor instructions and disposition of this icon This report Isnquhed by low (49U.S.C. 1421). Failure to foetid can result In *civil penalty not to **coed 51.000 toe *fah such violation (Section 901 Cedes* AMNIA Act 01 10!1). 1 likaell Make Boeing Model 727-31 WM No. 20115, Nationally and Regialialscw Mock • . ., N5OOLS 2. /Nome !ulna (As shown on flu mica C•StitiCarin Northwest Holding Corporation Aadtaaa (As *P0PP on geplOration citrialcoN) P.O. , Box 7138•..i.. ! - Wilmington, DH 19803 . 3. Pei FAA Use Only I. Unit klenttlIcelless R 1114/ Unit Mad Model I SOAPING, 'Repair Alteration AIRFRAME , (As OM tad ' Mae I above) X POWERPLANt • i PROPELLER . *FALANGE TYPO Mobilactueer • t Conlertint Ilabtrosel A Agency's Myna end heltinnif fl. Kind 01 Agency C. CeRilltate No. Page Avjet Corporation 9809 Tradeport Drive Orlando Flor da 32827 u I. CA...lawny waving OS41142514 I wow Ovulated Mycboroc x C....fain Raw pas.. . uswisckaa• D. I candy Malilia mow and/0, alientlion made to the unit's) idantilie0 in nano abOra and dantat006 on Ina Mafia 0. anaChinenis Imola have Wen made in atcuidanCts with the tagoLf•Mants ol Pail 43 ol the U.S Fadagoi Aviation Ragullatiani and Mat IN InkirinatiOn larniatiod herein is Ina awl CO4 MCI 10 thll best °tiny nowledge. Date • 22 4 . _AK!, lAtif 1 ..._9 9Z Sawatute ol *obeli/ad - _": Individual arnt.5 r. 191l1- Jr. . tor Rattan Te Sento, Po Mnbn.Ili BY manic ma stithtway &ICH Ones Fade, We Naar* specilied Mow. UM unit identilied in hem 4 was Inspeclad In the manner pintaibil4 by the I bvibliab AOMAIMIMIOn and is B APPROVED CI REJECTED FAA AR 51403.101 Instwv-Wr Manufacturer Inspection Aushorlowon ONMISANOW FAA Designee X Sept, SWOP.. bibtOn App pod by lialnyal Canada Airwoilhinem Gioup OMe ol noon:nal*. Reloction ,p.11.3rh-) (19a Cs/Inhale ea Crosignaton No. OS4R425H Sig Nee of Authoring Individual - .. 41-1,11-,,,,e.4 Ds.) F./ 1471/0/4 I'M% Yuan 337 .o mm e: SDNY_GM_02759931 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246853 EFTA01331316 SDNY GM 02759932- - FAA AIRCRAFT REGISTRY CAMERA NO. /,y DATE t _ q_. 9a NOTICE WHO: and balance or operating limitation changes shall be aniseed in the appropriate aircral record An alteration must be compatible with ell previous alteratiOns to mute continued conformity with the applicable airworthinen regiulatinentS. OneApliantitottAecompialed Of more space Is required. nown additional sheeti tclontily with WiciaknotiOnstity and regulation mark and We work completed.) A727-3I 4/A ,n115 1: INSTALLED- EXECUTIVE INTERIOR IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA313750. 2. INSTALLED HONEYWELL EDZ -805 ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EPIS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA308550. 3. INSTALLED MODE "S" TRANSPONDER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA309550. 4. INSTALLED JAMCO SMOKE DETECTORS IN ACCORDANCE WITH PAGE-AVJET CORPORATION STC SA313250. 5. INSTALLED DUAL HONEYWELL AA-300 RADIO ALTIMETER SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3087S0. 6. INSTALLED HONEYWELL PRIMUS 870 RADAR SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3086S0. INSTALLED HONEYWELL PMZ-800 PLIGHT MANAGEMENT SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA308950. 8. INSTALLED DUAL COLLINS PROLINE II COMMUNICATION AND NAVIGATION SYSTEM IN ACCORDANCE WITH.PAGE AVJET CORPORATION STC SA3090S0. 9. INSTALLED HONEYWELL TCAS II SYSTEM PROVISIONS IN ACCORDANCE PAGE AVJET CORPORATION STC SA309450. 10. RELOCATED FIRE "T" HANDLES IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA311150. 11. INSTALLED FAIRCHILD II PARAMETER FLIGHT DATA RECORDER IN ACCORDANCE WITIOPAGE AVJET CORPORATION STC SA309180. 12. INSTALLED DUAL 40 AMP HR NICKEL CADMIUM BATTERY SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC 5A309250. 13: INSTALLED DUAL. HONEYWELL ADZ-800 DIGITAL AIR DATA SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA308850. 14. INSTALLED AES AUTOPILOT INTERFACE UNIT IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA309350. AddeVerurl SMell Am Anached SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246854 EFTA01331317 FAA AIBLEAZT ■oGIEUT cans so. i# 6_1_ 9a, rya. • ..a•••••• 'WIN* - PAGE 3 OF 3 - 15. INSTALLED HYDRAULIC ACOUSTICAL FILTER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA313650. INSTALLED RSSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC 5A25985t, SUMMARY•: AIRCRAFT WEIGHED AND NEW WEIGHT AND BALANCE COMPUTED. EQUIPMENT FURNISHING LIST UPDATED ACCORDINGLY:, ALL SYSTEMS INSTALLED. OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. ALL WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. AIRCRAFT. TEST FLOWN BY CUSTOMER AND ALL SYSTEMS CHECKED NORMAL. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. • END- • _- - - _ SDNY GM_02759933 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246855 EFTA01331318 SDNY GM_02759934 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246856 EFTA01331319 • FAA AIRCRAFT REGISTRY CAMERA NO3 M DATE: 9 . Tam AppeOve• lot pt 100p1 APPLICATION FOR untpaine• AIRWORTHINESS - " koncesisa . ==•• coo /.....9 CERTIFICATE INSTRUCTION1 —•••••••• typo 00 tool voila in 0.603vem.thete we lorFAA ISO*. dobed Ongietanmay an Repeektv4on• 11500bon0 IDKIIII•lqVire0.440snalladienimi 50FIDIC•iripmperrnA5C0,00115.ccw.th• ll among iall •55053•50.1. • . - t 8 LAIONITAA St) Sc II . 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Atha ; . i 1 TARTAR,IZI,Idi in CIIII•CM Ki.04.4.5 CwWew a- COlli•CATICIROWICK.,* C•••••••••• LOMICATIDPU0.01/51000•••CanAta• len d • NICSJ t WNW ACIWCP i i a) .• nor e I tems ' ..c. .. .. - . ti• I Mil lenn•Al4 esvreanets. a dna 5 nee det IntC000ILAII ALOLII5150 • ••••••••d••••••••no41010 knee I la VII sm. re.0.550••• • sthamose•rf 04M001•0110. • 0 .0100 050 .0)40 •54,1055•05005 1. If 0. 405060•••0••t••• ly • 0155• 03•00SSealerel l ' 5.5 7 0•305CnIR 05040;55 s 0 .; I ••••••••0fi COII 1•CaCi NIC•55 • Walt W m M I Irma.. e Iasi f Pm li b I r" Mn 71.7 bfri 6 OGIACI 000 ir r ' .. kb e Uothe - - F5- I\I M , MAdtf••00•560440.015 . CAA mm 11106 ill el; -00145.EttS Pn&Y.OUSCOti SDNY_GM_02759935 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246857 EFTA01331320 FAA AIRCRAFT REGISTRY CAMERA NO) A' DATE: 9 - 27 - 97 • •73 :CM:MO-2U -471.10.1) Ai rir • .......ACTLPRO. - HAW • MS* I Migais 0 mooLICTIONCARTSCAlt IG ral•001010.4410.4~/ MIECEIttlf1OO1O611.y . ANTOVIDPII0OIXT011.1111C10. SYSTEM C.G.KOWITITTOP CIATIII0•113410,POWD101101ISTINOPWS 0•VrtO/AMICATICNI NMI I MO MU I40•00•0.0.01 serontuat 2 2 to 5 G 1 1 i I & .10 5 t A.0.5041P,ON OF AIRCPArt • 11.1t0IMAIDO•040 SWICCACM.0.1 .1.006 UMW MtIMISCR PlGtiTtAlttiMIN• • • 000.1•1010M10411 ji./ Tow otmoranva co WOWS O Kb +moose, To - . n 1101/2 11TURECIAtt . . r'-inaT O. C env Kowa° /0 OK4O.1 g 7.4. *scion Mailittfluthftpol . ' Inns I I COA.OT I IT* 00 I I Oint. rtate.y. 0 TN A.Cian Ott POT WO bit A/YMCAS" •••••000.naSS nCO2041•0114ASIOLLOWS .. . . . . . : ma. • 0. Lcm..G r.t.”.c1,0-....., cc,.....c..•• ..cciesan. 'caw. 24 ... o. ........... ........, . LT: . . ...PT "..... . I. ccranc,„0“_,.........1........s....„..1..0.,: e.a.; 11 4... . ...1.......:6L1.4.- I.' 1,94 nint." ..'S.a., '''' "erear."....."•Xidar...ar"...." ......t..?":..9.1!” ..,..4"..I.e-11.".” ....t r r i ; • .0•04.4 • . . • I. WI • C4.4" 0,-,-"Pnr, .,......^n NAME MO MU WSW 4,, Val 0 C.4..../. *mak • , . ^ O...loir I *a GIMI.Sp.r ~11G1fl IM' . AA fem030•614019040.20400~0.- sl I g f ti el 3168004.<re ' • s . , O . . g . . , . 0 , O s : : : • - o n -I . . : : : : : : : : 7 4.. A.- 1".b. ar- al?It ..""4".. . °"1"4- it aty-m-a -a.. . .. 4-11 A Cons 0 Wpm 6,4 11.Y.-0 iftwouate 0.....i a natal • r La row-emboss V 41••••••••••..../AlemeoMM 1...1), Gareth ~wean .„ a 00.... la... ••••• ."1/4 1.aine• .0 -21 1 1 lf.K1SI4esibe• Mani linos f rut • I Kew woke -Mb . _ „P- spir-f .ctiS§a43 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246858 EFTA01331321 •••••••.— FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 27 :91 IMMO Malt Op 614.e.• eitPARTMOIT OF TRAMIPCSITATION-MOW. AVIATION ADIAOUSTRATION “. • STANDARD AIRWORTHINESS CERTIFICATE. . I Pr lawn , NC I ONOISAC7100I1 WOK N505C BOEING 727-31 3 &SCA.? MIt Wa41. 20115 TRANSPORT ▪ NJTMORITIPMO &WS roo. MUNK, • lidelaalnes aiit• pothmal IOW fed**, ..1104•13 of II] II int [Mg. pap net um*. Omura we w ow. le • 110 Moog M l••• •••••014 rel !oar icresor rem bype •••••N•It Peeler Not a 'a wn. vo OS I. ••• TS or..e. M..* ........P 00" ^"K"C•••ef e,a• • • •••• • • by Seems eta re Grew .ak.nertrweat ON Mare* @..p Si roma Peon t emplet* ▪ WIWI reb CObriTCrl Yrs MOW surnames use,. ar.••••. IV • 06•Imii••• Iona 011•••••• nianann et.N ...ay.... at •••••••••••••••••••• • e•C.• a W fl ew PairlInns eristra••• Oman. Dna •Caleit•••••••••2 a Nati oneeareA.seanopow••• as into* seal •••• I ....Wad ! DATE CSIOLYNCE switire•ar 'A Mt 7/23/90 WING C. CHIN 13t1GNATKINNWOVI DAR-61-FS-NN . lOpeAS.0.4. fir ...And Monica. ow a•pardiSI• 1, <Of Crailp40.000. •atnelela33, Tait r sn THIS rrrrr CATC WS, Ni DYWID • INC Allieltall N ACCOSCONCt %min Met011it 'IMAM • TantlIULMIC•45. FAA Fona $3100.2 SDNY_GM_02759937 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246859 EFTA01331322 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - - 91 SDNY_GM_02759938 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246860 EFTA01331323 a , MAJOR REPAIR AND ALTERATION 0•00,P.,1 areverves • (Airframe, powerpient, Propeller, or Appliance) Sams ban lavirsenvien Form McKeelel OMIINer Z120-0020 foe FAA the Only Mee lelenDlic p 5 .73 C>A I R ..- 0— 0 / INSTRUCTIONS. Print am* NI ectuns.See FAA 43.9, FAR 43 APPONI,x. E. and AC 43R-I (Or Weerant irnsiOnewneolI lot instruction, end eseemiien Minis lam Misreport's/poem:toy Irm I4R U.S.C. 14211. F ;ere to Tr:Demean noun in • enelperolty nauseated 31.000 for each turn vrotegOnlannon 901 Fedora Adobes ACt of Ise). -1 I. Alston Was B0E1AD Mott* ' . 727 -10D.• Udall No. 20115 i Natiameny ono Registration talwa. N5OSC 2. elite. ton (As Mem 00 tegatstrettoncedlikan). NORTHWEST HOLDING CORPORATION - Adds* IA: abort ors regrstradon cenidcond 1409 Faulk Road, P.O. Box 7138 • Foulkstone P Dela laza, SuitI8a2 Wilmington. ware 1 3. kirsauarosi . t . .. . A IAA monialcoruso Iv TM Unit MO* ,A0001 - Weft. Prep* • Attention AIRFRAME /AS Ss< tea ISM I DOH) , X 1 POWCRPLAtir PROPELLER • — •----• - --•,— 4,,t(ANCE TTIM Manureclurer & Caraway sear -. A. Agency, Anoint) Adore!. e. WOO Of Asiore C. Ceti tate No. North American Aircraft - U.S. Ceneemrameetene , Airframe Class 4 Rockwell International Corporation Fere", Cameos) Alecene Limited Powerplant 2825 E. Avenue P X CAnecerel Reset Serer Class 3 Palmdale. Cat 93550 _Mmuerawer ' NXAR688K 0. lawny mettne repaltenWoralterinne made 10 Oa unite) klenageoln dem oaten end ciliated On On sews* or alteCnmento norm hen Veen Merle in emeorctince Rah Vie leillaftri• of P alt 4341Ine U.S. Federal Avineri ReeuraeMmi Mel I mionnatien (visioned Minn le true and correct to ma bar of my nomMelee. i \ Oslo July 20, 1990 7, anwewe Signature of AuMortal inelnvOlial D. A. Perazzo I Rerun. To Senna. Pursuant to the ountored given Demme umocatect Wow. our urn nennied in Rem 4 as Maker* in lecleenner prime/as' by TO ACITISSItIllOr ol the F•0001 Aviation Aaninimmeon and is 0 APPROVED 0 REJECTED ... . . FAA Fn. SIMINV011 VOSPOCIOf l Menulactiver Other tattecOn Findocuon Aumenzahon . • Y FAA Qesign" k Ian" Swan I iCnrn anadlaAnitsntiVess bYTEG( har cwi ve . r i1 .....:,..,„,„,A.,...on }Cornmeal* a of AUNDIUM) Meteorite, I ' ' / ) . 01H19141/C41 No. ' July 20, 1990 ... NXAR688K U. A. Perazzo' i , . • SDW-GtA 0275993r -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002461 EFTA01331324 FAA AIRCRAFT REGISTRY CAMERA NOJ N DAIE: 9 - 27 - 91 • - - SDNY GM 02759940 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00246862 EFTA01331325 FAA AIRCRAFT REGISTRY CAMERA NOJ N DATE: 9 - 27 - 97 Is • NOTICE • • • Weight and balance or operating limitation changes Snell be enteral in the aOProprial• aircraft morel Pri alteration must be compatible with all previous attentions to assure Continued conformity with the applicable airwortniness requtramantS. U. oteecnpnon et Went Acton (II mote Ana 4 /.dewed, Identity with aircraft nationality and fit* trati0n mem an; lo completed.) A. Modified Boeing Model 727-100 , Serial Number 20115, in mental type certificate SA4363101, amended September 1, 1. Valsan-Boeing 727-200 Re-engining Document VA000001, 15, 1990. 2. The following drawings and engineering orders (E0's) aboVe document: NOTE: "VA" denotes Valsan Drawing. a. Chapter 24 ELECTRICAL POWER ' . VA240000 A Llectrical System Intl. - Strut E.O.: 003A, VA240007 E Panel-Load Control Center Modification E.O.: & 006 '"-- b. Chapter 28 FUEL SYSTEM INSTALLATION, STRUT VA280001 8 Tube Assy - Fuel Strut Feed Thru E.O.: 100 c. Chapter 48 MISC VA48I100 A VA481200 C VA481300 C VA481324 NC VA481325 NC. d. Chapter 53 FUSELAGE VAs30001 B VA530003 C VA530004 NC e. Chapter 54 NACELLES VA543000 C • 1A543100 D accordance with supple- ' 1989 as follows: Revision F, dated January are in addition to the 101 003A, 004, 005, Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy Sta 1263 E.O.: .101, 103 Fuselage Skin E.O.: 106, 114A, 114, 116 Intercostal Assy - BSTA 1223 lo BSTA 1243 W/L244.39 E.0: 106- Intercostal Any - BSTA 1223 to BSTA 1243 W/L234.06 E.0: 105 STRUCTURE Ballast Weight Installation E.0: 100, 102 Ballast Weight, Support Structure Assy. E.O.: 002,100 Ballast Weight Instl. STA 312 - 360 E.O.: 002, 100 & PYLONS Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 Firewall Rib, Side Engine E.0: 36A, 003A f.' Chapter 71 POKER PLANT. . VA/10000 Mt Power Plant Instl. - Engine Pod V7Z7RE E.O.: 002, 1058, 109, 108, 001A, 104A, 005A, 004, 110, 003, 111, 006A g. Chapter 73 ENGINE FUEL AND CONTROL VAJ32301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev L), 002 (Rev. MI, 003(Rev. M) VA732303 0 Relay Instl. - Approach Idle Solendid E.O.: 103, 003, 1008 VA732304 0 Switch/IND Light Instl - Approach Idle E.O.: 002, VA732310 A Switch Instl. - Nose Gear Position Approach idle E.O.: 103 VA732315 NC Relay instl. Pilots Overhead Panel E.O.: 100, 002, 101 h. Chapter 76 ENGINE CONTROL VA7SUUOU A Engine Controls Instl. - Strut E.O.: 002A VA760014 A Drum Instl. - Eng. Controls E.O.: 100, 101 VA760015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 In Aeldattonal Sheet Act AMMO • BUSCIOI•6110443 lit -e SONY Ga4-027-549;i1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246863 EFTA01331326 SDNY_GM_02759942 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246864 EFTA01331327 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 97 (2) DESCRIPTION OF WORK ACCOMPLISHED (Continued). Serial No. 20115 1. Chapter 77 ENGINE INDICATING 9A771005 NC Indicator Engine Pressure Ratio EPR, E.O.: 001 j. Chapter 78 ENGINE 11A780000 B VA783010 E VA783011• F VA783013 D VA783017 J VA783024 B VA783028 A VA783101 C. • EXHAUST • Engine Strut Controls Instl. E.O.: 002. Fit Deck -Indicator Instl. T/R Sys. E.O.: 003, 004 Thrust Reverser System Wiring Diagram E.O.: 002 (Rev. G) Support Bracket Assy - T/R Control Valve R/S E.O.: 100 (Rev. E Placards E.O.: 007. 008 Relay Instl. - Thrust Reverser Control E.0.: 003 Mixer. Exhaust - Instl. 727E E.O.: 100 No. 2 Engine T/R Wiring Deactiviation E.O.: 002 • k: Chapter 91 CUARTS VA910002 • A Instl. - Electrical Wire Harness E.O.: 003, 004, 005,006, 007 • VA910008 NC : Wire List V727RE E.O.: 001, 002. 003 •NEW DRAWINGS ADDED TO MODIFICATION • B. Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989. Subject: Fuselage - Station 1182 Pressure Bulkhead web, Crack Repair and Preventive Modification • C. D. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Manual D6-21100. Weight and Blanace Manual Supplement, VA-CR279 is attached. VA000003, Rev. A, Dated 4-4-90 is equivalent to VA000001. Rev. F. dated 1-15-90. END • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246865 EFTA01331328 FAA ►IRCRAFT REGISTRY•, CAMERA M0I M. DATE 27 - 91 SDNY_GM_02759944 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246866 EFTA01331329 FAA AIRCRAFT REGISTRY CAMERA NO.? t DATE: 9.- - 27 . 97 . STATKIN 13t - WEIGHING RECORD & CHECK LIST DATE AIRCRAFT MODEL h 72.7-- kV REG. NO. 1 9-19- 5 - C TER. NO. NC INTERIOR CONFIGURATION /Of 44/eiteil AC /eta/We - - T. PERSONNEL ACCOMPLISHING THE CHECK LEST WILL INITIAL LACK IT tra In IN. Amount..... CLOCKS NOT APPLICABLE TO A/C BEING WEIGHED. . 2. ALL BOTTLES (02102.1420) SHOULD PE IN NORMAL OPERATIONAL CONDITION. 3. ANY DEVIATION FROM THIS LIST MUST SE COOR DINA ES WITH CHIEF INSPECTOR OR HIS DESIGNEE: & DR COMPLETION OF PARTS A THROUGH 0 THE FOR E mAN/LEAD MECHANIC OR A ssicp E 0 INSPECTOR WILL CHECK 6 SIGN FORM SE. PORE PROCEEDING WITH WEIGHING. ,-- -- T IC ) FLUIDS Checked rt:ILI r A B. LAVATORIES CLEANED • VACIJUMED • Chick. BY I. !iLLINO. OIL SYMMS • TANKS FULL se 4.) lIct. I.L.41' IV 2. ALL FUEL T KS DRAINED USING ORAI PLUGS WI PH AN AIRCRAFT Livia - mer iPi T. ALL MAGAZINES. NEWSPAPERS & SEAT SACK - LITERATURE REMOVED , y DRINKING 6 WASH WATER TA,IFILE DRAINED an FILLED I... I - sza ifit • .a PROTECTiNE ENTRY. AISLE a STAIR COVERS POISONED K. HYDRAULIC SYSTEMS FULL • • % O. WINDSCREEN STOWAGE EMPTY • CLEAN 'AP -A1= .1,411 tik ••/V ; 0/ 1 q,1 S. TOILETSSERVICED TO NORMAI: QUANTITY .sPrisoy .rf , A Fit ISM. 'STOWAGE COMPARTAIENTS0N FssOft AFT. LAY. '- . OULKNIATM EMPTY I & SEAPLANE&TELY DRAIN Wilt • WINO FLOATS COMPLE : ' • • . - (:) CARGO, LANDING GEAR a POWERPLANT (DI CONTROL CABIN 1. ALL INSTRUMENT PANELS COMPLETE 34 . 1. ENGINE FIRE SOTTLES CHARGED • , ALL MANUALS; CHECKLISTS. LOG BOORS, t FORMES OTHER WRITTEN MATERIAL REMOVED OClie 211# -1 .:Iiit Call sweilATf ACtr oLETE Virm SEAT BELTS • 44., .U.IT 2 ALL ENG HISS cOMPUTE ;E. ACCESSORIES. ' PLUMBING. ETC. FLIGHT ENGINEERSTAOLE EMPTY • ' CLEAN EXCEPT FOR STRETCHER KIT 9 2fig, . 3. ALL COWLING • PANELS IN PLACE • C) PASSENGER CABIN a . 'RAKE AIR 00171-1 CHARGED e sh. • REMOVE ALL ITEMS FROM HAT RACKS EXCEPT 1. MEGAPHONES. FIRST AID tut MOUNTED Oxlf. BOTTLES. DEMO OXY. MASK • UPS VEST IN " POUCH ti O S. ALL AVIONICS GOUIPMINT INSTALLED - is B. a CLEANED FWD. A APT. CARGO COMPARTMENT EMPTY ....Z.Z.; ...Y.; q Pf:1 ALL PASSENGER SERVICE EOUWMENT REMOVE*" . FROM GALLEY II w.S.11 MA OXYGEN SYSTEM SERVICED 2. . IM FULL 3. ALL SERVICE EQUIPMENT REMOVED FROM PRO. • APT. LAVATORIES --. - . - ALL GALLEY AREAS CLEANED a • VACUUMED glat 4 r4 SP; 4' ..) • & MAIN 'PATTERN • AUX SATTERY IM USED) INSTALLED O. yaw DoORS • SAWN= CLOSED • LATMEND 44. - :. ,.-- ' • G. PASSENGER PATEN CLEANED • NACtRIMED „r ip, , o. g ligi ulit INFLATOO TO OtaiLintiO _-W I. PARTS O THROUGH ® CROWD &COMMIE 2. STANDARD INTERIOR CONFIG. EQUIP. LIST COMPLETED r.AIRCRAFT READY FOR WEIGHING r .4 0/4.4 h MSS SIO OLON fredmaniteml Man. O. Paw Forwnw/Losol Mat O. hewn. Foteamn/Lse4 Meek Or Moque, SIGN OFF COPY PAGE I OF 3 • SDNY_GM 02759945 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246867 EFTA01331330 figlifliNigl"R"."4"147.4" . "bcfa*"'" *14 SDNY ;0271994:""ell SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246868 EFTA01331331 1 FAA AIRCRAFT REGISTRY CAMERA N03 N DATE: 9 - 27 - 91 •• AincnArt WEIGHING SCALES: MAKE Eva-iced-Ey SERIAL NO. 10499 MODEL 73) c CALIBRATION DATE S . - 3 - 9 .0 REACTION SCALE READING CALIERATION CORRECTION CELL DRIFT TARE NET WEIGHT LEFT . S•Gtat RIGHT S, G0 65?TAIL pia 4 7735- -20 -0- 4/ 7 7/5- 98/0 0 - SO - 4 7- O - 4/87so q3 VC +I 0 - ,9^2- or - 4 3 .55- I / CIRCLE REACTION MCI NET WEIGHT TOTAL /041.20 SECOND WEIGH REACTION SCALE REAOINO CALIERATION .CORRECTION CELL DRIFT TARE NET WEIGHT MIA 4/7750 -SO -te 4 1 419 .OO LEFT WING RIGHT MLG WINO NOSE/TAIL itegi 0 #/z) -e -61- its570 ' ii3&5- 4 1- -es,- ZI g4S ...24L WOMOAREACTIONUM NET WEIGHT TOTAL / 00/ 6, Cr...0 I. MIMIC COWLETEO 2. WITNESSED • ACCEPTED . aaN esd NAN. 0, fo 00•IM•0• 4 •et, • Ovisrow 11/b44Wil 4134 NOTE: PART F. AND SUBSEQUENT PARTS TO BE ACCOmPLISHED BY THE DUALITY CONTROL SECTION. NET WEIGHT AVERAGE • .••••.....• •• FIRST WEIGH SECOND WE TOTAL AVE RAGE LIFT il .9T„Q-- RIGHT M4- 40 NOUN All. 1 / 7 1 /g . 11,750 1-t35-5- 1/7900 lag 20 11145- 95-& /5- 91/ 70 X -72O 97801.5 V1575— q3oto CHEOCED•Y 6sf PAGE 20F 3 SDNY_GM_02759947 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246869 EFTA01331332 SDNY_GM_02759948 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246870 EFTA01331333 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 91 • SIC EMPTY WEIGHT COMPUTATION P2 515c GATE --/q- 70 I.,/ CIRCLE REACTIONS USED. 2. ENTER AVERAGED NET FROM /ART F. IO , WEIGHTS REACTION NET WEIGHT ARM MOMENT 'LEFT /OWING I t? Crat- 5- ?gal 45, inkiakr6 S RIGHT 0 NG I i7:575 - (15 Z, t 2 lief , /#5, 447 ..-OrAIL I n 3b0 / 75. 7_ )97, 752 -N itnr - TOTAL &SE/SIGHED - b 200 q9,552.s 111 4 / at 2. 925:27 -277, ListO ?:;4:;;;;; S:, , ".ri?::,,yIs'4! BEw ITEMS NOT ON AIRCRAFT ATTACH SUPPLEMENT IF ADDITIONAL SPACE IS FIEGIARED I (3 AT WEIGHING SUB TOTAL (4 —) ITEMS WEIGHED OUT NOT TO ATTACH SUPPLEMENT IF ADDITIONAL SPACE IS REQUIRED BE INCLUDED IN DEW O SUE TOTAL () °ea®. BASIC EMPTY WEIGHT • .. ci t?, .532 s 1725,27 9 2,1/ 3, 1/6.5: 5- PREPARED IT CHISCHEO BY II PAGE 30F3 SDNY GNL02759949 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF-EA_00246871 EFTA01331334 FAA AIRCRAFT REGISTRY CAMERA 10.1 Y DATE: 9 - 27 - 91 SCH•IY_GM_0 9950 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246872 EFTA01331335 FAA AIRCRAFT REGISTRY CAMERA NO3 A' DATE: 9 - 27 - 91 SDNY_GM_02759951 • • wsegnan. pootoporots now.* tie citation Sy," wrists,* oy • hoo not ocoto•V_SI ot posoranl MI • aces*. 3 vest or bon INK CESITICATE DE DISPLAYED el THE AO.W.IT Accoitont-E %NTH APFISAIllt FECOW. AVIATION REGULATION& SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246873 EFTA01331336 FAA AIRCRAFT REGISTRY CAMERA t4O.3 a DATE: 9 - 27 - 91J A The orwoolunaw Mutes* ea iliPAO View Mt aulhonly 01 the 2108,0 AvissonAci SSW imash•Rops Awaton PogulatiOnS (MR). . B This altwonlunes crlihate Buten:SOO Want/actor netted On On nww$1118NIOCCOduCI PrOduCtiOn 11.01 NUL and Only peCitluctien floghl ICON. 01 San teptsuwed in MIN. Ho Melon May conduct CuOduChon IligN WSW Or OMs cortehale 01 Clurting Pet OnCON properly /01 COrNiOnfahon or hue. anal& (2) Carrying P604cC not toserdal to did papas ol . . IN We t., C Ind alrwOnhntida abrUltcato atnhOuNts the Mghl upacifOclonthe reverse 0011 lot Mown in alock b. . D rho atowOrItOnnuCen.hcalo oerules [rotas ot the dale 0111avanea. the staaftle ' 1810.1•2 has tworonspacied and lound to meet the requirements WON Wheal , FAN Trdaftern8 doe not mew ihe to:tokenism, of the aDO1calUe corntuonensive and detailed anawthinwaS code an Otowded by Anon 0 lo the Contention On Wend's:oaf Caul Aviation. No Meson May Operate MU bode dolcobcd on Ow Wien< Snit (I ) excepi in accoedancewin Me KOlicaleFAII and in arxoslance Yam ctaxmons and linwati0m much may be yr eicntod twtheAdminisuatorin pen 01 Ors commie-Mt 121 over any tOccuan coLoiry without Ina tOecdllutontiSiOn of 111•1 country. . E • unless sooner aurrendone. Satpan:100. Or revoked. and airmen/1nm owtilicawn effective 10f We duvets:in end undid the condthona prescribed in FAR Pon 21. Section 21.1810F 21217. SDNY_GM 02759952 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246874 EFTA01331337 I-- FAA AIRCRAFT REGISTRY OsnERA NO3 & DATE: 9 - 27 91 ' 4 US Worn oflonspyroncn FederalMa:Ma AdministrotIon Manufacturing /nspection District Office 7300 Perimeter -Road South Seattle, WA 98108 • May 1, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's/MARKET SURVEY MAKE:_Boeinq_ MODEL: 727-31 SERIAL NO. 20115. REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market Survey to accomplish the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi River, on the- North by the U.S.A./Canadian border, on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the West Coast of the United States of America. .2. Base of operations is Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a 'Letter of Authorization" issued by an FAA General Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This aircraft shall contain the placards; markings, etc. required by FAR 91.31. SDNY GM_02759953 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246875 EFTA01331338 FAA AIRCRAFT REGISTRY CAMERA 10.3 N DATE: 9- 27 - 91. * 7 2:I,• • • :.!! • ; r; • • i?;•!:f•V; J • t :z - r .:,th 7;• 7.7 gt 7 2,, ‘7:. ..77.11 r:c• • 7! :Sta.: ▪ Ct • ▪ eieiT • .. . SDNY_GM_02759954 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246876 EFTA01331339 FAA AIRCRAFT REGISTRY CAMERA NO) N DATE: 9 - 27 - 91 . 1-4. . .1 • Federal Aviation Administration Manufacturing Inspection District Office Experimental - Show Compliance with FARis/Market Survey, Cont'd Page 2 of 2 7. The cognizant PAA office must be notified and their response received in writing prior to flying this aircraft after incorporating a major change as defined by FAR 21.93. 8. This aircraft approved for day/night VFR/IFR only. 9. 'No operations shall be conducted over densely populated areas or in congested airways except for takeoffs and landings, and when under ATC control. 10. No person may be carried in this aircraft during flight unless that person is essential for the purpose of the flight while in the Show Compliance category. • 11. This aircraft is prohibited (Tom aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by the cognizant FAA office. 12. if aircraft, engine or propeller operating limitations are exceeded, an appropriate entry will be made in the historical records. 13. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). hie ael J. Aviation Sa ty Inspector (Mfg) SEA-MIDO, ANM-1085 These limitations will expire on August 1, 1990. I • SONY GM_02759955 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246877 EFTA01331340 FAA AIRCRAFT REGISTRY CAMERA Nod h. DATE: 9 - 27 - 91 - -_ SDNY GM 02759956 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA 00246878 EFTA01331341 • MAJOR REPAIR AND ALTERATION - - 0 . 14 0103csacni a samtotatca (Airframe, Powerplant, Propeller, or Appliance) Ietsusulistmen . Amambaram Form A00towd OMB NO. 2170-0020 Of* Fee FAA Uwe woe MOMMOM0a PRY FSOti INSTRUCTIONS: Print Of tyCieall OMAN. See FAR 03.9, FAR 43 Appenlia B. and AC 43.9-1 (or stable/NW revision dIereffb 124011nAlIOns end disposition og thbs form. Thy mow is requital by law (49 U.S.C. ICI 1 FailuM10 rePOCI Can romounocfrol Paten). MX la •InOE EIEDE tor ascii such vIONOMI (Seaton 901 Federal Aviation Act of 19581 nEggiUrn FAA 1. wan • BOEING wool 12L-100 ' 2 4 ao ' Aircraft Serial No. 20115 tletionalay end Racietterion Mark Ail N505C rc°1) 2. Owner Name (As shown on rogistran0n cerohmele) NORTHWEST HOLDING CORPORATION ' . AddrIlia(A4 Mown en fRiarration oaMAXAV - [ADDRESS REDACTED], P.O. Box 7138 Pitieln;t2:1:f:WaSuil;8032 i Far PRA 1.18•Only • • • . . - • • A Unit IdmitlecatIon tribe - • Unit Mate ' Modal t . WS RapiIIT • . Al MINOR AIRFRAME (As dincithol In nom t abort) • • X POWENRANT, I ' • PROPELLER . APPLUNCE Type • Manufacturer 6. CoMormi Starent i A. Agency's Name and Address • B. Kind of Agency C. Certificate No. North Amt..ican Aircraft US Gentians rnsnic Airframe Class 4- Rockwel international Corporation roar Canificac Manic Lilited Powerplant 2825 E. Avenue P X Certiricatea hop. Station Class 3 Palmdale. Ca, 9a5.50 -- Menteig fat _ N1CAR688K 0. I tett; iy that the maw and/or situation node to Men Mn been made in eaconlanos with the refttilfemeMS lurMshed herein Is ,we ono Carla 10 the heat of my 1(11 Mar/tined in Item I eatlee end 0600100.00fitN. Monitor tlechments hereto of Pan 43.0, the U.S. Fliderld AvlationtRectutallons and inforKation nowledpe Oats • July 20, 1990 Signature of AuthorMadRiclividual O. A. Perazzo - k «L. 7. Aerial ter Ram" Te Swiss ih m Putan! M the authority given persons swirled below. Administrator 01 the Federal Aviation noannionnice and Dm tau en t identified fn 'ism 4 ass i ea l ...red In the manner prescribed by I he , Is %APPROVED CI REJECTED t FAA Pi. Statiderds Impede. Manutectunor I IrsoactiOn AelhOreabon CRON (SOscriyi BY FAA Designee x Ronan Stun I •Cr w A al ,"" T n' Tj, ""P r, ' Dote or Approve, or Rejection July 20, 1990 Conontno or Oesignahon No. NEARERBK Signature of Authorized Individual U. A. Perazzo k ;4. ,„... ,. SbNY_GM_02759957 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246879 EFTA01331342 I SDNY_GM 02759958 146TICE Weight and balance or operatinplimittilion changes OW be entered ln the sOpropfiale Wreath record. An eller& ion must in compatible with all previous alterations to assure oOntinUei COnfOrtittly with the 'DOUG'S &Matthews. requirements. Modified Boeing Model 727-100 , Serial Number 20115, in accordance with supple- mental type certificate SA4363101, amended September 1, 1989 as follows: 1. Valsan-Boeing 727-200 Re-engining Document YA000001, Revision F, dated January 15. 1990. 2. The following drawings and engineering orders (E0's) are in addition to the above document:: ROTE: 'VA' denotes Yalsan Drawing. Chapter a. 24 ELECTRICAL POWER A24(1000 A Electrical System Instl. - Strut E.O.: 003A, 101 YA240007 E Panel-Load Control Center Modification E.O.: 003A, 004, 005, & 006 Chapter Chapter 100 A Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 200 C Frame Assy Sta 1263 E.O.: 101, 103 300 C Fuselage Skin E.O.: 106s 114A, 114, 116 324' NC Intercostal Assy - BSTA 1223 to BSTA 1243 W/L244.39 E.0: 106 325 NC Intercostal Assy - BSTA 1223 to BSTA 1243 II/L234.06 E.0: 105 53 FUSELAGE STRUCTURE Ballast 001 8 Weight Installation E.0: 100, 102 003 C Ballast Weight, Support Structure Assy. E.O.: .002,100 004 NC Ballast Weight Instl. STA 312 - 360 E.O.: 002, 100 54 NACELLES & PYLONS • 000- C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 100 D Firewall Rib, Side Engine E.0: 36A, 003A VA/10000 NC Power Plant Instl. - Engine Pod Y727RE E.O.: 002, 1058, 109, 108, 001A, 104A, 005A, 004, 110, 003, 111, 0064 Cha ter 73 ENGINE FUEL AND CONTROL 301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev 002 (Rev. M), 003(Rev. M) 303 D Relay Instl. — Approach Idle Solenoid E.O.: 103, 003, 100B 304 D Switch/IND Light Instl - Approach rdle E.O.: 002, 310 A Switch Instl. - Nose Gear Position Approach Idle E.O.: 103 315 NC Relay Instl. Pilots Overhead Panel E.O.: 100, 002, 101 76 ENGINE CONTROL • 000 A Engine Controls Instl. Strut E.O.: 002A 014 A Drum Instl. - Eng. Controls E.O.: 100, 101 015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246880 EFTA01331343 • s*-il, ,t..^% .DESCRIPTION OF WORK rCOMPLISHEO y:- Serial No. 20115 1. Chapter 77 ENGINE VA771005 NC INDICATING Indicator Engine Pressure Ratio EPR, E.D.: 001 J. Chapter 78 ENGINE • VA780000 B VA783010 E VA783011 VA783013 VA783017 VA783024 VA783028 VA783101 k. Chapter 91 CHARTS VA910002 A Intl. - Electrical Wire Harness E.O.: 003, 004, 005, 006, 007 • VA910008 NC Wire List V727RE E.O.: 001, 002, 003 *Hew dr/Linos added to modification. B. Boeing 727 Service Bullekln 127-53A0171, dated December 14, 1989. Subject: Fuselage - Station 1182 Pressure Bulkhead Web, Crack Repair and Preventive Modification EXHAUST Engine Strut controls Instl. E.O.: 002 Flt Deck Indicator Instl. T/R Sys. E.0.• 003, 004 Thrust Reverser System Wiring Diagram E:O.: 002 (Rev. G) Support Bracket AsSy - T/R Control Valve R/S E.O.: 100 (Rev. E) Placards E.O.: 007,, 008 Relay Insti. - Thrust Reverser Control E.O.: 003 Mixer, Exhaust - Instl. 727E £:0.: 100 No. 2 Engine T/R Wiring Deactiviatfon E.O.: 002 C. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Manual U6-21200. Weight and Balance Manual Supplement, VA-CR279 is attached. • x. SDNY_GM_02759959 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFrA_0024688 I EFTA01331344 IIMONShs- SDNY_GM_02759960 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246882 EFTA01331345 IAN AIRCRAFT It CISTRT CAKES FS. DATE: 4.2 - g - " • 1.;',.4)q.. 0 • No 2I7J-0018 APPLICATION FOR mmo' AIRWORTHINESS 0 loomo ---- 21%•......... ...... cco ey c iiCERTIFICATE • ...mucnoges — Porn or typ• DO ROI NAIDAIOD AMA We BOO IAA DOM , WAN •••••140O to WOMMI IAA ADADOUID OJOIMII IWO NOMMIOnonatloord 'wino-am o'o.e MOWN DOW Awn o in, inomos• .. „ . IMMOD — t MOW WOOS NAM Iwo e-tioa 1 NOMAD MOD 00010DINAN ... 9 727 .-- )tta..—A.1.4,/ PM 3 tei 11 ........ “...“.:, 20115, &Oda was Not .4.An idto • 0...bom WOK DISSINAT• ,..32>a:,--m-,7271 I. MOM a 0. N011st• ft Ar... OMAN D. • 9 , ANON. WAGNATIOW IIL NOMAD of iCANA 0 kVA A.)//c. • peon WUC4110•• OW YAM MA i'VW• 8•1•CINA• SIN.. • 5 614/411••0 41.1.0• 144VOSSCIAMICATI 01/40.1~ 7 :7 1 .0.1" 1 I ACAWAVCI DWG"' I lams I Inacco • K VII0.4.. issue., ra.S1Clia co ICAT ,Ovate ray...." . • I WOO • I C. OD . I II POOOPIAL Mins MN i ll C OO • I ' AMODIO —161 CONDI. S .404041MMANO WWADVOIODO • 0 , 461.-OrMisomeD/ . MITAICITIOWasowprom me story 4 9 I /1 POICOM • • MAMA MOO I 7 C77077070FCIAGO • OMR ISOOserl I lOWIDI APO DIVILMIIINT a ANATMOMT II MOMS a IL WiltiOnn.,ot;rnis;sof Oa ineresSie? ...4 noica • CNIAMOING k NM WAD • . abt IIIIIIM COGIROCI WM FM • 1 FCMY RAO IDI POMO ADVI MO NOTION= OA DOOM WOO NWT NOWT MOW I INAMATi IT AND M WOOD MOM WWII, WomeNAW • . P . 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OOMOVIDDIVRE AID NO DONECT001 MOWN • allaan , - SDNY_Gli 62759961 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246883 EFTA01331346 4 —" tam$ area PROMICTIOM COITIOCATC /Wm pa actb•arborto saran TYnalartreaellOhn . ie moon° /110DLCTION itetetiON MIMI Ora WONT. OP CiliniraTa an Or AnurATION Mi. ,/Oa 0000•174010200 isle Me MS Ma • Pal OONANOS S. Milasinel Of AMOVOI lif.atnerrt0 044.40. AOCASI IMOLA iMer) WOE. Mitt Nowaei ittooymATOI•44/0, 11. C407.71.0010M,Onr, • • CUSTOloaletiorlaTION PU3HTi 13 /do a Notate) TO vt& OVOinulit On . • Mamie.' . i C. CAPV MOu MID TO MONTI THE **CAM ANO in tOJII.IONT, — F - TFLOT I 1 COALOT I I imviOATOT. I I OTKO4 'Swain I I O. ilit Mown 004.3 NOT MEET THE AMC, . i AIIIISOMPIOAS 141O01.444.41i M POu.Ora . .. . i L 5 g fit • OLLO•nri0 fittoKrais in ectisacatO Nititn•Prt 105 WI OPOyl v a I *ram« a *smart) . . . . . . . r • . . . V. 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DIM 2— g wino 'Urn 01 *LUCA IM.PAPIVAte . nuAssommou (OEM AVIATIOPI nAINSMATONIi SPECIAL AIRWORIIIINESS CERTIFICATE BUILDER 2OflG DATE OF ISSUANCE 05411410 OPERATING LIM TAT IONS DATED E. sen•Tilt017AIL SERIALS°. 20115 MARY 08-01-10 Alt A PMT OF THIS CERTIFICATE DESIONATIC*4 OR OFFICE RD. sointaCar SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246885 EFTA01331348 aDNY GM _02759964 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 • AAs AIRCRAFT RECTSTIT CAMERA PD. IN DATE: „.2 - g-Q/ A Mb airWOrthl(wSr tertitcate laissubribraell}atifibtily ottha FeoralAvt*Ice. AU of 1F68 • 010Inefixteral Aviation Regu1/4 1:3rts WART. .. . ..... B TIN Wpp111t1certifweaumord9Mb nia.h6feclvoti nomtgl On the reroevaThrtla lo Conduct PrOOXIbb le *Mt arb, ally prOcluGtiOn lgot4 l_a 01 literal' I ragistared In 115 nacre. No WPM SW Conduct production flight lab Older Mb bort:buds (I) Careyng persons or properly km corropeossuon or Nnr. and/or (2) Carrying persOne no OWIMIlto the pulp= of IN Ibult C D , " TNerwrrommesseerlocalo aulhorizte the flight speciCerd on the moms skle kg mamma. roan n BOO A. . The snorisnaki avolancerures that POI Modaleof imams. thosiraaftlovatth itstard has been imPecled ond lewnd to rite•4 the legurernenta 01 theaDigteoble FAR Thbalreran does nal morn thomiqueemere atm spoise.stre cam/nibs:mho and detaDed aliwortbiness coda Ls l.nrrided by Ann.. (I lo the Convereran On Intern:40ns. CM Analion Noperson may oxrate ihnircraft Or/sated cn the revorsiouchz 1 1 I areePOn SCCOrdrinc. mlb the 0POicable FAR an, In•O:Oldtanamothcenctthafn and inutatonswhch may be treschtea GY tt,0 Actinm'Mita. 45 pan of thm certitude: (2! cre an/ Idai9n aaurarY ' ,thou! Ina laaGlat aaann:,, n Ot that Gauntry. . . , • . • tMlessfiete &Wandered. aulpanclad.Or ren'Oked.thts smonhmen cofttlatte **neon" to, the &San and under IN ;andirons prescrtal ci FAR pen 21. Socuon 21 nil o.21217 EF1'A_00246886 EFTA01331349 ,- ,II FAA- AIRCRAFT PEGISTRT CAYERA WO. N DATEt - / 4•;,:f;7"41-?( it'ILZ7v,".9 ...Tege:3/41 h •-,-,64011."-VAtzt,re' • 10•1•00, 0•14 O M • Me 2:20401. ••• ;.• • - APPLICATION FOR 0 ra es. AIRWORTHINESS a knce- ocnuo* New•••••••• .• CERTIFICATE •••••••••• } crwrducnom — Pnnl a MD Op nol rat a .M444 WM thee 8.00, FAA vs•Cmh 1.3cti Copy: cry le an 1•1434•11 FAA ••••••••••••• 4 •:13.10•M le&C•4 myna use inuciveri fa W/44114.4 pormtis CO40441•414•4 gam *not Yu •J annamie ii... SV I SC. • tie0131114/103 Ma L•a3:10/ act IS fLUME HM*. 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Dm a 5 - 0 / - 9 , 0 OiSTPICTOSICII , 5 EA- mtbo M M - 1 o a s 0 1 OCMAIIS SI001•404 Me s) 1 • • • • • Oa ir•PICTORIPSSAWill ' • , e i d u a r . . . . FM Fenn 41304 I,24.4 TuKtisr3C3 InInnOu5 Menem eC ti soir-t ti-offabe8 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246887 EFTA01331350 tire -M-027544es— — SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246888 EFTA01331351 b VALSAA:OARTNERS 3014 Westchester &venni) FAA form 8130-6, ,Application for Airworthiness for adding •Margot Survey* to the authorised our Experimental Airworthiness Certificate. The aircraft is • Boeing 727-100 which has been retrofitted with P G W JTBD-219 engines on tho POD positions and -78 in the center position. We have flown the aircraft approximately 17 hours under the presently issued Experimental Certificate S' We aro requesting •Market Survey" so that we may take a TV reporter and cameraman from Paine Field, Everett, Washington to Grant County Airport, Moses Lake, Washington on 1 May 1990 for demonstration of the Stage IIV Noise Characteristics. The duration of the "Market Survey* portidn of this Experimental Certificate will be only for the one, flight from Paine Field to Grant County Airport. The certificate will then revert to 'Show Compliance with DM's' until expiration of the certificate on 1 August, 1990. SDNY_GM_02759967 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246889 EFTA01331352 [ 7 FAR AIRCRAFT REGISTRY CARIRA 10. I DAUS s- SDNY GM 988 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA 00246890 EFTA01331353 ! 2- .FAA AIRCRAFT Picts/at CAXERA SD. 1 DATES - 8-9/ USOmennen: efren:PC0114s Feclen0Adelion AdmWastreeon ,Manufacturing Inspection' District Office 7300 Perimeter Road South Seattle, WA 98108 May 1, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH PAR's/MARKET SURVEY MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market survey to accomplish the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). . Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi RiOer, on the North by the U.S.A./Canadian border, on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the Neat Coast of the United States of America. 2. Base of operations is Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to -be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a "ratter of Authorization'Oissued by an FAA General Aviation or Air CaYrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing. Low U441ization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This, aircraft shall contain the placards, markings, etc. required by FAR 91.31. • ''..7.1:40 -4 • SDNY_GM_0275998.9 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024689 I EFTA01331354 FAA AIRCRAFT A GIST&T PAM 02 g CAMERA AO. ._I .Federal Aviation Administration Manufacturing Inspection District Office • Experimental - Show Compliance with FAR's/Market Survey, Cont'd • Page 2 of 2 7. The.cognizant FAA office must be notified and their response - received in writing prior to flying this aircraft after incorporating a major change as defined by FAR 21.93. S. This aircraft approved for day/night VPR/IFR only. • • 9. No operations shall be conducted over densely populated areas or in congested airways except for takeoffs and landings, and when under ATC control. 10. No person may be carried in this aircraft during flight unless that person is essential for the purpose of the flight while in the Show compliance category. 11. Thin aircraft is prohibited from aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration riot necessary for normal flight unless approved by the cognizant AAA office. 12. If aircraft, engine'or propeller operating limitations are exceeded, an appropriate entry will be made in the historical records. 13. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with PAR 91.42(a) and PAR 91.42(b). • Michael J. Aviation Sa ty Inspector (Mfg) SEA-M100, ANN-LOBS These limitations will expire on August -1, 1990. • sparacerabio SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002461 EFTA01331355 FAA. AIRCRAFT RTG1STRT CAMERA ND. S1 DATES VALSAN PARTNERS 3014 Westchester Avenue PuraiS77 May le 1990 ' FAA, ANM--108S 7300 Perimeter Rd. Seattle, WA 98108 Dear Sir, Attached is FAA 'form 8130-6. Application for Airworthiness Certificate, for adding "Market Survey" to the authorised operations of our Experimental Airworthiness Certificate. The aircraft 'is a Boeing 727-100 which has been retrofitted with P 4 W JT8D-219 engines on the POD positions and -78 in the center position. We have flown the aircraft' approximately 17 hours under the presently issued Experimental Certificate. We are requesting "Market Survey" so that we may take a TV reporter and c aaaaaaa n from Paine Field, Everett, Washington to Grant County Airport, Moses Lake. Washington on 1 May 1990 for demonstration of the Stage IIV Noise Characteristics. The duration of the "Market Survey" portion of this Experimental Certificate will be only for the one.ilight'from Paine Field to Grant County Airport. The certificate will then revert to *Show Compliance with FARIa• until expiration of the certificate on 1 August, 1990. Sincerely yours, Cheryl BZoyd fotlS.J. Wright Valean Project Pilot SDNY_GM_02759971 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246893 EFTA01331356 SDM'_GM_02759972 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246894 EFTA01331357 I lOt FAA A I REP.AFT REGISTRY Il C IRA NO. I DATEt .2 - g - qi • UNITED STATER OF AMERICA .0113tAPTIMENT OF TRANSPORTATION— FEDERAL AVIATION ADMINISTRATOR ' • • S'ECIAL AIRWORTHINESS CERTIFICATE A CA • ORIMDESIONATION Punt OM 8 maw). Ns)" p FACTURE ADDRESS C FLIGHT FROM TO O "- R 10. — •UILDER I • MODE I A DATE OF ISSUANCE a E °P oat 0 %PART OF THIS CERTIFICATE 0 FAA T,1sY A a ORATION oft OFFICE NO. CH RT S A DAR-48-AC-NM • PRIV•Iwor wan* .1 am Cenfloo on emadis4 3 ram or 70. TWO CERTIFICATE MUST MI Es A Al AWATIAN menus •rinvy by • I— ea says 7100 w espissanns AN LATID MIKE AMA-Ian IN ACCOADANCE WITH FAA POSH SIII0> (7.70) Wt milv sou! EDITION 888 REVITASS SIDS . • SONY GM_02759973 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246895 EFTA01331358 I FAA AIRCRAFT PICISTRT CAVARA PO. .1(4 DAT!, 2 — 8-9/ ---- . A Thb OblOgratthett hart ow Fecterh/ A autlfla ii SPX IF atbl fithAaRROAtity Of the FalethlAVitloetitaat t vition ... . . B r c nD _ E Tbit altwortIgneu mace. auttutitha tA• aliMittater fumed on the nine Wilt. coo- , duct production Mat nits. ad oily prodnetke RI* tote. of sitaaft reidwered al Us nuns No pence may conduct production night tuts undo; this certfEcate: (1)Curybrm per. sone or wpm>. for COMPPLIt4011(II hut; and/or (2) Carrying parsec. not e a to the moon of the MO I. Thb airworthiness certificate authorize. the (bah, apecifird oo the men. site lax the put. pew abown le Block A. This sintorthineu cortillcate certifies that. as of tho data of issuthm., the simm to which Sued has been trawled and found to mon the repot:unmet of the spoilable FAR. The theraft does not mew the nquinewrou of the ep-Araba comprehend,' and duelled a- worthiness code u nodded by Anna 8 to the Connmeloo On laterunboal Ord Minion. No pawn InrY Operate the Wendt ditscribea on the mean side: (I) exaspt In accordance with IS applicable FAR and In accordance with conditions and linutailoos which may be ponalb by an Administrator ea part of thiscortilkata;(2) one any fccelvt coulay with. pure ed special permisdon of that country. .• Vann wooer oatnedered, oispended. or revoked, this airworthiness catillate a for the dentioe and under the conditions presethed in FAR Part 21. Section 21.101 or 21.211. --,,,hotyFT‘ sh>4 soiiiWA_:62757thiC SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246896 EFTA01331359 SDNY_GM_02759975 tAAr.kiRCRAFT REOIStf! • • CAMERA MO. j DARLA oia - 8-en Manufacturing Inspection District Office 16501 Sherman Way.-Suite 200 • Van Nuys, CA 91406 February 2, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's MAKE:'Boeinn MODEL: 727-31 SERIAL NO. 20116 REG. NO. N505C " THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must -be operated in accordance with the following limitations: 1. No person may operate this aircraft for-other than-the purpose of Show Compliance with the FAR's to accomplish the tests outlined in the applicant's program letter dated February 2, 1990 describing compliance with FAR 21.193(d). Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: . - _ 1. Western United States of America bounded on the East by the Mississippi River. on the North by the U.S.A./Canadian border. on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the West Coast of the United States of America. 2. Base of operations is Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to.be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft most, as applicable, hold an appropriate • categmry/cIpss r In aircreft type rating, have a flight instructor's tootiirdatOme ssl"Letthr of Authorttatlon'-issued'by an FAA General Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing Low Utilization Program. I/A/M FAR 91.169(f)(4). 5. This aircraft shall contain the platards; markings, etc: required by FAR 91.31. 6. The cognizant FAA office must be notified and their response received in writing prior to flying this aircraft after incorporating a major change as defined by FAR 21.93. :7. This aircraft approved for daY/hight VFR/1FR only. :2 f' SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246897 EFTA01331360 TAX AIRCRAFT RICISTILT CAF.ERA NO. / DATER 2 - lc- eiv • • '.7. 'Federal Aviation AffieiflstYdtoi-i Manufacturing Intpection DiStritkOffit8:- ExperimeNtal - Show Compliance with FAR's, cont'd Page 2 8. No operations shall be conducted over densely populated areas or in congested airways except for takeoffs and landings, and when under ATC control. 9. No person may be carried in this aircraft during flight unless that person_ is essential for the purpose of the flight. 10. This aircraft is prohibited from aerobatic flight; that is, in. intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by the cognizant FAA office. 11. If aircraft, engine or propeller operating limitations are exceeded, an appropriate entry will be Made in the historical records. 12. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). These limitations will expire on August 1, 1990. -• awit ALtoc99i6 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246898 EFTA01331361 Tat Al ECM/ I 'ITCH TIT CAX88.1 Ar DATES 12—S- 0 ' MAJOR REPAIR AND ALTERATION Form Approved OMB No 2120-0O20 eatromew. oftwendu Poworplanl, Propeller, APO:num) Fat FAA the Ore (Airframe. or mete Men Ameraments Oda Idemilication SO- fSb0-isr INSTRUCTIONS:1feet WOWSinew. See FAR 439. FAR 43 Amanda, S. areAC43.041 (Or sublievent revisionmm.00R for infittections end disposilen Of this term. This revert is rebuked by law (49 U.S. C.14211. Fallen/IC moon runnel M la anil penalty nottearcendS1.000 fraellaCh such violation (Section 901 Fleets/ emotion Act of 19551. i. Adman Adman Boeing Mete Model 8727-31 Serial No 20115 Nationality and Registration Mart 85001.3 1 Ownat 1 Name OR Shown on reptstraion Cerribra) . .• . • forthweet Holding Corporation . • • . kerne (As shore on nopisteafkal Certilkalfl . • • ' P:O. Box 7138 -rn Milaington, DE 19803 3. Per FAA Mee Only - - • I. UM lemilliesike t 5. Type the Make • Meal Side Ng. Repair Alteration AIRFRAME lAd SWOON In nom lobe ) x POWERPLANT PROW : t.' t APPLIANCE Type ( — Manumetutm S. Conk/rate Stalemate A. Adeney's Nene and Addams J a Kind of agency C. Choi rale No. Page Avjet Corporation . 9809 Tradeport Dr4ve ' Orlando, Florida 32827 ua Centaur madame 0848425H Fenian Canneeme Mae a Ceneenve Ate) SUCe. vauftows 0. leorIllyttnat the repair ancifor enetelion mum tat oon ID) idemnied in non 4 above and deiented on the reverse of attachments hereto have bee made in accortlence Mtn the reQuillarienta °IP ri 43 ol the US. F Ott* Aviation Regulations and that the iNormatiOn • famished herein is true and Cermet to the best of my Dila • • / Ae '8' 6•Pr /970 ' ''... sure 0l Auye dlndS4dual 7. APPlevel lot Re um To Service Pareent to the authority Lee persons specified Wow• the rdmitined in item 4 mental . jinn was In the TOMx preKribed by the Mintage/Mot Of the Feces, MiadOn Adninntratl0n end Is 43 APPROVED CI REJECTED ' BY Pearl,. Starearcit Immusof Manufacturer . insundonAuthorttation - Omer again • FAA DM*" x . Floss Station Person Kee/WOW nangen Carleas AirmanhInesa &outs OateolApproaetaReeMIon /4 4 ' elef 0 r. 90 Certificate or Designation No. 054842511 L Sig crYAbilionsed Individual / ,C, -;:a /6 0 1 -1.4-7 /2.4-2/1-1---4 wirwailiaz‘a.L." .. • L.. SDNY_GM_02759977 4 a SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246899 EFTA01331362 FAA AIRCRAFT 1E61ST1I CARIPA N0./ N DATER 12 1-90' NOTICE Weight anti balvies at operating limitation changes Visa be entered in the appropriate sorcraft locoed. Amelioration mull be compatible with all prewous initiations to assure continued conformity with the applicable iitworthiness requirements. • B727-31 y well auctin nar onatdyowl regatrithon mart and date *Cy* COmpt•led.) 115001,5 $/N 20115 1. MODIFIED POWERPLANT INSTALLATION TO FACILITATE RE-ENGINE PRODUCTION FOR AIRCRAFT HAVING REMOTE ENGINE OIL REFILL SYSTEM IN ACCORDANCE WITH VA 71000, REV. B) DRAWINGS PER DER THOMAS F. CURRAN NM-383, APPROVED BY 8110 DATED SEPTEMBER 4, 1990. 2. PERFORMED AIRSTAIR INSTALLATION IN ACCORDANCE WITH REPORT 442 (STRUCTURAL SUBSTANTIATION OF EXTERNAL DOUBLER AND MISCELLANEOUS COMPONENTS FOR INSTALLATION OF FORWARD AIRSTA/R) AND REPORT 444 (INSTALLATION INSTRUCTIONS, BOEING 727-100 FORWARD AIRSTAIR) AND IN ACCORDANCE WITH N.D.L. 750-1-002 DATED 9-10-1990 BY D.E.R. BOYD SMITH SO-351. SUMMARY* 1. PROVIDED WEIGHT AND BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS OPSCHECICED AND DO INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT. PAGE. AVJETIDRPORATIa5 UNDER WORK ORDERS 4706 AND 6278, DATED i*:5".or./9 19(.7 . • . SDNY_GM_02759978 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002469(X) EFTA01331363 TAIL AIRCUTT XECISTIIT CAEttA II0.1 N DAM / 7 21 90 totatOPAYLI MCC. WM WENT Of TIW4PORTATICOI—FECSAL AVIAtiONOMNISMATION STANDARD AIRWORTHINESS CERTIFICATE sl:41,444C44•00441 {) 4.440 44411.0444... 14 CAntipor • rociPoitYr., •••3 IMIS.• .the WOO. 1150013 BOEING /27-31 20115 TWJWFWN ...,16650.1/•MCI 1613 fro:: I:U....a on.cio n....0.3....1....,10.OFSMIA4.40•Ma it WA sencorti. ost.lootamotinwns tr4 4 lotto% ben 44044:1440 444 .14. 112 to••• 0 Ole 448 (.444.4614 week ot4 oProl.• tr'd sat*. trieo".0 It% ••••••••tootnt.. DoOsitato 4:0•Vonntira ats•ad haf..totnas 1•01 at aMENbAw. • wC44/0010 1•04110 144. 11414(44 I C444 *seat oocootos orma Nom EM. s. • 6 TEM., 66.0 6 0.1:611066 Von% 6:-...• soSibrat 0441114.4.44 onset Y tennwilo••••• • owe.. saes. w r.• Airmsyster v..• Arnit4 4443 0411402/1 On•Cos• IWO 4.4001.40 60•616.14.160 Y. 01•6610.1 et 06.10.6.64 es . MCOIWC6 ,..taastilainill et ye Foln. AasPeossem osavron. win •••0401. it oi noise> 4 SUS k'...eilop!'• • 1 SDNY_GM_02759979 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024690 I EFTA01331364 • r-iAA A)F:AAFT MEGISTRI Ck,-.ELA IND.7 # Dent 72-27-90 I ;its; sorit A:6O89saa SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246902 EFTA01331365 FAA AlICIA TT AEG111117 CAXTEA RD.; fei DATSI• Zia/ —90 • • ' • 1 OEPARTMENT of TPANSPOIVItgaMITZ CZ/lATIOPIPalllarntATION STANDARD AIRWORTHINESS CERTIFICATE • 1.410.•trIvne ICOISTMTVP. Man N505C P m000. BOEI.NG 727-31 AUTIOWTY NC AS* 'OA 11.10.10C.1 14•4•••••••~fletatSeeluage.....••••Sefilaila0Anill•nAcniltilitloW4.1kniMi $10•01...• •Lteagre ihr • loatI01 hi iSc *Mall IV twit ••••NIN rd loWneSiinst.PreCIPPMAPM.I•Sir Ina it.../..r.t• 14. 011011•Ork NV No Non re.r. new,* •••••••••••• r w 01.001,0 rolsowerweir. • • - patairy AMIN I Oft CC"..0100 a lolorranr C./ at.s.an yam a•O 4010.1.• t. 3 wA10.41 11....14 • cam • 20115 ine. 7RANSPORT • NONE I Tata uo CON:01010 lb.m• scri vireo. wsiev.• two.* ✓. w..Mrm wt t fawn. twessys a... tr.' aineinnspo modes.* OW.* a tap ...ratan sof ninnti• .traes when.. a Nast. ..u.Pes: nen COMO stulasegow 11....went ay. II septet ntiati A “Ipaenn.••1••••• SW. JAY( OF ig$VANCC 7/23/90 iltryaima."•••••agaastolenwdm e.••••••11<sona. twOrnywes nalinbett .; COP to ap..w.onsort.u.nno.-11 Oian, re 7..15 COMMA C IC DISKAVIO TI.L.WCAM T ACCOOIONCE APNallt It Of AM AVATONFILGuLATOOwS FAA Form 81004 o••••• liCtiK500 Alta VS % VINO C. CNINW •••• DiSed.0 0414P/W4A DAR-41.4S-NM ' • ••• • • .4170 c S. • .• _ _ SDNY_GM 02759981 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246903 EFTA01331366 FAA AIP:FAFT REGISTRY CA,JF-A O. s DATE: _ ref. A. !nit ar.• • • _L_ SDNY GMOffc9982 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246904 EFTA01331367 0. 011 % .44 ‘.. 1•06 Ns., •••••••••• APPLICATION FOR AIRWORTHINESS g m .. CERTIFICATE Inlealellella — Pe• m Os Do ea urli• in ••••1•0 eat Tag on fc• /AA ww ally Sun* moo on• •••••••••• CO Peprnenlene H i4c. 'scow AMCION0.0011.Men sltnemen FM *Os lir corn e nom Sec lion nommotAintipW.Aew " T nnAtb:""W. b5o5C Ausatuyenalluielit Ilda•O# Boeing \seen* eltol*z.0M•lattrei 727 - 31 ' 'A' • ell. ••• 69 IAA 007 24:101.0 •. ' S. AICAMT 14144003 .,... 20115 • 0.40.• WA ours NN /maw . Pratt & Whitney • poet .4000. oneOnone J780 - 711 m e P29,5 •••••••• Of •••••••• 3 - A na•ntat is 00 5 NAY* 0••••• IA •••••••••• soaci.o.eyourco st. ArACANT IS Wan • eeeknes) IMAM ArIVCAlliCe 4 NNW Omer Fa (Goa •••••••• Ant - A I STANDAR* mffireaborlia• COUVICAlteleme eibeila I LIMO& I I UTIUIV I lAlaelealet 1114•41001 1 100001 HON:LOOM • YUMA utabilyelbUICOMOCAltreaeins.40005•My `I IWO) . € I PROVOICMM. I woo g esimolaii • COMM • I, • Ale•ClallatO/0007 I F. Cann SOL SISIMICI • ••••••••••• 74•••• • Pa MC=ne* Metw•Alni•410 40 4 0000210014••••••••••••/ • § le no fATIOLL0.0 • VICATNIDO•wrilel a WOO! OF WA* • OTennessen y se sum. se waterlog! I' NAOMI loun.T • I ,g i FO I . IssliOlepoL neon in -•C,> lonesome* • . RAC•4 • Oa Menai 40.4401 NM NSW I I TO SNOW COSIPWOICOWINIPM I war negro.; wet ...truaricsi IMMTliaget O IT maw FLOIT Iilliert &ands • avacuon no. WAOf asSIOad CANON • •••Aires.•lries.v. tee •••••••••• SA is I Of•A•TION •• MAU OF SUIGNA. COUIIICATO) T404-0ff Maar • •••P m . . ' - • 0•44.04141. OM Weer f a I pii0oucncei tuna Tunic . II a.morsua 40.60.6TOATION FlOC3 , C lel MIATVIANIIIISITISNEMCW0Cotla.sUA•OK Ornserf lommees *nog .see e. Melenn e wenTIVID) MOM Moine •••••••••••1••••••••••••• IF SUR, OAP a Audi i latag Foulkstone Plaza. Suite 102 Northwest Holding Corooratioi 1409 Foulk Road, P.O. Box 7138, Vilmington.DE • Ana. UMW CATION4AIN IC ••••••••••••• am 1•••••••••••• same 19803 AMAMI MO/CAMS CM My CUMICAll DMA IMP Ham Al• sal Arran.N•1 A3WE I x •EnegiorrnieSS MCCAW:3 Mew •51 ••••••••••••••••• ea ••••••• IssaADssiAL90 ; t0c0 2- rli ncA9 ..ACOL807LellegiOinen.~0.1, Rev. 18 Dated February 20. 1987 „r„, 5 ......sio C.I4OCIOVirt ortatatiCa MO iiArtIPIMaCI ateore0 *CCU OleCOICON . Toni MOW* MOM 1e WilingliiThlOitillY Mar hike IR a no✓A ..... orWar• •g X Catissaaffh. TI ' 29820 Hours • leis. •,.•..p -0- a COITOCATIO0 - 1 roe . Owl ell Oneellnoe we alesevinamontleares ea Yoe So sop lets elm el 41•111dI es ••••••••••011er Ma innione• Osioneobea en we or* Imo nom /Wain Inner* w1- Ono one same moons.- ye nomeremaolleeineemen memo semen oneetimmtoone eon cm MPLICATION February 2 1040 IT re yyalsan 7 71:14Y: lik noinperino Program & Hanaoer 4 IONIC•On 040•040••0* OS Pam *WIC Tgio NO FOUM) 0.11•0117NY ay etisoble Pe •••••••••••F•Al , rotar...vo In C in I Wpm,' On illtry.CATI .4000.1i0o• 1/4. lc.......a., b p I laminCAZD a re•Onnelles , 11. till w TI (Tint mo b..,...1...,..............c.,..... ,..... ALL arra.. •••••• •••••• • seIlb Alia. Os es stun •••••••••••••• I X THICalliCMCNOlartal, I it nol••••••••••••• Y • _ •••00110(r046.00,FICATIONOF0.101•04T•IANGIOPMO•CM Milt ilIPCATe .1 • ii.41.040I•41•114•111#10••••• fl ier Ilalluall • so IAA 040•Cere EtAA Need/ .• 2 weVOW Crean *Con teen wits f 'fault>. in.. 4--[..,„ 1 ------- WS - 04•••• OU V. 4-!•-• ansy.S ft " I C' a .. . . -. . tvityt - $r - "re -,- Ai n i I IAA NORA TOR 6 YANA Tyne 4. • AA AIRCRAFT REGISTRY C RA O. I N DATE: 8- 15. 90 neer ••••• ••• • ram AtOrtref E. • en"- SDNYfilt02-7r9983 - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTAS00246905 EFTA01331368 lA AIRCRAFT REGISTRY NO. 1 N DATE t 8- 15- 90 IL wimeSACTJUX ... last ... , . - SOUS -- -_ I in niCouCTIONMSOIOM. Ogaftn.M.9 — - .CA.c ."— It 4 3/4 .. - \ b - c .• Nr --.‘ 1 - . I 0.00X1IONCUMOCATIMP4 Kneadm.S.•00......M.A , L.., • A Ti - • n connininisava -: < G 1 " • I; 4 ‘ , 1/ MUM° 0.0ournoltealtatiCol nips I C OW MAMMY OF CeRrintialinameo MR Of OniCATiOix Ka COSMO hirtgO Tinnig NOITIVE Omi rine/ Vomiting Miff/S.7Mo O. anatT Kola Mimi I/004a UAW laelial latinlIATICOI WM ' • O1.101/r4. Of Ivan . ' ainC400104010714.4110•0000 1 CI gam ovinaloi WM TO • . 1 W4 Cogniavng OM ISM.. 1 C ailvolvOunin TO MOOTS T.4 kinigan NOVI War. Into, [ coaLca I loom:worn I prhaiss.ort 1 I 1 wing Arlawfi 004.• *OW ImEnnomoott durvoOP Of NM ntOu•VOONTS PA POW:4ft . ' • - ' • • • I 1 tai; 64:, a tui mason marktrawg tooted° seam red ipmar area • rommort • . . . .. _ . _ . . ., . . . • - • min. tatotil ...am.. in. Nem, fr.simmomeasia .. taVOTCATOS- • onVI color mii I m ihgeOvvm m 4s Wm 00441•40mansomenom ' elpiNVIS ......., v. Masi III -- w noel ,WOO\ sae. . - . .. .... . . Out 10014 NO Taut S. to toot 6M...rust . . .= ..M........... " 0116. Cary illibine MA c, kw...a, 0,..,....,,. Su Ara 2130* Mann *Asa •••••••••/ I X 17: • I woo. mm...... c.,mom s 1•9001..{..41 i >LS C4m.gommili Laing.. men (4.0~•••••••01 1 II COS. 0••••••• ••••••••• IN rum. ~over, .".'es'..." 22 'IMa ..atanSerr 3 Xo.C....1~••••••••••••••••••••ASSIOSAMIlt -2 N err i iTu *a niownwn • E - I. WOW IWO. W /SOW Wiles O OSINO WWI _..nil , A Cur. Aomrtme aim... . moms. ma I. f... n usniniironi• es. at. MI (b) Kau ...nu I UAWsulkosenu v SDNY GM_40498C- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246906 EFTA01331369 cir AA AIRCRAFT RECISTIT RA NO. I PATS, 8- 15- 90 VW= STATE* CS AISCA DEPARTMENT OF TRANSPORTATION • KOOK AVIATION ACAPPASTRAThiOIS ' SPECIAL AIRWORTHINESS CERTIFICATE A SAIEGORY/DMIGNATION / j ,yr PURPOSE Alga . i MANKI- FAG-TOREN NAME ADDRESS 4,10 C fl.NIPC FI:3° .,W aziar D P - ftEcc rais SERIAL NO /Ar BUILDER MODEL 02y; . E DATE OF IEXWAFICE•AtAlrty /#'t,9 EXPIRY /Va. OMNI ISA/TATIONS DAM) ,r E A PART OF THIS CERTIFICATE ming DESIGNATION OR OFFICE NO. • - — . 27 4 WO.'" • .... anosanon. traaace ir tat= IN. coeScarriegtbe runatuti* tg • Ins Ng ••••••10A01.7: ..ronocantni ••:• ap•Anx 3 VON. at coin IRIS CERTWICAT1 MUST IX Oi3PtATIO Oa IRE Al ACC-OACAACE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. • Sll SIKASE SIDE SDNY_GM_0219985 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246907 EFTA01331370 A A This obsrocilsinliscorldwals is 19Sult1 under 11111 sat* of M hen AselitmAr3 Of 1951k up see Fedora, AviiliOn PlOottistion• (PAM. TM elniewihirten een if cateauthertenitternenutechee name:Ion Ile Mine Ws loc0rlduel proijosiion leper lasts and city th, OckCtiort eehl *Ste of ,earls repaired in NS nine. WO B porsOn msy conduct proOscros soN tests unit.' Insi etallfiesis. (11 Goyim pinta or properly lot compensetio.n of hriP 0°310. 121Corryail PerSOos ha saribidloOrriOurPOSOI tem Mont . . .• . , C o E Thissinsociiteces conduits as:bonzes the Hight specilesd on this resomillti0t for Its surpass shows in Bock 01 This heworminisss conilicillireroodres lost n arms Oats onisusneo. Iheeitasn lo which owed nn boon isspricifslionO mound 10 neer Iristechssemerus 01 thes011hersbili FAR- Try sirses11000” no. meet the cetteremente Of Info •PPUCIWO COmOrthenSwit end date*, Itintierthhhale 00de re Phireilled by Arnett 11 to the COreenttOn On IntemetitYleCtet Anehteit No Oman may opal* .the &retell drlOthed On the revoltletele III Ceeept et accottlincetetate What* FAR end In SCCorchirio. isrlh Concsisans and limitations which may be pasted tiy treAdminisirsior as pert 01 Mrs °nice* (2) over any !onus., osontry *Sete the peed prioninion 04 Ina C0 AWy. Unless 100ost surreoileso0.ssisq0000.or revoked rho is mon/Incas soraissto isomichssior Is din hon tad 'ander the eeroltens petterebed n FM Pan a Serlion 21 III or 21217 ' . . • SDNYNA_027599136 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246908 EFTA01331371 AA AIRCRAFT RECISTST C. RA WO. I N DArtt 8- 15z 90 NAT= 0' astAira DEPARTMCHT Or T•ANSPORTATION-910ENN. AVIATION AOMINI STANDARD AIRWOR ESA CERTIFICATE "Ns ,...NNAPTPON 1.4.40 *oh o:••••••••••••• ••••••••••••I 4••••C••••••••• eitneh I• •••••••••.0 • IMIC Or ICS•••••CC Exchange 06 • 1••••• ire IS CI IICA•••• motto,. 141404 MCA 64.1•MabOn NUNIIM WP -FS00 -10 *Lott In • wain. vfl N 011eLATID IN AMMO': IN ACCOID. SDNY_GM_02759987 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246909 EFTA01331372 ?AA AIRCRAFT REGISTRY C RA NO. 7 4 DATE: 8- /5- 90 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246910 EFTA01331373 AA AIRCRAFT REGISTRY C. ZIA WO. 1 N DATZ: 8- 15- 90 • — . UNITED STATES OF AMERICA DEPARTMENT OP TFtANSPORTATION - FEDERAL AVIATION'AOMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE 1 CATEGORY DESIGNATION Pt; RPOSE 8 AN,. NAME OM AR 000mu C •LIONT FROM TO 0 N- OW/0EN II 14000 . DATE OF ISSuANCE e I • E OP T ON V 0 2 FART OF THIS CC ',TIP MAT( VI o No DONATION ON OFFICE NO. R t.• --- DAR-48-AC-IIN As sralamo• onalm•shileelbas AN be 'mans N. IN ow NamElism Er onsAaramm madly 3 ...mose TOG CERTIFICATE MUST st DttmAyto 04 THE MICA/0TM ACCOADOia WITH MI AMAIION 0120ui roost SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024691 I EFTA01331374 AA AIRCRAFT RECISTRT ERA NO. 1 N DATE: 8- 15- 90 A TSS Mt artifice Avietimi s Reed l an le sailor* of the Fate Aviatioes'Act of IN of the F ral ece (PARh. B ml. ewes gee authorizes the menufactern mewl es the roe 61e to con. duct Fief we DS: Mk ea ce Weak* Welt a of *bath ressesi la his mete. No pee eftey edam proclortIon Matt teat vet this catillkste: 01Canying pet- was or p competIon as hie: atiffee (2) CliffIRS Pme eel tette to Od pep— of c Tab tenrcelltire wilifIcete 'those the let eptichled cm the me aide lot the pm. pow the la Block A. n, •-• Tit eremites oertitlate cadre% that,. es of the On of hatmee. the ties l to which burst hes beta Wreak, ad led to meat ti. reiremeats of the applable FAR. The deft don not meet the niquIrementt of the tippet& compteedve and clouded thi- rookies cede as pewit.. by Amex Ito the Commotion Os latereationel CIMI Mese. No pence may copes the diet dewed co tise tan We: (I) except In saccade with the applIcebk FAR and in eccodtace with comillikos and balutIons which may he prescribed fey the AA meet Ike centres; (2) ewe my fore misty teeth pot the epee penalsion of thet matey. E Unless tomer winederad. eameneed. ot levet. this itiniorthbas renifkaM is elTecelot fat the thine ad toe the cordlike. prescribed la FAR Part 21. Seen 21.111 or 21.317. SDNY_GM_02759990 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246912 EFTA01331375 AA AIRCRAFT REGISTRY MERA NO. I N DATE: 8- 15- 90 Manufacturing Inspection District Office 16501 Sherman Way, Suite 200 Van Nuys, CA 91406 February, 2. 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 _ REG. NO. N505C THESE; OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. no person may operate this aircraft for other thaerthe purpose of Show Compliance with the FAR's to accomplish the tests outlined in the applicant's program letter dated February 2. 1990 describing compliance with FAR 21.193(d). Additionally. this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91. and all additional limitations herein prescribed under the provisions of FAR 91.42(e). °. All flights shall ,be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi River, on the North by the U.S.A./Canadian border, -on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles front the West Coast of the United States of America. . • . 2. Base of operations is Palmdalegincaster Airport, Palmdale, California and secondary base of operation to be loses Lake Airport, Moses Lake. Washington. f 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book-endorseienf orposseli a 'Letter of Authorizattorrissued by an FAA General Aviation or Air Carrier Operations Inspector. A. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. This aircraft shall contain the placards; markings, etc. required by FAR 91.31. 6. The cognizant FM office must be notified and their response received in writing prior to flying this aircraft after incorporating a major change as defined by FAR 21.93. 7. This aircraft approved for day/night VFR/IFR only. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246913 EFTA01331376 taletArr lumina ERA NO. / A. DATE: 8- IS- 90 Federal Aviation Administration Manufacturing Inspection District Office. Experimental - Show Compliance with FAR's. cont'd - • Page 2 of 2 8. No °aerations shall be conducted over densely populated areas or in congested airways except for takeoffs andlandings, and when under ATC control. ,9. No person may De carried in this aircraft during flight unless that person is essential for the purpose of the flight. 10. This aircraft is prohibited from aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved.by the cognizant FAA office. 11. If aircraft, engine or propeller operating limitations are exceeded, an appropriate entry will be made in the histofical records'. ' 12. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). These limitations will expire on August 1, 1990. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246914 EFTA01331377 pen OttIce: - Febrti1Py 2' 1990 - . %OS LonsseAchSivo.#206 TO Fax Mr. Bud Martell, Manager. Federal Aviation Administration Manufacturing Inspection District Office .16501 Sherman Way. Suite 200 refer to Van Nuys, CA 91406 001020290 Subject: Application for Experimental Airworthiness Certificate (To Show Compliance with F.A.R.) - Gentlemen: This letter is to infone\you that'Valsan intends to operate Boeing • 727-31 , Registration N505C, Serial 120115 owned by Northwest Holding Corporation. Foulkstone Plaza. Suite 102. 1409 Foulk Road. P.O. Box 7138, Millington, Delaware 19803 in an experimental flight test program. The flight test program is in support of . the Valsan JT80-219 Re-Engining Program TIA NM-100S-1320. Tents and conditions of the Experimental Airworthiness Certificate are as follows: . Valid for Six (6) months from effective date of the certificate. 2. Geographic area is the. Western United States of America. Operation of aircraft will be in accordance with all . applicable F.A.R.'s and F.A.A. 8130-6 (attached). 1. Aircraft to be maintained in accordance with Federal Aviation Regulations Part 91.169(f)(4). a current . inspection program recommended by the manufacturer (Boeing low Utilization Maintenance Program). Very truly yours. R.A. Broulik Valsan Program/Engineering Manager C/O - Rockwell International 2825'East Avenue P Palmdale, CA 93550 Attachment RAB:Ig SDNY_GM_02759993 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246915 EFTA01331378 . 74matitsin itztittitt th ifts. NO. 1 N . DATE: 8- 15- 90 ro,9!cb s.r‘!.91:rr n r. r • ", ✓-;64.1 km44; SDNY_GM_02759994 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246916 EFTA01331379 AIRCRAFT REGISTRY CAMERA NO. 1 ?V DATE: 8- 15- 90 us otyurnovrr or IllANIPOWANCY. flOCRAt. AVIATION AtOMSTRATKIN i SaMOSIS MAMIE RPM AND ALTERATION . POI FAA WI ONLY (Airframe, Plwerplint, Propeller, or Apr,liana) OITICE IDENNocAna. • ' WP-PHX-FSDD iNstRucTIONS Prod or type ell eon,. te FAR 410. INA if Append., 8. aed AC 43,-I (Ore Natitent ~in For inoraroont tad dispearoon of 'his form. MAXI .TIC/Oft . • BOEING 1 27:.3 I. AllaAFT ISTRIA1 NO, sNATIONAWY NW liCASTRATION Man I 20115 . ,: T .... • I. ME '. t ~St iota . I Ms twat a at tatintertettationalot otO • 1110Eftat y rt A. AGENCY'S .4&491 ANO ADM» L MO Of AGENCY • • . C. CIETOICATE NO. v... aitICAreir ratoot DYNAIR TECH OF ARIZONA. INC. rot. Orr Cirttiart 'Otto .CRS .407-36 3737 E. BONANZA WAY. . . ciamcas isle raw» • AIRFRAME IV PROENLE, ARIZONA 85034 - 0. I cent that rho Nepali eat of al ttttt too sat to the larrila I ;totaled to too 4 Ate sad diKeted on the 04 •nKhee•µe taco Ito St sat in Ktlledaµo oat. the requetotts of Pan 43 of the C.S. Tittel Arena» Itigulation, utd that the Ifi4011•4400^ for ea bed boron is owe e d torten Ira the trio of at kroNNYEEY. GAT! SIONANIII Of AWINOIIIMI INDIVIOUACR . • . • a„,, - AUGUST 10; 1989 . RENNETH ROW80111AMkr ; — fitinaaas nit Natty One peract riaortd bolot the old °tote' in ore i on curd ao the eater proontod,br tio Alsielarnot of do ION& Ansoor, Aonoroloo NE i• APPROVED htlft . laf NA fat total onnoNCIVISA ~KIP orntatrsON . IN No osmor -. GA11 CO APPIOVAI OR ~KATE OE Ø ING4ONATION NO. 1111.a 4g , al AUGUST 10, 1989 CRS 407-36 SDNY_GM027&D9 G6~ SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246917 EFTA01331380 AIRCRAFT REGISTRY CAKtRA NO. 1 IV DATE: 8- 75- 90 it- 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 (II more space is required. attach additional sheets Identify with aircraft nationality and registration mark and date work completed.) • 1. FABRICATED 6 INSTALLED REPAIR ANGLE ON LOWER EDGE OF FUSELAGE .SEIN FOR NO. 2 ENGINE SIDE COWL AT FIREBALL SUL/BEAD 'APPROXIMATELY PS 1455 PER SRN 51-40-4. 2. REWIRED CRACK AT RH HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY STA 78.3- , 88.8 PER SRIC55-10-3. 3. REMOVED CORROSION. CUT OUT BULGED AREA IN EXTERIOR FUSELAGE SKIN. INSTALLED DOUBLER APPROXIMATELY FS 1157 AT STRINGER 27R PER SRN 53-30-3. 4. REPAIRED FUSELAGE' SKIN CORROSION DAMAGE ES 1166 - 1174 AT STRINGER 271. IN ACCORDANCE WITH BOEING REPAIR MESSAGE NO. ISPN23200D. END 0 12011001 SHEETS ARE ATTADIFI) 6 COvir MMMMMM TtriC orricg. itl4.6.16.631/ NMI ighigtar t gaW S ea 'SDNY GM 02759996 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024691S EFTA01331381 Vasswie....~.me AA AIRCRAFT RECIStRT RA No. 1 N DATE: 8- 75- 90 • 1/4AA US DIAUTUNIO Of IIIANYORTAION '. ' , • IltDCRAL AVIAT/ON ADMINISTRATION 4 eprit.artffiå den` Fewer ~N • ed ~fen Nor. Os-IMO, MAJOR REPAIR AND ALTERATION FOR 41.44 LIE ONLY (Alrfrems, P•vearplaM, Pa/pollen, or Appliance) VNY FSDC "a pwipkinnif.—_ IWI CH4 rs -05', onyaoot ONE: Prim ar gyp. di sewn. In FAR IIA/. FAR 41 Append% S. sad AC 431..1 lei aubenwne nr.i.Na Sawn for Inetrandien• Ned dIspnelMan et Ihb fern. I. AIRCRAFT /Ant RECEIVED FM imam BOEING ' • 727-100 %east 1990 . MAY 0 ii INATODNAM AND REGISTRATIpN MAU . 20115 N505C !ADDRESS F. WANE /4,8 Maas An totein/Nan ortiAnitumy Fspo IN aaln... •I;an 4NIAtoN) LIMITED INCORPORATED ' I ' . • • 1 4387 InternationalSateuaX -• 'Columbus, Ohio • 43219 . 1. POE fu USE ØT • • 4. UN( ID1312±Wle S. TM We ~0 i MIA. 9BO• «WO &Mt , Anon AGNAJAC A* duscried own I X in Wen) POLVERNAIR X PROPELLES AIMUANCI YIN • • manniviili e 4. Clili011UTI STATEMDIT • rase A. AGENCY'S NAIVE AND "MSS S. KIND Of AGENCY C. CERTIFICATE NO. North American Aircraft - . .. .. 44. CittOIWIO oLOCM.41,0t t11;;EgW e PhiW?)1Int Class 3 V NXAR688K Rockwell International Corporation weep. alrtnicann asaInmec 2825 E. Avenue P • ' amscane mom, 'NNW Palmdale, Ca. 93550 aswinanvere D. I nnify WI the Link ai/d/as dramatis-Ns& ea snaeltmws Mine Mn Ina mule fa Arandanet aids and that on laktafinIaa twalabod Awl. In tn. and the ualiN) id...Lila in INN 4 awe en &mint ea the wen* et IN requltasent. of Pan‘ips et abe U eraI Aviation Rtgulstiont coma Is Ma Rest el donne...Wu. DATE . . MO .2Y n9d • SIGNATURE Of AU114O# FDI D. A. Perazzo • .• å 1. DUO ,m POE *Max 10 servi , ~own ea the W4 baler W nit ryriied le he 4 watelt.rd fe. W sa....,er pr..cRim i by • MI• ASNIILENNNted i enatekra nZIalslatimlen and k APPAOVED RE) i ST IAA fit.IITANNADI ACIFICKM awasiesa aVIDIETIWALINGNIANON Ewan elesan I IAA SSW Yaw. ttanON Eameill •ILLSLANA l Of TWINGE, DI MOAN DATE Of ATTIOVAL OR 179:2 1;1 r? V /9q,f) e-- e-- _ CIIIIINCATE OR DESIONATION EC NXAR688K SIGNATURE AUT ED INDIVIDUAL • - a,-.. .....v.....,c41. SDNv GM_02759997 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246919 EFTA01331382 sorii ikoff994 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246920 EFTA01331383 ?PAA AIRCRAFT REGIS/MR CAMERA BO. 1 N DAM 8- 15- 90 NOTICE Wiight and infante 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 alnvorthiness requirements 8. DESCRIPTION OF WORK ACCOMPLISHED (IF more space is required, attach additional sheets. /den ti y with atrcra/t net/dn;lity arkt registradon mark and date wVv/t completed.) • • .. • A. Modi Model 727-100 , Serial Number 20115, in accordance with supple- ' menta, type certificate SA4363NM. .amended- September 1, 1989 as follows: 1. Valsan-Boeing 727-200 Re-engining Document VA000001, Revision F, dated January 15, 1990. . • 2. The following drawings and engineering orders (EU's) are in addition to the above document: NOTE: ' fliAs denotes Valsan Dealing. a: Chapter 24 ELECTRICAL POWER • A240000 A Electrical System !esti. - Strut E.O.: 003A,'101 VA240007 E Panel-Load Control Center Modification E.O.: 003A, 004, 005, 006 b. Chapter 28 FUEL SYSTEM INSTALLATION STRUT- - A280001 B Tube Assy - Fue Strut Feed Thru E.O.: 100 c. Chapter 48. MISC A481100 A VA481200 C VA481300 C VA481324 NC VA481325 NC Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame AssyoSta 1263 E.O.: 101. 103 Fuselage Skin E.O.: 100, 114A, 114, 116 . Intercostal Assy - BSTA 1223 to BSTA 1243 W/L244.39 E.0: 106 Intercostal Assy - BSTA 1223 to BSTA 1243 W/t234.06 E.0: 105 d. Chapter 53 FUSELAGE STRUCTURE VA530001 - B 'Ballast Weight Instillation E.0: 100, 102 VA530003 C Ballast Weight. Support Structure Assy. E.O.: 002,100 VA530004 NC Ballast Weight Instl. STA 312 - 360.E.O.: 002, 100 e. Chapter 54 NACELLES & PYLONS A543000 C Main Strut Assy (Sh. 1, 2. & 5) E.O.: 003 VA543100 0 Firewill Rib, Side Engine E.0: 36A, 003A f. Chapter 71 POWER PLANT • A/10000 NC Power Plant Instl. - Engine Pod V727RE (.0:: 002, 1058, 109, 108, 001A, 104A, 005A. 004, 110. 003, 111, 006A FUEL AND CONTROL • Approach (Rei. IM), dle 003(Rev. Solenoid W iring Diagram E.0: 002(Rev 002 VA732303 0 Relay but'. - Approach Idle Solenoid E.O.: 103. 003, 1008 VA732304 Switch/IND Light Instl -.Approach Idle E.O.: 002. VA732310 A Switch Instl. - Nose Gear Position Approach IdleE.O.: )03 VA732315 NC Relay Instl. Pilots Overhead Panel E.O.: 140, 002; 101 NTROI, ngine Controls 'Intl. - Strut E.O.: 002A Drum Instl. - Eng. Controls E.O.: 100. 101 Bracket Assy - Pulley ESTA 100 E.O.: 105 g. Chapter 73 ENGINE VA732301 K Chapter 76 ENGINE 9A760000 A VA760014 A . VA760015 A ACCIIIONK SKITS A17/040 •1/.11•00VillIMIIIST INVINTIOIO Or net me 4111.raligrin SDNY_GM_02759999 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _0024692I EFTA01331384 , %- . , plrevriSairrl " • -5*.41.‘ smisacoatio SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246922 EFTA01331385 DESCRIPTION OF WORK ACCOPPLISHiD (COAtinUeN) Serial No. 2011S i. Chapter 77 ENGINE INDICATING VA771005 NC Indicator Engine Pressure Ratio EPR, J. Chapter 78 ENGINE VA/80000 B VA783010 E VA783011 F VA783013 D. VA783017 J VA783024 B VA783028 A. VA78310I C Chapter 91f.HARTS VA910002 A * VA910008 NC EXHAUST Engine Strut controls Insti. E.O.; 002. . Flt DecknIndicator Testi. T/R Sys. E.O.: 003. 004 Thrust Reverser System Wiring Diagram 402 (Rev. G) Support Bracket Assy - .T/R Control Valve R/S E.O.: 100 (Rev. 10 Placards E.O.: 007.. 008 Relay Instl. - Thrust leverser Control E.O.: 003 Mixer, Exhaust ‘. Inst1. 727E 100 NO: 2 Engine T/R Wiring DeaCtiviation E.O.: 002 • Inst1. - Electrical Wire Harness E.O.: 003. 004, 005, 006, 007 Wire List V727RE E.0.: - 00.1, 002, 003 *New drawings added to modification. .8. Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989..: Subject: Fuselage Station .1182 Pressure Bulkhead Web, Crack Repair'and Preventive 1 Modification C. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Manual D6-21200. Weight and Balance Manual Supplement, VA-CR279 is attached:. SDNY GM 02780001 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246923 EFTA01331386 ,FAA AIRCRAFT REGISTRY CAMERA NO. 1 N DATE:. 8- 15- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246924 EFTA01331387 IAA AIRCRAFT REGISTRY - kg.AuggA No. / N DATE: 8- 15- 90 41 r . 727 - 100 / 200 Weighing Form . : .7.4.144krgt:‘ . . 1:e2 r' ict i 'a:. Dote ' Model 'Serial Number Place Weighed eohniclan: 1 4/18/90 727-100 2011B- 8505C EALMDALE POLE" REACTIONS SCALE READING . . ..:, TARE NET WEIGHT, ARM 4 .49. 1* 6 Left Outboard' Main 24402 it 6 244 10: Left Inboard Nolo 21066 21_ 2186 ' . a..drale...s..trre..1.... A. 0 - 4' la ,..v.J.:,-. 4 Right Outboard Main 23687 • -4 • -4 23603 c ...-: .. Right Inboard Main 23381 -.-, ''• 23304:U ail a % -...mie.a.....i.ipildr Pd. N Taw e ie Subtotal (Mains) 93335 : H - 7 93342 A 4 .1 688101 CAMatriLIE,Mt$ AWID::: ' Left Nose 13351+ n 0 1339 Right Nose 1498 0 14 8 en- ..dde..2-4.*,,,m.4.4r),41.2- - .‘vh... Subtotal (Nose) 2837r, 0 2837 s 311 2 ,-ma-4.emosna--4.144:e"vemsracavaric: V- . , TOTAL 1 96172 'ar.f. 7 9617 931.20 89 9364 . 'zt 1155, 4 c..., LESS .41 .,.. .1, Items NOT pare of Basic Weight Iiii ,-;:::!:.. t 4, 1.76804 PLUS EAL iv .710.1maz,drpkt41,0141,1,, ,x. r er 1-..feh:i: s * !' Items part of BasiC Weightl:ut not Weighed I zee -1 208347 AIRCRAFT BASIC'WEIGHT 96278j 930.651 38.991 89600897 1....iwactipt.i‘vfa c igro:4.7'31W- reaMinfielillihaAN....td 7,calpett z. . „.., .1 •..., E, 2 ?.•••7,-..4:...1.:: ciSteiNVU.4*.:05b(411740:61 CORRECTIONS W.-:,e1,i6c1 'i 7 : .. lei? . ,r.,,,1 MOT Part of . Basle WekOht Items NOT weighed but not i r et' Basic Weight Description Weight Arm 'Moment Description Weight Arm • Moment Usable Foal Orelosetlerunnable 7reee•i1 177.0 1001.0 137277 'feel --- Ind Tanks 171.0 9111.0 110002 Intim Inlet 0119 92.0 1100.0 Se$00 27.0 407.0 tetra Overige*. I I 17.0 - 1031.0 Wien 427 9290 1017 ''. ' eel 14119 Cl) 41 0 On 0 tOTAL. . 188 176804 Total . 264 208347 fr, -“. ...e..!:...:• ;:: :. z.z.:-... t... - !...1 ''.1.,4• • ' Itri afriA 1 _,,,.taj ,4:ii 4-n-ii-..vr - i* ,-... - moans •• r 111.12 • (MI) Olsten fl aw the 319 point to The mole ale centerline 210. 11 a (MI) Dineen* between tie 1•14'ncee sale centerline and the 419 point. 115.05 a (MO) Meters t.t.na the flint nese Salt centerline and the Pa point. 110 .90 a (MI) Oletellee free the reference Sam two the Cie point of the aircraft. 960.12 • (A) Ness eau llosalert . A a NOM . 311 • tin ens /ale Mallen e • 111•(42•111)/2 . er, "-^ lit e; ' -4.E.A.'1‘, ' T' REMARKS e.le.,:'•,....,," - • ras..3 r - . 'Alp..! 0 •:,• • . ,... 1.. The aircraft was weighed in a level attitude and in an • ...c • enclosed hanger,. 2. The wing panel jack point was used for the aircraft Jig point. 3. This is the summation of 'the 3 weighing°. 4. Baseline Weight Results for Post Mod Flight Test, dated 4/18/9D. . . SONY .61.132760003 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O246925 EFTA01331388 eNr-r••••••Sailrorr",osar cr. SDNY GA4_02760004 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246926 EFTA01331389 *PAL AIRCRAFT REGISTRY CAMERA NO. / N DATE: 8- /5- 90 Model ri•I /27-100 Left Outboard Main . Left Inboard Main • • t Outboa Main ght Inboard 'Main 727 — 100 / 200 Weighing Form Number Place Weighed 0115 9505C •ALMDALE SCALE READING Subtota (Mains t• 93329 'urn. Left Nose 1340 Right 'Hose 1497 ubtotal Nose 2837 96166 tees NOT part of Basic Weis PLUS Ai-44r4,4:-4y teas part of basic Weiat. t not Weighed echniclan FOLEY TARE NET ARAI WEIGHT I RCRAFT BASIC WEIGHT 1Atfitlitt -0:74.. 23378 93336 96173 • 950.12 it 311.37 iltririTfr.Wirli. 332 CORREcTlogg AV NOT Part of Items NOT weighed but Part of Basic Weight Basic Weight Description Weight Arm Moment Descr ption Weight Arm 00.11 • (Ng) Distant* between the left roes axle conterl no mad cm Jig point.. gill.•5 • (10) Distince between the right nowe'ons center Ire anti the Jig pint. MOMENT 883357 89563757 0 89563'57 Moment 530.10 • (II) Distance Ira the reference datum to the 31 point of the aircraft. SSO.12 • (a) Mein MU Unction A • ADM 311 .371 . (I) mss. Ail. ancessft a • DI-Ottwant REMMUIS WI; .1. %-p- :5-1/ • Rif/ tit$ 11.V.H ' 4 t. The aircraft was weighed in a level attitude and in an enclosed hanger. 2. The wing panel Jack point was used for the aircraft jig point. 3. This is weighing 1 of 3 SDNY GM_02760005 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246927 EFTA01331390 •vass-c-302.-- r stseibW. • - - - - — — —• • — 7,4 SDNY GM_0276u006 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246928 EFTA01331391 Wok AIRCRAFT REGISTRY CAMERA NO. 1 N DATE: 8- 15- 80 • SDNY_GM_02780007 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246929 EFTA01331392 sserVilattRWSlagell,behrit--, SDPit_GM -627606CTS SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246930 EFTA01331393 FAA AIRCRAFT REGISTRY AMEBA NO. I DATE: 8- 15- 90 72 7 - 1 00 / 200 • Weighing Form ,x l tI.V4 -C7976 -. 4:4 Dote . Id 8.411•3 Number Place Weighed Technician , 4 18/ 0 - - N505C —\7ALMDALE FOLEY 'REACTIONS .: SCALE READING 1..4 ; ' x ...414 TARE NET WEIGHT ARM . MOMENT Left Outboard Main 14401 t . !•4 6 24407 Left Inboard Main 11882 _ N i,1i 2 21864 ; ° Right Outboard Main 23688 , - -4 23684 Right Inboard Main 23388 23391 5 . Se h-lt.Ittiitilain;) . —" Bait/ 7 93346 a 950.12 88689902 Left Nose Right Nose . 1339 a. 0 1339 . .‘‘ 4:,,I. 14 0 4 74J . 2, ,., r, .: Subtotal (Nose 2834 y. 0 2834 5 311.37 882423 r . t. • ' -• Ars. A. ♦ • . -s Y• •N, r, „, ,t„ n' n3 , .. TOTAL 96173) eicrila 1 96180 931,30 69572324 ' Lar -1143,;44:7ghjel: 1441a14 3-4. 4:. : 'teas NOT part of Basic Weight I o o PLUS I i. ,T,-.0:44.(26,71”0,2:614-1-4.'...PeOce" . tees part of sic Weight but not Weighed °I ' ' '1--- o AIRCRAFT' BASIC WEI I 96180 031.30 39.35x 89572324 4,7 1:1,t$47: W eTt c ..tc:‘ 7,1 .. i 2S1 ' 1 ' ' W 1:3 14 ".)5tItrE : - ! . .13 'V et' ,1,41”..\ . CORRECTIONS .79, .. t.t.._ eTt [email protected].,,rf .• NOT Part, of Swan Weight , Items NOT weighed but Part of Basic Weight fleacriplion Weight Arm Moment /Description Weight Arm Moment `,T 1 . . 1 :41‘14. '''y;.a•. . liEASUREKENTS 0 TOTAL N r ii est r5 .1l 7.1 II• 42 • OH) Distance trio the JIG point to the thin axle caritorlIne Sg0.11 • (Nl) Distance totroon the left now axle oenterlino and the 34 point. San • PO) Diortarce Mthion the right roes sale centerline and fp, Iii point. SiO.O0 • ell) Distance free the rogiirinico ata to th• 31, point of the etreaft• 960. t2 • IA) Slain ono ...mt••• • . moll . 311.37 • (I) ogee Axle wafts • s 51-012•10)/t Y4i... ••ier“: 1/4 ,,,i4 a v REMARKS Li • a -. -k,„c-..... .A.p, ca,$.4-zatargc...4- - 1. The aircraft was weighed in a level attitude and in an enclosed hanger. 2. The wing panel jack point was used for the aircraft jig point. 3. This is weighing 3 of 3 .;•ts SDNY_GM_02760009 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024693 I EFTA01331394 • '‘,^'•"" SDNY GM_027(0010 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246932 EFTA01331395 FAA AIRCRAF REGISTRY CAMERA MO. • DATE: 1- g9 c„,„..,,,,„,,o, WNW PAIALA).. ADALNUTILAIION 4,sfec..,... 04-R060. I MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY (Airframe, Powerplont, Propeller, or Appliance) na l--'4 e INSTRUCTIONS: Enos or type all snows See FAR USA. MR 4, Appeadin ft. and AC 15.9-I See subsequent 'TANN Turd) for isstrucnoni end disposition of ebb Eons. I. AIINPAFT DAME Boeing - . ACM 727-31 Mina NO15 . 201 NATIONALITY AND IIKILSTILADCA4 wee N505T NM (As Penn en rogietiOhts tertiRosiNI ADDRESS (As than co ) T. Orli Tenneco Inc. sg)serotocs 16951 J.F. K. Blvd. Houston. TX 77032 I. FOR NA ISE CORY 4. UNIT IDININKATION 5 ITM win no. NAM ALMA mica. AINSILANLE 'NAL I &ANN - xx (As thoothod - powwwa TM ' IT MATING A noeticrs NAME MM ACCESS S. KIND Of AGENCY C. CEIMFICAll NO. Tenneco Inc. 16951 J.F.K. Blvd. Houston, TX 77032 . us. ONINCALTO ANKANIC . 205-10 • fOltO644 SeenticAsto ANNUM CIONICAIVO WAN AIMION OINIVPACTUNIt D. I rosily that as mob and/cte idteretion sae to sesebseiencs Nebo base bees bade in istordosee sich end ma the informasion furnished herein is tear and the NOUN identified in itemising,. and leScribed ea tilt mint er at reqsireesmis of Put 0 of dm US alml Avinko Ilatmatbm (O MR CO cbe bes or try knowledge. DATE . 04-04-85 SIGNATURE Of ALTIOVED INDNIDUAl I .110a•- it ,_ -gii i--- 7. WNW FOR El= TQ Silvia 'cumin coo. falforict firyen. Roos Verified below the snit identified is i..., I As, •••LLA-.....1 A IS. •s..... pin:sr...I S. the Adoiaistruor of the navel Aviation Ationiantistice end it ®APPROVED °RUE( ca) 0.4 Re PASS 06.1001 ofeenfaumet itarealom eimioaranine _ — OM* flow', NA INNONN X ISM SPOON wog*. Olitattrailid Or ITarelIOOT litY6C1011 OF an DATE Of APPROVAL OS leKnell - 0‘85 . - CSIMOUE 04 DISIONATION NO 20510 . - SIGNATURE Of AUTHORIZED INDIVIDUAL ..24ft.... t -re-sr FAA Fens 227 17-671 f 83201 SONY GM 02760011 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,15, and 17 EFTA_00246933 EFTA01331396 NOTICE Weight and balance or operating limitation dsonges shall be entered in the appropriate aircraft record. Are alteration most be compatible with all previous alterations to assure continued conformity with the applicabli airworthiness requirements. I. DEXRIPTION Of YAM MtOliftISIAD (If more space is required, attach additional sheets. Identify with Mr. craft nationality and registration mark and date work completed.) CREW AREA CHAIR INSTALLATION I. REA0Ved folding.couch from L/H crew compartment station 400. II. Installed (1 each) Tosington 71150M24 F/A AFT facing single chair on sliding rails from station 420 to station 180. ' III. This alteration was completed in accordance with Threshold Engineering Company of San Antonio. TX. drawing 0270 and instructions identified in report 0259. IV. All engineering drawing and reports were drafted and approved on FAA Form 8110-3 by J. A. Dugelby D.E.R. (designation number.SW-256) and are available to the administrator on request. V. All work performed utilizing acceptable methods, techniques, and practices per AC 43.13-1A. VI. Aircraft weight and balance amended, 0 ADOITIONA3 SHEETS ARE ATTACIIO OVi ooroarrain rowing Iona rm-rneratom 'Pr • ' • SDNY_GM_C0000i SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246934 EFTA01331397 SDNY_Gtd_02760013 wax Isamu teXtu. AriAnON ApoicensinON MAJQR REPAIR AND ALTERATION Alcfccone, oseerplool, Propeller, or AppliOthal) , .. An badsifletti S. 0.-/OMOI POR FAA USE ONLY OFFICE IDENTIFICATION .....,4,0.45, INSTRUCTIONS: Pint or sype all entries. See FAR 41.9. VAR 4) APploti D. ANI ACR1-9- 1 Co. 066640mM id•WOO S fir Seaw:Owss sad disposition of this form. I. NEM Nan Boeing • N4(41 . 717.-31 • NSW NO.2011•••••4 .0- . . . NATIONALITY' AND REGISTRATION MARX ...1 N5051 SIN . HARE (As dam en neelereeien esirlattthal •-•-' TanneCIP Igo ADDRESS (As d an negiereeics ceenEctON • 16951JIMBlvd. • , .Bonston. Texas 77032 • • 3 RR MIZE OKI • ••• ddstsdools• seethes stn. proona SO. aimo$0.• - . . dre.464•••• tollsOsorms .n it .slur! re. Ins as.' encore own soften is etorresily .nt ono:. se oases • 4 , •••••••664 6 ••• 6- Oa ..• • • • /.2_.r. - Ode 4. T INIMDCATICel 3. TN - . ? MOT ' SOW WO. MTh. MOM ARAM! in dee 1 • II (As chiscitod above) • PO%VENIANT • • . Pal* • • Tine AMAMI MAMPFACWPItt 4. 0NF0UNIT WINE A. AMID'S HAM I .110 ADDRESS I. *ND CO A00401 C. °INTRICATE NO. Tenneco Inc u.s. armeicAno asionsiE 16951 JIM Blvd. melon Ctema1tp edlirsgANIC HOoRtoo, Tx. 77032 y asiltrUJCIS MACS 11571051 205.14 . OintUfACIVIde , D. I certify thee the repels Nadler Abandon .Me re •Ctoctsimetit. Invite ban bee rode is words< with sad that the lefonnaiise fenisbcd heeds is true and the nairity ideno6ed in k4 4 than sad described es the recant of the reiltdreasems of Pan 4) of dee U.S. reinsil Aciadtha Revelations menu to the ben of by kzewledet DATE • • - . ' SIGNATURE Of reit 7. mnv*t FIX unit 70 R1fl Penned to die endeethy_plyea pussies specified Slow the aniigniiiied injele 4 ...Sal .n site mum, rent:bed [truncated]