EFTA01329414.pdf

`Oral No 2120-0020 EMatenc ' ,sank Hint*. Exp Sal /2014 MAJOR REPAIR AND ALTERATION e el? (Airframe, Powerplant, Propeller, or Appliance) Fa FM the arty US Doormen ol turepottabon Nan/ Avignon Admislettifte 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. 44701). Failure to report can result in a Civil penalty for each such violation. (49 U.S C. 46301(a)). Nationality and Registration Mark Serial No. USA N722JE 760750 1. Aircraft Model Series Make S-76C SIKORSKY Name (As shown on registration certificate) Address (As shown on registration certificated AC4ens 610O Red Hook (Nana. 10 2. Owner Hyperion Air LLC City SL Thomas State 20 00F02 Country USA 3. For FAA Use Only • 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. • ISI AIRFRAME _....._......___ ____.-- (As described in item 1 above) • O POWERPLANT • O PROPELLER APPLIANCE O O itivackew & Conformity Statement _ A Agency's Name and Address B. Kind of Agency r Manufacturer International Jet Interiors U.S. Certificated Mechanic I C Certificate No 2221 Smithtown Ave Foreisn Certificated Mechanic Ronkonkoma, New York x Certificated Repair Station CRS I1JR439Y 11779 USA Certificated Maintenance Organization I D. I certify that the repair and/or alteration made to the units) identified in Hen 5 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 15 true and correct to the best of my Au knovAed Extended range fuel per Signature/Date of widual 14 CFR Part 43 O INSP App B 001 Jay Masser 8/272019 7. Approval for Return to Service _ Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Adnwiistrator of the Federal Aviation Administration and is n APPROVED O REJECTED Persons Approved by Canadian FM FN. Standards Department of Transport Manufacturer Maintenance Organization Inspector BY Other (Specify) FM Designee X Repair Station Inspection Authorization Certificate or Signature/Date of Authorized ual Designation No. INSP 002 CRS I1JR439Y Thomas Norden 8/27/2019 ^ FM Form 337 reek SDNY_GM_02757629 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024455 1 EFTA01329414  NOTICE Weight and balance or operating Imitation 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. IL Description of Work Accomplished (If more space is reQuirad. attach additional sheets. Wordy with 011073n nabonakty and registration mark and date work accomplished.) USA N722JE Dote Nationality and Registration Mark 8/27/2019 I) Reupholstered the existing Divans (Outer Cover Only) with Cowtan & Tout Fabric: 1.8905-07, EMI Silver. All PAX seat belts have been rewebbed by Aircraft Belts Inc. (FAA/CRS # YBIR632K) reference Certificate of Conformance dated 8/9/2019. 2) All PAX Scat Cushions have been fireblocked in accordance with FAA Title 14 CFR 29.853 (a) Amdt 29-23 and Part 25 Appendix F Part I (a)(1Xii) and Title 14 CFR 29.853 (b) and Pan 25 appendix F part II requirements. Reference Skandia Inc. FAA/DER form 8110-3 (attached) dated 08/21/2019 (Skandia TP 28191 Rev A dated 8/21/2019) by FANDER Mackenzie Kacvinsky, (DERV-834396-CE). 3) Relocated the existing phone & reel any (P/N TN1003.101) from the window line panel to the Fwd facing Divan RH cabinet in accordance with International Jet Interiors structural drawing No. 131-S76C-750-01, Rev IR dated 8/13/201% Titled "Instl-Phone Relocation". The listed structural drawing was approved via (attached) FAA/DER Form 8110-3 dated 8/22/2019, by Karol Mordasiewicz (DERT-834582-CE). 4) Reupholstered the existing Crew Seats with Aeristo leather: Aeronappa Incas P/N AN-G-018M, D/L 1118-P-1214 and Aeristo Leather. Alcantara Anthracite PN ALCA-AV-1883 (center insert). Reference Skandia Inc. FAA/DER form 8110-3 (attached) dated 08/21/2019 (Skandia burn report TP1/ 360764-19, Rev A dated 8/21/2019) by FAA/DER Jane Biberstein. (DERV-832780-CE). Crew seat belts have been rewebbed by C&M Marine Aviation Services Inc. (FAA/CRS # VO5R749Y) reference 8130-3 dated 8/1/2019. 5) Stripped and recovered the existing Headliner Panels, Window Line and Side Wall Panels throughout the cabin and cockpit with Aeristo leather: Aeronappa Incas P/N AN-G-0113M. D/L V18-P-1214. Reference Skandia Inc. FAA/DER Conn 8110-3 (attached) dated 08/21/2019 (Skandia burn report TP# 360764.19, Rev A dated 8/21/2019) by PANDER Jane Biberstein, (DERV-832780-CE). 6) Stripped and recovered the existing Headliner Insert with Perrone Fabric: Alcantara Avant 4883 Anthracite ALCA-AV- 4883. Reference Skandia Inc. PANDER form 8110-3 (attached) dated 08/21/2019 (Skandia burn report TP/1 360764-19, Rev A dated 8/21/2019) by FAA/DER Jane Biberstein, (DERY-832780-CE). 7) Stripped and recovered the existing upper and lower side wall panels, cabin door overlay, cabin side ledge throughout the cabin and cockpit with Aeristo leather. Aeronappa Incas P/N AN-G-018M, D/L VIII-P-I214. Reference Skandia Inc. FAA/DER form 8110-3 (attached) dated 08/21/2019 (Skandia bum report TP# 360764-19, Rev A dated 8/21/2019) by FAAMER lane Biberstein, (DERY-832780-CE). 8) Stripped and recovered the existing Cabin Fwd Bulkhead Panels with Aeristo leather: Aeronappa Incas P/N AN-G-018M, D/L YI8-P-1214 and Dedar Fabric: 3040/14 Contemporary/Perla. Reference Skandia Inc. FAA/DER form 8110-3 (attached) W4418/21/2019 and 8/23/2019 (Skandia burn reports TP# 360764-19, Rev A dated 8/21/2019 and TP 360828-195S% dated 8/23/2019) by FANDER Jane Biberstein, (DERY-832780-CE). 1'00 9) Stripped and recovered the existing Cabin Alt Bulkhead Panels with Aeristo leather. Aeronappa Incas P/N AN-G-018M, D/L Y18-P-1214 and E&T Mirror 2064 Grey M IMP K. Reference Skandia Inc. FAA/DER form 8110-3 (attached) dated 08/21/2019 and 8/23/2019 (Skandia burn reports TP# 360764-19, Rev A dated 8/21/2019 and TP 360828-19, Rev A dated 8/23/2019) by FAA/DER Jane Biberstein,(DERY-8327130-CE). 10) Installed new replacement Carpet throughout Cabin and Cockpit with Red Rock carpet: Hampton I -I GR968, Color Black. Reference Skandia Inc. FAA/DER form 8110-3 dated 08/21/2019 (Skandia bum report TPN 360764-19, Rev A dated (attached) 8/21/2019 by FAA/DER Jane Biberstein, (DERY-832780-CE). El Additional Sheets Are Attached FAA Form 337 (10-06) SDNYGM02757630 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244552 EFTA01329415  NOTICE Weight and balance a 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 S. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work accomplished) USA N722JE Date Nationality and Registration Mark 8/27/2019 I I) All affected areas of the aircraft interior have been placarded in accordance with Keystone Helicopter Engineering Document No. IC01217 Rev G. 12) This aircraft's W&B has been revised (calculated) this date showing new CG. 13) A logbook entry has been made reflecting this alteration. 14) This Refurbishment/Repair/Alteration to the existing Cabin Interior furnishings requires No Scheduled Maintenance Tasks or Airworthiness Limitations, refer to the OEM Maintenance Manual, and all other existing ICA's. The Aircraft's Scheduled Maintenance Program is not altered by this Modification/refurbishment. IS) The work described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. Work Order No. 19150, on file at this agency, covers the above described work. No further entries. 0 Additional Sheets Are Attached FM Form 337 (10-06) SDNYGA402757631 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244553 EFTA01329416  SDNY_GM_02757632 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFIA_00244554 EFTA01329417  Control Number. 2019-117 Sheet 1 of 1 119. DEPARTMENT OF TRMISPORTAT/ON I. DATE FEDERAL AVIATION ADMINISTRATION Elnrzois STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT empower IDENTIFICATION 2. MAKE & MOOG. NO. 4. TYPE Obtat &Una Pnettn. Vol S NAME OF AFRICAN Sikorsky Aircraft S-78C Aircraft International Jet Interiors. Corporation UST OF DATA 6. CDITIFCAIION T. MIRE .121: a: UkS76C-750-01 Rev Instl-Phone Relocation. IR Dated 08113)2019 Decurnents IJI-S76C-750-0ISA Rev IR Structural Analysis Phone Relocation Installation Sikorsky S76 Dated: 08/16(2019 END END Notes I This approval is for engineering design data only. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as Applicable Requirements. 2. This form constitutes FAA approval of all the engineering data necessary (or substantiation of compliance to necessary requirements for the entire atterationirepair. Electrical and Flammability approval may be required. 3. The modified cabinet is not part of the seat TSO. 4 Applicable Requirements are per the TWA HINE Rev 47, dated Apr1130, 2019 a. PURPOSE Of DATA Engineering drawing and report release in support of Field Approval of major alteration for Sikorsky helicopter Serial Number 780750. N722JE as outlined In drawing'. IJI-S78C-750-01 Rev IR, Dated 08113/2019 9 FFPuCial McMullinNo WOW maws) 14 CFR Part 29 Arndt 29-11, Sections: 29.301 Amdt 29-0, 29.303 Amdt 29-0, 29.305 Arndt 29-0, 29.307(a) Arndt 29-4, 29.309(a) Arndt 29-0, 29.337(a) Arndt 29-0, 29.561 (a)(b)(e) Amdt 29-0, 29601 Amdt 29-0, 29.603 Am* 29-0, 29.805 Arndt 29-0, 29.607(a) Arndt 29-5, 29.609(a) Amdt 29-0, 29.813 (a,b) Arndt 29-0, 29.825 Amdt 29-0 and 25.787 Arndt 29-0 10. aRTIFICATON . Undo autarky inset by Orecbon d OW AONIUMOY and n entadinca ent cantons and Inane:dm or aapposentani &d 14 CFR Pm In. data Bled is. AM 00 toted ghee furlIblred hat ONO atanted in liett0nfalce ern estatlases porettwes and town to amply at toncatle ettnernenb of the AnonymMesa Slant MINA 0 Recommend approval of Mese Oats I ONal TORO= = e Approve Owns darn 11. SIONAIURE4 • TED ENGIICERING REPRESENTATIVES) n. CESIGTATIONTAMMERS(S) 11 CUISSIFWATKVES) Karol a DERT-834582-CE Structures vewiat FAR Fens 91104 (0OJI0) SuPERSEOES PREVIOUS EOTiON SDNY_GM_02757833 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00244555 EFTA01329418  SDNY_GM_02757634 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244556 EFTA01329419  U. S. DEPARTMENT OF TRANSPORTATION 1. DATE FEDERAL AVIATION ADMINISTRATION 08/21(2019 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MANE 3. MODEL NO. 4. Typo (Mw.Eva Atspasc. as f 5. NAME OF APPLICANT Sikorsky S-76C Helicopter International Jet Interiors LIST OF DATA 6. IDENTIFICATION 7. TITLE TP 28191 Skandia. Inc. Flammability Test Report Rev A Oil Burner Testing and Vertical Burner Testing Dated 8/21/2019 Notes: 1) Work accomplished under Skandia Inc. WO e 360502-19. Ref Document ID 102212 2) Flammability test witnessing only, does not constitute Installation approval of the matenals. 8. PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair 8 Alteration for WI 760750 9. APPLICABLE REQUIREMENTS (List speak sections) 14 CFR Part 29.853 (a) Anull 29-23 and Ran 25 Appendix F Pail I (aXIX ii) 14 CFR 29.853(b) and Pan 25 Appendix F Part II 10. CtaTtFKATION - Under authority vested by direction of the Administrator and in th conditions and limitations of appointment under 14 CFR Part 183. data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Ainseethiness Standards listed. 0 Recommend approval of these data I iYerd Therefore tjlk Approve these data 11. SIGNATURE(S) OF OESIGNATED ENGINEERING REPRESENTATIVE 12. DESIGNATION NUM['ERIS) 13. cl.ASSiFiCATioN(S) A fr Oc irtjA au fild - aCkenzie Kacvinsky DERY-834396-CE Structural Special FAA Form 8110-3 (WO) SUPERSEDES PREVIOUS ION SDNY_GM_02757635 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244557 EFTA01329420  SDNY_GM_02757636 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244558 EFTA01329421  U. S. DEPARTMENT OF TRANSPORTATION 1. DATE FEDERAL AVIATION ADMINISTRATION OW21/2019 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE I. MODEL NO. 4. Type wen, &oak Props. WO S. NAME OF APPLICANT Sikorsky Aircraft Co S-76C Helicopter International Jet Interiors UST OF DATA S. MENT1P1CATION 7. TITLE TP 360764-19 Skandia. Inc. Flammability Test Report Rev A Dated 8/2112019 Bunsen Burner Testing Test Specimen Part Numbers: PN: 1 (Represents: Headliner panels) PN: 2 (Represents: Cockpit door panel & side wall panels) PN: 2A (Represents: Cockpit door panel & side wall panels) PH: 5 (Represents: Cockpit crew seats) PN: 6 (Represents: Cabin floor covering carpet) PN: 12 (Represents: Headliner panel insert) PN: 13 (Represents: Cabin door panel overlay) Notes: 1) Work accomplished under Skandia Inc. WO # 360764-19, Ref Document ID 102231. 2) Flammability test witnessing only, does not constitute installation approval of the materials. 8. PURPOSE OF DATA Demonstration Cr compliance with material flammability requirements in support of Major Repair 8 Alteration for S/N 780750 9. APPLICABLE REQUIREMENTS (List specific sections) 14 CFR Part 29.853 (a) Arndt 29-23 and Part 25 Appendix F Part I (a)(1)(0 14 CFR Part 29.853 (a) Arndt 29-23 arid Part 25 Appendix F Part I (a)(1)00 10. CERTIFiCATiON - Under authority vested by direction of the Administrator and in accordance with conditions and limitation of appointment Mkt 14 CFR Part 183. data fisted above and on attached sheets numbered have been examined In accordance with established procedures and found to comply with applicable requirements of the Airworthiness Standards listed. O Recommend approval of these data I (Prt.)Thefefore X Approve these data it. 814 TURNS) \ OF DESIGNATIDEN8INEERING REPREStNTATTVE 12. DESIGNATION NUMBER(5) 13. CLASSIFICATION(S) i ... bmJani\Biberstein DERV-832780-CE Structural Special FAA Fom181O.3 103110) SUPERSEDES PREVIOUS EDITION SDNY_GM_02757837 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244559 EFTA01329422 1 SDNY_GM_02757638 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00244560 EFTA01329423  U. S. DEPARTMENT OF TRANSPORTATION 1. DATE FEDERAL AVIATKIN ADMINISTRATION 0803/2019 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE 3. MODEL NO. 4. Typo (Nrplem, Engtv, Prewar. itc.) S. NAME Of APPLICANT Sikorsky Aircraft Co S-76C Helicopter International Jet Interiors UST Of DATA • IMMOLATION 7. TTTLE TP 360828-19 Skandia, Inc. Flammability Test Repel Rev A Dated 8/23/2019 Bunsen Burner Testing Test Specimen Part Numbers: PN: 9 (Represents: FWD cabin bulkhead) PN: 14 (Represents: Aft cabin bulkhead) Notes: 1) Work accomplished under Skandia Inc. WO # 360828-19. Ref Document ID 102236. 2) Flammability test witnessing only, does not constitute installation approval of the materials. S. PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair 4 Aiteratlon for SIN 760750 9. APPLICABLE REQUIREMENTS (LW specific sections) 14 CFR Part 29.853 (a) Arndt 29-23 and Pan 25 Appendix F Part I (at] xi) 70. CERTIFICATION - Under authonty vested by *renew of the Administrator and in accordance with conditions and limitations of appointment under 14 CFR Part 183, data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the AinvortNness Standards listed. O Recommend approval of these data I( ) Therefore yc Approve these data 11. TURERDOF D64961M-11TED ENGINEERING REPRESENTATIVE 12. DESIGNATION NUMBER(S) 13. CLASSIFICATION'S) r \ -,. c l-) A 1)j (Z:v_ r t 1 XO DER Jarte Bibersiein \IR DERY-832780-CE Structural Special FAA Fon\ 110-3 ( 10) SUPERSEDES PREVIOUS EDITION \ SDNY_GM_02757693 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024456 I EFTA01329424  SDNY_GM_02757640 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00244562 EFTA01329425  roan Aperoad I WI/0/K Tn.:bay Wrest OM No 21200320 0 MAJOR REPAIR AND ALTERATION 2/2610‘ I Le DaierUmm amIML We ay <I Treigatieo• (Airframe, Powerplant, Propeller, or Appliance) Feral miaow Mlainliengen INSTRUCTIONS Prnt or type al Nines See Tree 14 CFR §139. Part 13 Appends( R and AC 139.1 Mr subsequent mime thereof) for instructions and depasMon of this form The report a required by law (19 USG 644701) FaUe to report can resat to a awl penally for each such yolaton (49 U S C 546301(a)) Nationetly and Regetration Mark Seral No N722JE 760750 I. Aircraft us, Motel Series Keystone Helicopter S76 C++ Name (As shown on regestranon certificere) MOMS (As Moan on registration comfiest.) bad 151 Farrningten Ava 3. Owner ch Hartford sum ST ASI Wings LLO be 06156 Car,/ USA 3 For FAA Use Only 4. Type 5. Unit klentifkation ROOM Alteration Unit Make Model Ser ai No El AIRFRAME (As deserted n Am 1above) O El . POWERPtANT O O PROPELLER Type O APPLIANCE O umanurer 6 Conformity Statement A Agencys Name and Address 8 Kind or Agency NPs( Aeennated Aircraft Smile Mr U$ Certfceted Mecham I Mandocauret men. 32 Griffith Way Fear CWced Mechem C Certificate No car 10/aXED4N1 F•11‘ airs NY i Ctourcated Repair Slaw* 7.4. 12590 owetv USA centsras MaulalelanCe Ononemon AYPR340S CI I certty that the repar anctror alteration mac* to the und( ) Identified n date 5 above ant deserted on the reverse or attachments hereto have been made in accordance weft the requirements of Pad 43 or the U 5 Federt Aviation Regulations and that the inkonabon !unshed hewn a true and correct to the best oh my knowledge Extended range fuel S Dale of Autnonzed Individual pet 14 CFR Pan 43 O Alt 8 ' Tom Henry 28 Apr 16 / 7. Approval for Return to Service Recut t to the authority 9 von pe Jr %decried tekm, the unit denied in Item 5 was napectecl in the manner prescribed by the Administrator of the Federal Amber, Adminstraton and is le APProved O Rejected FAA Pt Standards Persons Approved by Cowden Inspector Manufacturer Maintenance Orgamzsion Chicanmers or Tenger, BY Other (SPX* FAA Designee it Repair Sieben Inspector' AuthOrtZatiOn Cenificate or SgnatureOate of Authonred I intuit Designation No AYPR34OS a / C-2( -4 ?2-4-4-I CP Scheftic 28 Apr 16 FAA Form 337 norm SDNY_GM_02757841 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244563 EFTA01329426  NOTICE Weight and balance or operating hmitahon changes shell be entered in the composts 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 to more space gs requv-ed attach Sitcshei sheets Identify with suctalt nationekly end regsstaton ins* and dote work 00ettplitifx1) N722JE 28 Apr 16 Nationally and Repastration Mark Date Alteration to Sikorsky S-76C++, N722JE, 760750 @Aircraft TSN 1.747 0, Lndgs 3.698 Removed engine oil access door PIN 76302-07014-061 and installed new engine oil access door P/N 76302-07014-049, modified with the "Thumb Latches" IAW Sikorsky Drawing No 33776.84145 Ref also Sikorsky Drawings 33776-84145-AL-001 Application List and 33776.84145-PL-001 Parts List The Door with Thumb Latches is an on-condition component with no airworthiness life limited parts This alteration does not require a Rotorcraft Flight Manual revision Weight and Balance is not affected by this alteration Airworthiness Inspections will be accomplished IAW the existing Sikorsky Airworthiness Limitations and Inspection Requirements Manual, ALIRM, SA 4047-76C-2-1, Ch 5-20.00 Pertinent details are on file under Work Order 5262-04.2016 A AS O ildarbonal SheetS Are *decree INSP. FAA Form 337 ecot. SONY_GM_02757642 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244564 EFTA01329427  f. • SDNY_GM_02757643 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244565 EFTA01329428  SDNY_GM_02757644 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244566 EFTA01329429 I l e f -.4--, 2 211x 1 --- --- -- - . -- -- -- --- -- ---- f i•11 IVII ....._ ; 18 1 tr i l; I; ii le it 'Z' ,- 3 Ii1 4 114: 1 1 p i - 1 ptvi i l 1....11 Ip 'll ; 1! • g 01 .. 11 gilei a .2 Mi it! ; e ts l - S. l i E O21 1 I i h le . , t 4t 1) , Ili '1 § ... 1 ., i !' 9. i I II. !IS - I . Iliiii ::: 0 I Mai i! e M .- I Fi l l g 1 ... , i. !!! i!1 z z .. 1 ' , I 0 .. I if NOTED a C i 0 a 8 il i . . ' i 1 .a. 8 • !.? e 1 . o. I ill0 I / o 1 a. !! : : II R3 i I III/ rkgtices. APPLIE1 AUUMfNUM ALLOY gi I ii ! ' 2 iI 1 1 ea II L.I .. I ; t s k i II r,'" . Ili i . rs . IIII . -'. : : : : 1 . ft q ... I 2 14 • I • i., r. ' ! I iSl!! 5 Lo .• e. • * i i 15 ! if Li a li i l" , i i It 6 .i f44-2; 17 7'. 3 1. V i-2E4 Ili f • !I SI, iI • i I . 4 ta51' 1 z.1. ... ......... -- --- --- --- --A " - ar..-.,% .-..t.:g.:1- ..:.5.. .._..... .._______—_-- --- -!th ;1 :: 7 77 • m -iii It .. 4, - SDNY_GM_02757645 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00244567 EFTA01329430  SDNY_GM_02757646 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024456% EFTA01329431  0 Sikorsky DESIGNED BY APPLICATION LIST REL. AUTE 8E C • u•••• •••••••pwOmes o ACCESS DOOR MOD 39066A AL 33776-84145 001 CO CAGR SIZE CRTC . RUM. ORIG. PREP. UNDER CONTRACT CESOCIIR NATHRIAL REVISED BY REV. DATA R rn 78286 A NAPIER NAPIER N ERICKSON 13JUL98 E CODS 1 CODS 3 •PART ml D • DRTAIL I - IllTALLATION N - NOT TO II 011D T • TOOL CODS 3 - 100. WITIRCRWKWAIIZLITY A • All1WOLT 1 - On IT I • SIT V - tones cram, v. voccanan tawny. 2 .vor nertano 3 • en icons LA • WITS/ DUOS le • an V • TOI0ING I. • MOLT 0OWT OTT R • /Alt KleTS12/1• V • V131211031 APPLES/ TO PART NO. IN LETT RAND CO VIP H KW IleTSWIAL PART C • COMM