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ting a repair per the Structural Repair Manual (SRM): No serial number specific FAA Form 8100-9 is required and will not be provided in support of a GM. repair. The Engineering (Source) Data for this Service Letter has been shown to comply with the applicable FAR's and is FAAApproved. Engineering s
Waiting approval SC Paint Labor Only (L/P/S) Step: 15.1.9 Waiting approval Inspection Labor Only (L/P/S) Step: 15.1.10 Waiting approval Weight and Balance Labor Only (L/P/S) Item: 16 KA BAND HARNESS FABRICATION Team Manager: Customer Coordinator: Charles Thomas Julian Brown Part/Model 8: AC Se
al Separation Minimum — (RVSM) SDNY_GM_02754995 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241917 EFTA01327035 SDNY GM 02754996 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 19 I 8 EFTA01327036 EFTA01327037 SDNY GM 02754998 SUBJECT T
manual. Inspection intervals shall remain as indicated in the aircraft maintenance manual or operators approved inspection program as appropriate. Weight and Balance unaffected. Reference Constant Aviation work order CCM-3160 END MAGUS:nal Sews NO needled FM Form 337 (10/06) Page 2 SDNY_GM_02754906 • •
PECIAL AIRWORTHINESS CERTIFICATE (Crectiarreeem ram 7 PRIMARY 9 LIGHT-SPORT emisam I 1 AlMene I I Poser-Peradlule I I Weistit•ShisCentel I I GM.' I I LOW den At 2 LIMITED 5 PROVISIONAL I CLASS I Aeon On) 2 CLASS II r G I AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEY 3 AERIAL
manual. Inspection intervals shall remain as indicated in the aircraft maintenance manual or operators approved inspection program as appropriate. Weight and Balance unaffected. Reference Constant Aviation work order CCM-3160 END =Additional Sheets Arc Attached FAA Form 337 (10/06) Pagc 2 EFTA00011670 U.
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 DO
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
71/0/4 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 t
aintenance 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.
OTECTIVE 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
istrator on request. II. All.work Performed utilizing acceptable methods; techniques, and practices per AC 43.13-1A. . , III. Aircraft weighed.. Weight and Balance amended. • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246945 EFTA01331408 1Litat IMMPOILIOCIPI a ( FOSNIa AvIA110
roval: 0070900AA“ Page I of 6 SDNY_GM_02757653 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244575 EFTA01329438 SDNY GM 02757654 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244576 EFTA01329439 PHI-S76-DL-0015 Rev (8)02/26/14 REVISIONS
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 Inspectio
om.com SDNY_GM_02757332 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFFA_00244254 EFTA01329117 [I 1 i -O:124 . ITA • SONY GM 02i57333.: SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244255 EFTA01329118 Memorandum Date: To: From: Subject: Fed
port dated 5/5/2017 for the removal of the R/H Number 6 Passenger Single Seat. establishing new Basic Empty Weight and CG. 3) The airerafts updated Weight and Balance report has been provided to customer. 4) A logbook entry has been made reflecting this alteration. 5) Work Order No. 17124, on file at this agency
cOualts OIALION• NORM TYPE CERTIFICATE OTHER C GM QUANTITY OF CERTIFICATES REOURED FOR OPERATING NE
board the aircraft as a guide to equipment operation. 3.) This install is for VFR use, altitude above the terrain is advisory information only. 4.) Weight and Balance computed. and equipment list updated. 5.) An electrical load analysis determined that the electrical load of the aircraft does not exceed 80% of the
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