Epstein Secrets

00 Discrepancy: 40.56 CMP 6550 491301 Auxiliary Power Unit Turbine Plenum Drains - Operational Test Fo

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

l/Installation 29 3.2 Access Location 29 4 POWER DISTRIBUTION 30 4.1 Circuit Breakers by Bus 3

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 • •

ine Discussion Verification Step(s) Symptom I Power is not available to ASE The handset display shou

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

ET CORPORATION STC SA313650. INSTALLED RSSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH PAGE AVJET C

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.

notes Yalsan Drawing. Chapter a. 24 ELECTRICAL POWER A24(1000 A Electrical System Instl. - Strut E.

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

orsky S-76C STARTING ENGINES BATTERY OR EXTERNAL POWER 27. Avionics — As desired. a. Transponder (RTU-

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

Kimball Avenue Chino, Ca 91708 Subject: Special Power of Attorney Dear Khera: The undersigned is the

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

al/Installation 29 3.2 Access Location 29 4 POWER DISTRIBUTION 30 4.1 Circuit Breakers by Bus 3

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.

CORPORATION STC SA3136S0. . INSTALLED ESSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH .PAGE AVJET

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 IAW the prescribed loading information from the manufacturer. E

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43.13-1A, Chapter 16, Section 5, Paragraphs 927, 928 and 929 and AC 43.13-2A Chapter 2, Paragraph 23f. The Equipment List was amended and the new Weight and Balance was computed and entered in the aircraft records IAW AC 43.13-1A, Chapter 13, Paragraphs 659 and AC 43.13-2A, Chapter 1 Paragraph 9. The UNS-1D sy