Epstein Secrets

ing 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 lat

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

• 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 • STATIO

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.

ransponder system . . • ' l i, c Dual Collins DF-206 kW system Collins FPC -75 ground proximity warning Systel‘we -.. . ... ...-...„„, ..- . Collins 54W1C comparator warning system . . . • Collins 512-4 marker beacon system RCA Primus-400 HKO coloradar system Wulfsberg fligbtfone III air to

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

B. supplied to the operator. Where the CTL-92E Controller is referenced in the ICA, refer to the existing aircraft maintenance documentation for the Collins RTU-4200 Radio Tuning Unit. • No change to the electrical load for this rotorcraft. • Refer to the updated Aircraft Computed Weight and Balance,

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

date work completed.) 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKE/MODEL/DESCRIPTION STATION 622-7293-101 3 Collins VHF-422b Comm C37c, C38c 450.0 2. The following equipment was installed in the aircraft. • PART NUMBER QTY MAKE/MODEL/DESCRIPTION ISO ,j= S

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

te tapes. All channels'operated.normal. The tapes are on file at this facility. The operator was supplied with "Pilots Operation Instructions" for Collins AVR-101 Cockpit Voice Recorder", report no. A8910001. This report must be aboard.the aircraft during all flight operations. The above mentioned ins

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