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

red. 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 SENSO

• 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

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, P

ing 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. 34-60-09, Rev. 2, dated August 15, 1997 or la

d, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) N908JE, BOEING 727-31, S/N 20115, W.O. 18046 REFERENCE F.A.A. FORM 337 DATED 7/2/01 INSTALLING A UNIVERSAL AVIONICS CORP. UNS-ID FLIGHT MANAGEMENT SYSTEMS (FMS) WITH INTEGRAL GPS SENSORS

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

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 fl ADDITIONAL SHEETS ARE ATTACHED FAA AC 72-4906 EFTA00277827 0 . MAJOR REPAIR AND ALTERATION uSDeporrpent atralwavarxxl (Airframe,

: -.. • Installektinal CollinatICS.3iaysteme cceisisting of the fallo,hing: . ... • • • •;• each Collins NCS.31 Control 114aplay Unita It each Collins 339R-1 Progress Ramat Readout tinfta • 4 .each Collins 899P-1 Radio Adaptor Units . 1 each Collins 339R-7 Remote Readout Unit • 1 each Collins 339

STANCE FI' & IN. IN; a i b " I i_ a-b , i . / 0% MAC 100% MAC I PIT. 28 Cooper Airmotive Exec: Aire. Serv.• Div. DATE March 8, 1975 W.O. 215 VERT DATUM (WLRDE) MAIN GEAR HORIZONTAL ARM = •a. +.15. OD INCHES NOSE GEAR HORIZONTAL ARM = (a-b) = N MOIL ARM IN INCHES) INCHES 0,11.