Epstein Secrets

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

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

n AIRFRAME (As described In Item 1 above) X POWER PLANT PROPELLER • APPLIANCE Type Manufacture

, Identify with aircraft nationality and registration mark and date work acconwashed.) • AIRCRAFT: BOEING, TYPE: 727-31, SIN 20115, DATE 06/1412001, W.O. 16236. PAGE 2 0F2 AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-18, CHAPTER 4. SECTIONS 1, 2.3 AND 4, CHAPTER 6, S

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

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

AUDIO PANEL TO RS232 DATA TERMINAL TO AIRCRAFT POWER (2.8 Vdc) AIRCRAFT FUSELAGE Figure 2.1-1 Bloc

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

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

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,

TRICAL JUNCTION BOX, MODIFICATION OF ELECTRICAL POWER-LOOSE GENERATOR WIRING .s ENGING JUNCTION BOX-MO

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.