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o.: Sheepskin 3CCOOI, White. Rewebbed two (2) crew seal Spt seat and shoulder harness belts by C&M Marine Aviation Services Inc, CRS V05R749Y, under W.O. 4991, 8130-3 dated 8/13/13. Flammability Testing (Spec 12) was approved via Skandia Inc. (WO 1257726-13. Test Plan 0 21306) Vertical Flammability T

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

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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

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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,

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.