Epstein Secrets

M approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (I

corrosion, HFEC, no cracks noted. Fabricated and installed I ea. bushing IAW TIMCO REO-L01064 Rev. IR dated 04/14/08 approved by FAA Form 8110-3 by Richard C. Saltivan #DERT-40157-CE dated Apr. 17, 2008. SUMMARY 1. All work accomplished JAW TIMCO REO and FAA Form 8110-3. 2. Records of all work accomplished is on

M approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (I

e delaminated section and fabricating and installing a new T/E wedge and strips TAW TIMCO REO-L00464 dated 7/17/01 FAA Form 8110-3 approved by DER. Richard C. Saltivan DER # DERT-405157-CE dated June 19, 2001. MU 27918 Repaired the delaminated and corroded Left Hand Inboard Mid Flap bottom upper Rock-shield panel

A approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (I

he delaminated section and fabricating and installing a new T/E wedge and strips IAW TIMCO REO-L00464 dated 7/17/01 FAA Form 8110-3 approved by DER Richard C. Saltivan DER # DERT-405157-CE dated June 19, 2001. NR# 27918 Repaired the delaminated and corroded Left Hand Inboard Mid Flap bottom upper Rock-shield panel