TM 1-1520-240-MTF2-14EXTERIOR (CONT.)Top of Fuselage (Cont.)g. Engine fairing condition and security.O h. If EAPS is installed. Check EAPS to fairingmating surface for evidence of wear orchafing.2. Utility and flight control modules and coolerassemblies — Check for extended filtercontamination indicators and leaks. Check thataccumulators are precharged (Section V).Check PTU condition and security.3. Aft rotor (right side) — Check as follows:a. Check lag damper locknuts removed.b. Check components for proper safety wiringand security.c. Check blade lighting protection straps andcables installed on top and bottom of eachblade and condition.d. Check oil in rotor system reservoirs on rightside.e. Check droop stop weights and returnmechanism and droop stops for conditionand security.O f. Check droop stop shrouds for condition andsecurity.g. Check rain shield and stiffener for conditionand security.h. Check pitch change links, swashplate,slider assembly, and drive arm for conditionand security.i. Check upper boost actuator and pilot valvefor proper connection, condition, security.leakage, extended jam indicators.
Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business
