TM 1-1520-240-MTF2-19EXTERIOR (CONT.)Top of Fuselage (Cont.)23. Top of fuselage — Check skin condition, VHFantenna, GPS antenna, and foreign objectsremoved.24. Forward rotor (left side) — Check as follows:a. Check lag damper lockouts 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 rotor system reservoirs on leftside.e. Check droop stops, rain shield and stiffenerfor condition and security.f. Check pitch change links, swashplate,slider assembly, and drive arm conditionand security.g. Check upper boost actuators and pilot valvefor proper connection, conditions, securityand leakage. Check for extended jamindicators.h. Check longitudinal cyclic trim actuator forcondition and security.i. Cruise guide link and signal conditioners —Check for condition and security.25. Forward transmission — Check mount bolts.Check oil cooler inlet for obstruction.a. Forward transmission pressure transducer— Check for leaks and security.b. Hydraulic cooling fan — Check forobstructions, condition, and security.
Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business
