TM 1-1520-240-MTF
2-14
EXTERIOR (CONT.)
Top of Fuselage (Cont.)
g. Engine fairing condition and security.
O h. If EAPS is installed. Check EAPS to fairing
mating surface for evidence of wear or
chafing.
2. Utility and flight control modules and cooler
assemblies — Check for extended filter
contamination indicators and leaks. Check that
accumulators 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 wiring
and security.
c. Check blade lighting protection straps and
cables installed on top and bottom of each
blade and condition.
d. Check oil in rotor system reservoirs on right
side.
e. Check droop stop weights and return
mechanism and droop stops for condition
and security.
O f. Check droop stop shrouds for condition and
security.
g. Check rain shield and stiffener for condition
and security.
h. Check pitch change links, swashplate,
slider assembly, and drive arm for condition
and security.
i. Check upper boost actuator and pilot valve
for proper connection, condition, security.
leakage, extended jam indicators.
