TM 1-1520-238-23
5-32
Change 3
5.4.
MAIN ROTOR BLADE INSTALLATION continued
o. Remove droop stop wedges (para 1.83).
p. Inspect main rotor blade (para 5.2).
q. Remove main rotor blade tiedown (para 1.107).
r. Remove maintenance crane from aircraft (para 1.105).
s. Inspect (QA).
CAUTION
If TB 1-1520-238-20-62 (Deactivation of Main Rotor and Tail Rotor Blade De-ice Capability) is com-
plied with, do not perform step t. and u. Go to step v.
t. On the pilot aft circuit breaker panel, enable de-ice system by closing BLADE DE-ICE and BLADE
DE-ICE CONTR circuit breakers. Remove wire tie to reactivate.
u. Adjust de-ice system controller (para 12.56).
v. Perform main rotor track and balance maintenance operational check (TM 1-1520-238-T).
END OF TASK