TM 1-1520-238-23
11-1121
11.265.
TAIL ROTOR BELLCRANK LINK REMOVAL/INSTALLATION continued
b. Install link (3) on support (4). Torque nut (1) 225
to 285 INCH-POUNDS.
(1) Aline link (3) with support (4).
(2) Install two bushings (7) in link (3).
(3) Install bolt (2) through bracket (6), bushing
(7), link (3), washer (8), support (4), washer
(8), bushing (7), and bracket (6).
(4) Check fit of self-retaining bolt (2) (para 11.1).
(5) Install nut (1). Torque nut (1) to 225 INCH-
POUNDS. Use torque wrench.
(6) Increase torque to aline cotter pin hole, but do
not exceed 285 INCH-POUNDS.
(7) Install new cotter pin (5).
(8) Apply sealing compound to head of bolt (2)
and nut (1). Use sealing compound
(item 178, App F).
c. Inspect (QA).
d. Install tail rotor swashplate control bellcrank
(para 11.264).
e. Install access fairing L530 (para 2.2).
f. Perform directional flight control rigging
maintenance
operational
check
(TM 1-1520-238-T).
END OF TASK
M04-1758-11
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