TM 1-1520-238-23
Change 3
11-1125
11.266.
TAIL ROTOR CONNECTING LINK REMOVAL/INSTALLATION – continued
b. Install adjustable end of tail rotor connecting
link (3) on bellcrank (4). Torque nut (1) 30 to 40
INCH-POUNDS.
(1) Aline link (3) with bellcrank (4).
(2) Apply primer to bolt (2). Use primer coating
(item 147, App F).
(a) Do not apply primer on threads.
(b) Install wet.
(3) Install bolt (2).
(4) Check fit of self-retaining bolt (2) (para 11.1).
(5) Install nut (1). Torque nut (1) to 30 INCH-
POUNDS. Use torque wrench.
(6) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(7) Install new cotter pin (5).
(8) Apply primer to threads only of bolt (2). Use
primer coating (item 147, App F).
(9) Allow primer 30 MINUTES to cure.
NOTE
Do not apply sealing compound to spheri-
cal bearings.
(10) Apply sealing compound to head of bolts (2)
and (8) and nuts (1) and (7). Use sealing
compound (item 178, App F).
c. Inspect (QA).
d. Perform directional flight control rigging op-
erational check (TM 1-1520-238-T).
e. Install access fairings L530 and L540 (para
2.2).
END OF TASK
M04-1784-4
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