TM 1-1520-238-23
11-1124
Change 3
11.266.
TAIL ROTOR CONNECTING LINK REMOVAL/INSTALLATION – continued
11.266.6. Installation
CAUTION
To prevent damage to flight control sys-
tem components, do not use force to
aline bellcrank with bracket or to aline
push-pull rod with bellcrank.
a. Install tail rotor connecting link (3) on servo-
cylinder (9). Torque nut (7) 30 to 40 INCH-
POUNDS.
(1) Install link (3) with adjustable end towards
bellcrank (4) on servocylinder (9).
(2) Apply primer to bolt (8). Use primer coating
(item 147, App F).
(a) Do not apply primer on threads.
(b) Install wet.
(3) Install bolt (8).
(4) Check fit of self-retaining bolt (8) (para 11.1).
(5) Install nut (7). Torque nut (7) 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 (10).
(8) Apply primer to threads only of bolt (8). Use
primer coating (item 147, App F).
(9) Allow primer 30 MINUTES to cure.
(10) Apply corrosion preventive compound to
threads of bolt (8). Use corrosion preventive
compound (item 62, App F).
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