TM 1-1520-238-23
11-1146
11.271. DIRECTIONAL F.S. 534 PUSH-PULL ROD REMOVAL/INSTALLATION – continued
11.271.6. 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 push-pull rod (3) on lower bellcrank (9).
Torque nut (8) 30 to 40 INCH-POUNDS.
(1) Aline rod (3) with bellcrank (9).
(2) Install bolt (7) through bellcrank (9) and rod
(3).
(3) Check fit of self-retaining bolt (7) (para 11.1).
(4) Install nut (8). Torque nut (8) to 30 INCH-
POUNDS. Use torque wrench.
(5) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(6) Install new cotter pin (10).
NOTE
Do not apply sealing compound to spheri-
cal bearing.
(7) Apply sealing compound to head of bolt (8)
and nut (7). Use sealing compound
(item 178, App F).
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