TM 1-1520-238-23
11-719
11.163. CPG TO PILOT CONTROL DIRECTIONAL F.S. 120.00 RIG CONNECTING LINK
REMOVAL/INSTALLATION – continued
11.163.6. Installation
CAUTION
To prevent damage to flight control com-
ponents, do not use force to aline bell-
crank with bracket or to aline push-pull
rods with bellcrank.
a. Install link (1) on bellcrank (8). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Aline link (1) to bellcrank (8).
(2) Install bolt (11) through washer (12), bushing
(13), bellcrank (8), rod end (15), bushing (14),
and link (1).
(3) Check fit of self-retaining bolt (11) (para 11.1).
(4) Install nut (10). Torque nut (10) 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 (9).
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M04-5070-4
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