TM 1-1520-238-23
11-419
11.95.
CPG TO PILOT CONTROL LATERAL F.S. 118.50 BELLCRANK
REMOVAL/INSTALLATION – continued
11.95.6. 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 bellcrank (2) on bracket (14). Torque nut
(16) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (2) with bracket (14).
(2) Install bolt (17) through washer (18), bushing
(19), bracket (14), and bellcrank (2).
(3) Check fit of self-retaining bolt (17) (para
11.1).
(4) Install nut (16). Torque nut (16) 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 (15).
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M04-4348-6
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