TM 1-1520-238-23
11-715
11.162. CPG TO PILOT CONTROL DIRECTIONAL F.S. 118.50 SUPPORT BRACKET
REMOVAL/INSTALLATION – continued
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.
b. Install bellcrank (2) on bracket (8). Torque nut
(10) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (2) with bracket (8).
(2) Install bolt (11) through washer (12), bushing
(13), bracket (8), and bellcrank (2).
(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).
c. Install rod (1) on bellcrank (2). Torque nut (4) 30
to 40 INCH-POUNDS.
(1) Aline rod (1) with bellcrank (2).
(2) Install bolt (5) through washer (6), bushing
(7), bellcrank (2), and rod (1).
(3) Check fit of self-retaining bolt (5) (para 11.1).
(4) Install nut (4). Torque nut (4) to 30 INCH-
POUNDS. Use torque wrench.
(5) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(6) Install cotter pin (3).
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