TM 1-1520-238-23
11-382
11.86.
CPG CYCLIC LATERAL PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.86.6. Installation
CAUTION
To prevent damage to flight control com-
ponents, do not use force in alining push-
pull rod with bellcranks.
a. Install rod (1) on bellcrank (8). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Install bolt (11), washer (12), and bushing
(13) through bellcrank (8) and rod (1).
(2) Check fit of self-retaining bolt (11) (para 11.1).
(3) Install nut (10). Torque nut (10) to 30 INCH-
POUNDS. Use torque wrench.
(4) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(5) Install new cotter pin (9).
b. Install adjustable end of rod (1) on bellcrank
(2). Torque nut (4) 30 to 40 INCH-POUNDS.
(1) Install bolt (5), washer (6), and bushing (7)
through bellcrank (2) and rod (1).
(2) Check fit of self-retaining bolt (5) (para 11.1).
(3) Install nut (4). Torque nut (4) to 30 INCH-
POUNDS. Use torque wrench.
(4) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(5) Install new cotter pin (3).
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