TM 1-1520-238-23
11-392
11.88.
LATERAL F.S. 65.50 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.88.6. 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 rod (1) on bellcrank (8). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Aline rod end (1) with bellcrank (8).
(2) Install bolt (11) through washer (12), bushing
(13), bellcrank (8), and rod end (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).
b. Install rod (1) on bellcrank (2). Torque nut (4) 30
to 40 INCH-POUNDS.
(1) Aline rod end (1) with bellcrank (2).
(2) Install bolt (5) through washer (6), bushing
(7), bellcrank (2), and rod end (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 new cotter pin (3).
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M04-5086-4
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M04-5086-5
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