TM 1-1520-238-23
11-437
11.99.
LATERAL F.S. 132.84 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.99.6. Installation
CAUTION
To prevent damage to flight control
system components, do not use force
if binding or roughness occurs while
moving controls with hydraulic power.
To prevent damage to flight control
system components, do not use force
to aline bellcrank with bracket or to
aline push-pull rod with bellcrank.
a. Install rod (5) on bellcrank (14). Torque nut (16)
30 to 40 INCH-POUNDS.
(1) Install bolt (17) through washer (18), bushing
(19), bellcrank (14), and rod (5).
(2) Check fit of self-retaining bolt (17) (para
11.1).
(3) Install nut (16). Torque nut (16) 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 (15).
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M04-4377-6
14
19
17
16
15
5
18
