TM 1-1520-238-23
11-536
Change 7
11.122.
LONGITUDINAL F.S. 129.25 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
b. 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).
(5) Torque nut (4) to 30 INCH-POUNDS. Use
torque wrench.
(6) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(7) Install new cotter pin (3).
c. Inspect (QA).
d. Perform lateral flight control rigging mainte-
nance operational check (TM 1-1520-238-T).
e. If removed install forward fuel cell retainer
panel (para 10.52A).
END OF TASK
M04-4383-6
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