TM 1-1520-238-23
11-535
11.122. LONGITUDINAL F.S. 129.25 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.122.6. 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 rods (8) and (1) on bellcrank (9). Torque
nut (11) 30 to 40 INCH-POUNDS.
(1) Aline rod (8) with bellcrank (9).
(2) Install bushing (15).
(3) Aline rod (1) with bellcrank (9).
(4) Install bolt (12) through washer (13), bushing
(14), bellcrank (9), rod (1), bushing (15), and
rod (8).
(5) Check fit of self-retaining bolt (12) (para
11.1).
(6) Install nut (11). Torque nut (11) to 30 INCH-
POUNDS. Use torque wrench.
(7) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(8) Install new cotter pin (10).
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