TM 1-1520-238-23
11-1059
11.252.
DIRECTIONAL F.S. 216.25 PUSH–PULL ROD REMOVAL/INSTALLATION – continued
11.252.6. 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. Insert directional control push-pull rod (4)
through access door L200 opening.
b. Install forward end of rod (4) on bellcrank (10).
Torque nut (12) 30 to 40 INCH-POUNDS.
(1) Aline rod (4) with bellcrank (10).
(2) Install bolt (13) through washer (14), bushing
(15), bellcrank (10), and rod (4).
(3) Check fit of self-retaining bolt (13) (para
11.1).
(4) Install nut (12). Torque nut (12) 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 (11).
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