TM 1-1520-238-23
11-743
11.168. DIRECTIONAL F.S. 159.98 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.168.6. Installation
CAUTION
To prevent damage to flight control sys-
tem components, do not use force if bind-
ing or roughness occurs while moving
controls with hydraulic power.
a. Install rod (1) on bellcrank (8). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Aline rod (1) with bellcrank (8).
(2) Install bolt (11) through washer (12), bushing
(13), bellcrank (8), and rod (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).
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