TM 1-1520-238-23
11-628
11.141. COLLECTIVE F.S. 164.95 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.141.4. Cleaning
a. Clean removed and attaching parts (para
1.47).
11.141.5. Inspection
a. Check removed and attaching parts for dam-
age (para 11.5).
b. Check removed and attaching parts for corro-
sion (para 1.49).
c. Check all installed bushing(s) and/or bear-
ing(s) for wear (para 11.5).
d. Check all removed bushing(s) and/or bear-
ing(s) for wear (para 11.4).
11.141.6. Installation
CAUTION
To prevent damage to flight control com-
ponents, do not use force in alining push-
pull rod with bellcrank and servocylinder
clevis.
a. Install adjustable end of rod (6) on clevis (13).
Torque nut (15) 30 to 40 INCH-POUNDS.
(1) Aline rod (6) with clevis (13).
(2) Install bolt (16) through washer (17), clevis
(13), and rod (6).
(3) Check fit of self-retaining bolt (16) (para
11.1).
(4) Install nut (15). Torque nut (15) 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 (14).
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M04-4373-4
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