TM 1-1520-238-23
11-590
11.133. PILOT COLLECTIVE PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.133.4. Cleaning
a. Wipe removed and attaching parts with a
clean rag.
11.133.5. 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).
11.133.6. Installation
CAUTION
To prevent damage to flight control com-
ponents, do not use force to aline bell-
crank or to aline push-pull rod with
bellcrank.
a. Install adjustable end of rod (1) on arm (8).
Torque nut (10) 30 to 40 INCH-POUNDS.
(1) Aline rod (1) with arm (8).
(2) Install bolt (11) through washer (12), bushing
(13), arm (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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