TM 1-1520-238-23
11-543
11.124. LONGITUDINAL F.S. 159.62 BELLCRANK REMOVAL/INSTALLATION – continued
11.124.4. Cleaning
a. Wipe removed and attaching parts with a
clean rag.
11.124.5. 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).
11.124.6. 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 bellcrank (7) on bracket (19). Torque nut
(21) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (7) with bracket (19).
(2) Install bolt (22) through washer (23), bushing
(24), bracket (19), and bellcrank (7).
(3) Check fit of self-retaining bolt (22) (para
11.1).
(4) Install nut (21). Torque nut (21) 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 (20).
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20
24
7
22
23
M04-4357-8
21
19
