TM 1-1520-238-23
11-502
11.114.
CPG TO PILOT LONGITUDINAL F.S. 82.80 CONTROL BRACKET
REMOVAL/INSTALLATION – continued
b. Remove bolt (8) from bracket (9) and bellcrank
(2).
(1) Remove and discard cotter pin (10).
(2) Remove nut (11).
(3) Remove bolt (8), washer (12), and bushing
(13) from bracket (9) and bellcrank (2).
c. Remove bracket (9) from airframe (14).
(1) Remove four bolts (15) and washers (16).
(2) Remove bracket (9) from airframe (14).
11.114.4. Cleaning
a. Wipe removed and attaching parts with a
clean rag.
11.114.5. Inspection
a. Check removed and attaching parts for
cracks. None allowed.
b. Check removed and attaching parts for dam-
age (para 11.5).
c. Check removed and attaching parts for corro-
sion (para 1.49).
d. Check all installed bushing(s) and/or bear-
ing(s) for wear (para 11.5).
e. Check all removed bushing(s) and/or bear-
ing(s) for wear (para 11.4).
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