TM 1-1520-238-23
Change 5
11-291
11.62.
PILOT CYCLIC STICK FLIGHT CONTROL ARM ASSEMBLY DISASSEMBLY/ASSEMBLY
(AVIM) continued
f. Check removed and attaching parts for corro-
sion (para 1.49).
g. Check all installed bushing(s) and/or bear-
ing(s) for wear (para 11.5).
h. Check all removed bushing(s) and/or bear-
ing(s) for wear (para 11.4).
11.62.6. Assembly
a. Install shaft (23) on arm (1).
(1) Install shaft (23) through arm (1), cam (34),
and lever (33).
(2) Install two new rivets (32) in cam (34) and
lever (33) (TM 1-1500-204-23).
b. Install guide (28) on arm (1).
(1) Install pin (31) through arm (1), guide (28),
and washer (30).
(2) Install new cotter pin (29).
c. Install guide (22) on shaft (23).
(1) Install spring (27) and guides (22) and (28).
(2) Install pin (26) through shaft (23), guide (22),
and washer (25).
(3) Install new cotter pin (24).
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1
33
32
34
26
25
22
27
28
23
24
M04-4295-7
29
30
31
32