TM 1-1520-238-23
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11.109. LATERAL F.S. 164.95 BELLCRANK BRACKET ASSEMBLY REMOVAL/INSTALLATION – continued
11.109.5. 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).
11.109.6. 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 bracket (8) on airframe (16).
(1) Aline four holes in bracket (8) with holes in
airframe (16).
(2) Install two aft bolts (19) through bracket (8),
and airframe (16).
(3) Install two forward bolts (18) through bracket
(8), and airframe (16).
(4) With one person holding bolts (18) and (19),
install four washers (21) and nuts (20).
(5) Apply sealing compound to faying surface of
bracket (8). Use sealing compound
(item 174, App F).
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18
21
20
8
21
20
16
19
M04-4402-7
