TM 1-1520-238-23
Change 5
7-165
7.43.
COLLECTIVE SERVOCYLINDER ROD END REPLACEMENT – continued
NOTE
If nylon washer is excessively worn or
has debonded from bellcrank, repair
(para 11.12).
d. Aline rod end (1) with bellcrank (2).
(1) Insert alinement bolt (14) halfway through
bellcrank (2), nylon washer (7), and rod end
(1) from inboard side of bellcrank.
e. Insert bushing (6) through bellcrank (2) until it
seats against rod end (1).
f. Install rod end (1) on bellcrank (2).
CAUTION
Threads of bolt and nut shall be clean,
and compound free. Contaminated
threads can cause improper torque,
which may cause damage to flight control
system.
(1) Apply a light coat of corrosion preventive
compound to shank of bolt (4). Use corrosion
preventive compound (item 62A, App F).
(2) Install bolt (4) through washer(s) (4.1) (if re-
quired) and force alinement bolt (14) out of
bellcrank (2).
(3) Check fit of self-retaining bolt (4) (para 11.1).
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M04-792-9A
14
6
1
7
2
M04-792-10A
14
4
1
2
4.1
