TM 1-1520-238-23
11-90
Change 4
11.12.
AFT LONGITUDINAL BELLCRANK REMOVAL/INSTALLATION – continued
e. Install servocylinder (1) on bellcrank (2).
(1) Aline servocylinder (1) with bellcrank (2).
(2) Insert alinement bolt (2.1) halfway through
bellcrank (2), nylon washer (8), and servocy-
linder (1) from inboard side of bellcrank.
(3) Insert bushing (7) through bellcrank (2) until it
seats against servocylinder (1).
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.
(4) Apply a light coat of corrosion preventive
compound to shank of bolt (4). Use corrosion
preventive compound (item 62A, App F).
(5) Install bolt (4) through washer(s) (6) (if re-
quired) and force alinement bolt (2.1) out of
bellcrank (2).
(6) Check fit of self-retaining bolt (4) (para 11.1).
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8
2.1
1
7
2
M04-1719-11
M04-1719-12
1
6
4
2
2.1
