TM 1-1520-238-23
11-624
11.140. COLLECTIVE F.S.164.95 BELLCRANK REMOVAL/INSTALLATION – continued
11.140.6. 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.
NOTE
Dowel pin is used to aline bushing and
bearing inside of bellcrank during instal-
lation.
a. Install bellcrank (2) on bracket (14). Torque nut
(16) 30 to 40 INCH-POUNDS.
(1) Position bushing (22) and bearing (21) in bell-
crank (2).
(2) Insert dowel pin (20) through bearing (21),
bushing (22), and bellcrank (2). Use dowel.
(3) Install bellcrank (2) on bracket (14).
(4) Install bolt (17) through washer (18), bushing
(19), bracket (14), bellcrank (2), bearing (21)
and bushing (22) pushing dowel pin (20) out
of bellcrank (2).
(5) Check fit of self-retaining bolt (17) (para
11.1).
(6) Install nut (16). Torque nut (16) to 30 INCH-
POUNDS. Use torque wrench.
(7) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(8) Install new cotter pin (15).
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M04-3562-7
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