TM 1-1520-238-23
11-752
11.170. DIRECTIONAL F.S. 164.33 BELLCRANK REMOVAL/INSTALLATION – continued
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.
b. Install bellcrank (2) in bracket (14). Torque nut
(16) 30 to 40 INCH-POUNDS.
(1) Position bellcrank (2) in bracket (14).
(2) Aline bolt holes.
(3) Install bolt (17) through washer (18), bushing
(19), bracket (14), and bellcrank (2).
(4) Check fit of self-retaining bolt (17) (para
11.1).
(5) Install nut (16). Torque nut (16) to 30 INCH-
POUNDS. Use torque wrench.
(6) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(7) Install new cotter pin (15).
c. Install rod (8) in bellcrank (2). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Position rod (8) in bellcrank (2).
(2) Aline bolt holes.
(3) Install bolt (11) through washer (12), bushing
(13), bellcrank (2), and rod (8).
(4) Check fit of self-retaining bolt (11) (para 11.1).
(5) Install nut (10). Torque nut (10) to 30 INCH-
POUNDS. Use torque wrench.
(6) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(7) Install new cotter pin (9).
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M04-2518-8
2
17
18
19
14
16
15
VIEW ROTATED
17
18
13
10
9
M04-2518-9
2
12
11
8
