TM 1-1520-238-23
11-1079
11.257.
DIRECTIONAL F.S. 348 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) on bracket (14). Torque
nuts (16) and (20) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (2) with bracket (14).
(2) Install bolt (17) through bushing (18), bracket
(14), and bellcrank (2).
(3) Check fit of self-retaining bolt (17) (para
11.1).
(4) Install nut (16).
(5) Install bolt (22) through bracket (14), bell-
crank (2), and bushing (21).
(6) Check fit of self-retaining bolt (22) (para
11.1).
(7) Install nut (20).
(8) Torque nuts (16) and (20) to 30 INCH-
POUNDS. Use torque wrench.
(9) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(10) Install new cotter pins (15) and (19).
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M04-1802-7
17
14
2
18
21
20
22
16
M04-1802-8
15
16
20
19
