TM 1-1520-238-23
Change 4
11-1039
11.246.
DIRECTIONAL F.S. 199.25 BELLCRANK 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 (3) on bracket (6). Torque self-
locking nut (7) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (3) with bracket (6).
(2) Install close tolerance bolt (8) washer (9),
sleeve bushing (10) bracket (6) and bellcrank
(3).
(3) Remove dowel (4) from bellcrank (3).
(4) Check fit of self-retaining bolt (9) (para 11.1).
(5) Install nut (7). Torque nut (7) 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 (11).
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M04-1787-3A
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M04 1787 4
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