TM 1-1520-238-23
11-447
11.101. LATERAL F.S. 132.84 FLIGHT BRACKET ASSEMBLY 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 (6) on bracket (12). Torque nut
(14) 30 to 40 INCH-POUNDS.
(1) Install bushing (19) and bearing (18) on bell-
crank (6).
(2) Aline bellcrank (6) with bracket (12).
(3) Install bolt (15) through washer (16), bushing
(17), bracket (12), and bellcrank (6).
(4) Check fit of self-retaining bolt (15) (para
11.1).
(5) Install nut (14). Torque nut (14) 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 (13).
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14
17
12
6
18
16
15
M04-4407-7
13
19
