TM 1-1520-238-23
11-503
11.114.
CPG TO PILOT LONGITUDINAL F.S. 82.80 CONTROL BRACKET
REMOVAL/INSTALLATION – continued
11.114.6. Installation
a. Install bracket (9) on airframe (14).
(1) Position bracket (9) over bellcrank (2).
(2) Aline four holes in bracket (9) with holes in
airframe (14).
(3) Install four bolts (15) through washers (16)
and bracket (9), into airframe (14).
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 bolt (8) through bracket (9) and bell-
crank (2). Torque nut (11) 30 to 40 INCH-
POUNDS.
(1) Aline bellcrank (2) with bracket (9).
(2) Install bolt (8) through washer (12), bushing
(13), bracket (9), and bellcrank (2).
(3) Check fit of self-retaining bolt (8) (para 11.1).
(4) Install nut (11). Torque nut (11) to 30 INCH-
POUNDS. Use torque wrench.
(5) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(6) Install new cotter pin (10).
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9
2
M04-4332-6
15
16
14
2
8
12
13
11
10
M04-4332-7
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