TM 1-1520-238-23
11-404
11.91.
CPG TO PILOT LATERAL CONTROL F.S. 83.45 SUPPORT BRACKET ASSEMBLY
REMOVAL/INSTALLATION – continued
11.91.6. Installation
a. Install bracket (2) on airframe (8).
(1) Aline three holes in bracket (2) with holes in
airframe (8).
(2) Install three bolts (9) through washers (10),
bracket (2), and airframe (8).
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 (1) on bracket (2). Torque nut
(4) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (1) with bracket (2).
(2) Install bolt (5) through washer (6), bushing
(7), bracket (2), and bellcrank (1).
(3) Check fit of self-retaining bolt (5) (para 11.1).
(4) Install nut (4). Torque nut (4) 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 (3).
c. Inspect (QA).
d. Perform lateral flight control rigging mainte-
nance operational check (TM 1-1520-238-T).
e. Install access covers B80L and B85L (para
2.2).
END OF TASK
M04-4322-5
9
10
2
8
M04-4322-6
5
6
4
3
2
7
1
