TM 1-1520-238-23
11-528
11.120.
CPG TO PILOT LONGITUDINAL F.S. 118.50 CONTROL FLIGHT BRACKET ASSEMBLY
REMOVAL/INSTALLATION – continued
b. Install bellcrank (2) on bracket (8). Torque nut
(10) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (2) with bracket (8).
(2) Install bolt (11) through washer (12), bushing
(13), bracket (8), and bellcrank (2).
(3) Check fit of self-retaining bolt (11) (para 11.1).
(4) Install nut (10). Torque nut (10) 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 (9).
c. Install rod (1) on bellcrank (2). Torque nut (4) 30
to 40 INCH-POUNDS.
(1) Aline rod (1) with bellcrank (2).
(2) Install bolt (5) through washer (6), bushing
(7), bellcrank (2), and rod (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).
d. Inspect (QA).
e. Perform longitudinal flight control rigging
maintenance
operational
check
(TM 1-1520-238-T).
f. Install flex chute, turret, and area weapon
(TM 9-1090-208-23).
END OF TASK
2
10
9
11
12
13
8
M04-4326-7
M04-4326-8
2
1
7
4
3
6
5
