TM 1-1520-238-23
11-508
11.115.
CPG TO PILOT CONTROL LONGITUDINAL F.S. 96.59 BELLCRANK
REMOVAL/INSTALLATION – continued
b. Install rod (8) on bellcrank (2). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Aline rod (8) with bellcrank (2).
(2) Install bolt (11) through washer (12), bushing
(13), bellcrank (2), and rod (8).
(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
8
M04-4342-7
11
1213
9
2
10
M04-4342-8
2
1
5
7
4
3
6
