TM 1-1520-238-23
11-581
11.131.
CPG COLLECTIVE F.S. 118.50 PUSH-PULL ROD ASSEMBLY
REMOVAL/INSTALLATION – continued
b. Install rod end (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).
(5) Torque nut (4) 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 (3).
c. Inspect (QA).
d. Perform longitudinal flight control rigging
maintenance
operational
check
(TM 1-1520-238-T).
e. Install flex chute, turret, and area weapon
(TM 9-1090-208-23).
END OF TASK
1
7
4
3
M04-5089-5
5
6
2
