TM 1-1520-238-23
11-724
Change 7
11.164.
DIRECTIONAL F.S. 121.40 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
b. Install rod end (1) on bellcrank (2). Torque nut
(4) 30 to 40 INCH-POUNDS.
(1) Install bushing (8) in bellcrank (2).
(2) Aline rod end (1) with bellcrank (2).
(3) Install bolt (5) through washer (6), bushing
(7), bellcrank (2), and rod end (1).
(4) Check fit of self-retaining bolt (5) (para 11.1).
(5) Install nut (4). 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. Install directional F.S. 121.40 bellcrank (para
11.151).
d. Inspect (QA).
e. Perform directional flight control rigging
maintenance
operational
check
(TM 1-1520-238-T).
f. Install
area
weapon
and
turret
(TM 9-1090-208-23).
g. If removed install forward fuel cell retainer
panel (para 10.52A).
END OF TASK
2
6
1
3
4
8
7
5
M04-4374-7
