TM 1-1520-238-23
11-532
Change 7
11.121.
LONGITUDINAL F.S. 129.25 BELLCRANK REMOVAL/INSTALLATION – continued
b. Install rods (9) and (8) on bellcrank (2). Torque
nut (11) 30 to 40 INCH-POUNDS.
(1) Aline rod (9) with bellcrank (2).
(2) Install bushing (15).
(3) Aline rod (8) with bellcrank (2).
(4) Install bolt (12) through washer (13), bushing
(14), bellcrank (2), rod (8), and rod (9).
(5) Check fit of self-retaining bolt (12) (para
11.1).
(6) Install nut (11). Torque nut (11) to 30 INCH-
POUNDS. Use torque wrench.
(7) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(8) Install new cotter pin (10).
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. If removed install forward fuel cell retainer
panel (para 10.52A).
END OF TASK
11
10
8
13
14
12
M04-4369-7
15
9
4
3
M04-4369-8
5
6
7
1
2
