TM 1-1520-238-23
Change 7
11-731
11.166.
DIRECTIONAL F.S. 156.07 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION continued
11.166.6. Installation
a. Install rod (1) on bellcrank (10). Torque nut (12)
30 to 40 INCH-POUNDS.
(1) Aline rod (1) with bellcrank (10).
(2) Install bolt (13) through washer (14), bushing
(15), bellcrank (10), and rod (1).
(3) Check fit of self-retaining bolt (13) (para
11.1).
(4) Install nut (12). Torque nut (12) 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 (11).
b. Install rod (1) on bellcrank (2). Torque nut (7) 30
to 40 INCH-POUNDS.
(1) Aline rod (1) with bellcrank (2).
(2) Install bolt (3) through washer (8), bushing
(9), bellcrank (2), and rod (1).
(3) Check fit of self-retaining bolt (3) (para 11.1).
(4) Install nut (7). Torque nut (7) 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 (6).
c. Inspect (QA).
d. Perform flight control system maintenance
operational check (TM 1-1520-238-T).
e. If removed install forward fuel cell retainer
panel (para 10.52A).
f. Install access cover L160 (para 2.2).
END OF TASK
3
7
6
9
8
15
1
4
13
14
11
12
2
10
M04-5091-3
5