TM 1-1520-238-23
11-625
11.140.
COLLECTIVE F.S.164.95 BELLCRANK REMOVAL/INSTALLATION – continued
b. Install rod (8) on bellcrank (2). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Position rod (8) on bellcrank (2) to aline bolt
hole and bushing (13) in 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) Position rod (1) on bellcrank (2) to aline bolt
hole and bushing (7) in 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 collective flight controls rigging
maintenance
operational
check
(TM 1-1520-238-T).
f. Install transformer-rectifier No. 2 (para 9.32).
END OF TASK
13
12
11
M04-3562-8
2
8
10
9
1
7
2
M04-3562-9
6
5
4
3
