TM 1-1520-238-23
11-1044
11.247.
DIRECTIONAL F.S. 199.25 PUSH-PULL ROD REMOVAL/INSTALLATION – continued
b. Install rod (1) on aft bellcrank (2). Torque nut
(4) 30 to 40 INCH-POUNDS.
(1) Aline rod (1) with bellcrank (2).
(2) Install bushing (7) in bellcrank (2).
(3) Install bolt (5) through washer (6), bushing
(7), bellcrank (2), and rod (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. Inspect (QA).
d. Perform directional flight control rigging op-
erational check (TM 1-1520-238-T).
e. Install access panel L200 (para 2.2).
END OF TASK
M04-1796-5
1
6
5
3
7
4
2
