TM 1-1520-238-23
11-400
11.90.
LATERAL F.S. 83.45 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.90.6. Installation
CAUTION
To prevent damage to flight control com-
ponents, do not use force in alining rod
with bellcrank.
a. Install rod (1) on bellcrank (8). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Aline rod (1) with bellcrank (8).
(2) Install bolt (11) through washer (12), bushing
(13), bellcrank (8), and rod (1).
(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).
GO TO NEXT PAGE
10
9
12
11
8
1
13
M04-4304-5
