TM 1-1520-238-23
11-499
11.113.
LONGITUDINAL F.S. 82.80 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.113.6. Installation
CAUTION
To prevent damage to flight control sys-
tem components, do not use force to
aline bellcrank with bracket or to aline
push-pull 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
1
11
1213
M04-4306-5
10
9
8
