TM 1-1520-238-23
11-1137
11.269. DIRECTIONAL F.S. 520 PUSH-PULL ROD REMOVAL/INSTALLATION – continued
11.269.6. 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 adjustable end of push-pull rod (3) on
lower bellcrank (4). Torque nut (1) 30 to 40
INCH-POUNDS.
(1) Aline rod (3) with bellcrank (4).
(2) Install bolt (2) through bushing (6), bellcrank
(4) and rod (3).
(3) Check fit of self-retaining bolt (2) (para 11.1).
(4) Install nut (1). Torque nut (1) 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 (5).
NOTE
Do not apply sealing compound to spheri-
cal bearing.
(7) Apply sealing compound to head of bolt (2)
and nut (1). Use sealing compound
(item 178, App F).
GO TO NEXT PAGE
6
5
1
3
2
4
M04-1760-4
