TM 1-1520-238-23
11-1074
Change 5
11.256.
DIRECTIONAL F.S. 275 PUSH-PULL ROD REMOVAL/INSTALLATION – continued
11.256.6. Installation
CAUTION
To prevent damage to flight control sys-
tem components, do not use force to
aline push-pull rod with bellcrank.
a. Install adjustable end of directional control
rod (8) on aft bellcrank (2). Torque nut (14) 30 to
40 INCH-POUNDS.
(1) Aline rod (8) with bellcrank (2).
(2) Install bushing (16).
(3) Install bolt (15) through bellcrank (2), rod (8),
and bushing (16).
(4) Check fit of self-retaining bolt (15) (para
11.1).
(5) Install nut (14). Torque nut (14) 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 (13).
GO TO NEXT PAGE
M04-1800-7A
16
13
14
8
15
2
