TM 1-1520-238-23
11-562
11.127. LONGITUDINAL F.S. 164.38 PUSH-PULL ROD REMOVAL/INSTALLATION – continued
11.127.6. 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 rod (13) on servocy-
linder (22). Torque nut (24) 30 to 40 INCH-
POUNDS.
(1) Aline rod (13) with clevis (27).
(2) Install bolt (25) through washer (26), clevis
(27), and rod (13).
(3) Check fit of self-retaining bolt (25) (para
11.1).
(4) Install nut (24). Torque nut (24) to 30 INCH-
POUNDS. Use torque wrench.
(5) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(6) Install cotter pin (23).
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22
25
26
27
13
24
M04-3592-6
29
23
