TM 1-1520-238-23
11-491
11.111.
PILOT CYCLIC LONGITUDINAL PUSH–PULL ROD ASSEMBLY
REMOVAL/INSTALLATION – continued
11.111.6. 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 (5) on arm (12).
Torque nut (14) 30 to 40 INCH-POUNDS.
(1) Aline rod (5) with arm (12).
(2) Install bolt (15) through washer (16), bushing
(17), arm (12), and rod (5).
(3) Check fit of self-retaining bolt (15) (para
11.1).
(4) Install nut (14). Torque nut (14) 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 (13).
b. Install rod (5) on SPAD (6). Torque nut (8) 30 to
40 INCH-POUNDS.
(1) Aline rod (5) with SPAD (6).
(2) Install bolt (9) through washer (10), bushing
(11), SPAD (6), and rod (5).
(3) Check fit of self-retaining bolt (9) (para 11.1).
(4) Install nut (8). Torque nut (8) 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 (7).
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