TM 1-1520-238-23
11-396
11.89.
CPG TO PILOT CONTROL LATERAL F.S. 83.45 IDLER BELLCRANK
REMOVAL/INSTALLATION – continued
11.89.6. Installation
CAUTION
To prevent damage to flight control sys-
tem components, do not use force if bind-
ing or roughness occurs while moving
controls with hydraulic power.
a. Install bellcrank (2) on bracket (14). Torque nut
(16) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (2) with bracket (14).
(2) Install bolt (17) through washer (18), bushing
(19), bracket (14), and bellcrank (2).
(3) Check fit of self-retaining bolt (17) (para
11.1).
(4) Install nut (16). Torque nut (16) 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 (15).
b. Install rod (8) on bellcrank (2). Torque nut (10)
30 to 40 INCH-POUNDS.
(1) Aline rod (8) with bellcrank (2).
(2) Install bolt (11) through washer (12), bushing
(13), bellcrank (2), and rod (8).
(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).
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M04-4344-6
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