TM 1-1520-238-23
11-600
11.135. COLLECTIVE F.S. 161.54 BRACKET ASSEMBLY REMOVAL/INSTALLATION – continued
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.
b. Install bellcrank (10) on bracket (16). Torque
nut (18) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (10) with bracket (16).
(2) Install bolt (19) through washer (20), bushing
(21), bracket (16), and bellcrank (10).
(3) Check fit of self-retaining bolt (19) (para
11.1).
(4) Install nut (18). Torque nut (18) 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 (17).
c. Install rod (9) on bellcrank (10). Torque nut (12)
30 to 40 INCH-POUNDS.
(1) Aline rod (9) with bellcrank (10).
(2) Install bolt (13) through washer (14), bushing
(15), bellcrank (10), and rod (9).
(3) Check fit of self-retaining bolt (13) (para
11.1).
(4) Install nut (12). Torque nut (12) 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 (11).
d. Inspect (QA).
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