TM 1-1520-238-23
11-610
11.137. COLLECTIVE F.S. 161.60 BELLCRANK 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 (7) on bracket (13). Torque nut
(15) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (7) with bracket (13).
(2) Install bolt (16) through washer (17), bushing
(18), bracket (13), and bellcrank (7).
(3) Check fit of self-retaining bolt (16) (para
11.1).
(4) Install nut (15). Torque nut (15) 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 (14).
c. Install rod (6) on bellcrank (7). Torque nut (9) 30
to 40 INCH-POUNDS.
(1) Aline rod (6) with bellcrank (7).
(2) Install bolt (10) through washer (11), bushing
(12), bellcrank (7), and rod (6).
(3) Check fit of self-retaining bolt (10) (para
11.1).
(4) Install nut (9). Torque nut (9) 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 (8).
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