TM 1-1520-238-23
11-504
11.114.
CPG TO PILOT LONGITUDINAL F.S. 82.80 CONTROL BRACKET
REMOVAL/INSTALLATION – continued
c. Install rod (1) on bellcrank (2). Torque nut (4) 30
to 40 INCH-POUNDS.
(1) Aline rod (1) with bellcrank (2).
(2) Install bolt (5) through washer (6), bushing
(7), bellcrank (2), and rod (1).
(3) Check fit of self-retaining bolt (5) (para 11.1).
(4) Install nut (4).Torque nut (4) 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 (3).
d. Inspect (QA).
e. Perform longitudinal flight control rigging
maintenance
operational
check
(TM 1-1520-238-T).
f. Install access covers B80R and B85R (para
2.2).
END OF TASK
M04-4332-8
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