TM 1-1520-238-23
11-1051
11.250.
DIRECTIONAL F.S. 216.25 BELLCRANK INSTALLATION – continued
11.250.3. 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 directional control bellcrank (1) on
bracket (2). Torque nut (3) 30 to 40 INCH-
POUNDS.
(1) Position spacer (4) and bearing (5) in bell-
crank (1).
(2) Aline bellcrank (1) with bracket (2).
(3) Install bushing (6) in bellcrank (1).
(4) Install bolt (7) through bellcrank (1), bushing
(6), spacer (4), and bracket (2).
(5) Check fit of self-retaining bolt (7) (para 11.1).
(6) Install nut (3). Torque nut (3) to 30 INCH-
POUNDS. Use torque wrench.
(7) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(8) Install new cotter pin (8).
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