TM 55-1520-240-23-9
11-77
ASSEMBLE PILOT’S COCKPIT CONTROL ASSEMBLY
(Continued)
11-77
149.
Position cylinder (310) in upper mount (311),
ports (312) forward.
150.
Install bolt (313), two washers (314 and 315), and
nut (316). Torque nut to 30 to 60 inch-pounds.
Install cotter pin (317).
151.
Position cylinder (310) in arm (15).
152.
Install bolt (318), two washers (319 and 320), and
nut (321). Torque nut to 30 to 60 inch-pounds.
Install cotter pin (322).
153.
Position cylinder (323) in upper mount (324),
ports (325) forward.
154.
Install bolt (326), two washers (327 and 328), and
nut (329). Torque nut to 30 to 60 inch-pounds.
Install cotter pin (330).
155.
Position cylinder (323) in arm (16).
156.
Install bolt (331), two washers (332 and 333), and
nut (334). Torque nut to 30 to 60 inch-pounds.
Install cotter pin (335).
157.
Rig control assembly (336) (Task 11-42).
158.
Torque two nuts (296 and 301) to 30 to 60
inch-pounds. Install corner pins (337 and 338).
159.
Check bolts (293 and 298). Bolts shall not rotate
with torque less than 10 inch-pounds. There
shall be no axial looseness. If bolt rotates or is
loose, add washer under nut and repeat step
158.
11-381
