TM 55-1520-240-23-9
11-77
ASSEMBLE PILOT’S COCKPIT CONTROL ASSEMBLY
(Continued)
11-77
160.
Torque eight nuts (222, 226, 234, 238, 243-247,
255, and 259) to 30 to 60 inch-pounds.
161.
Install eight cotter pins (339, 340, 341, 342, 343,
344, 345, and 346).
162.
Check eight bolts (219, 223, 231, 235, 240, 244,
252, and 256). 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 steps 160 and 161.
INSPECT
FOLLOW-ON MAINTENANCE:
None
END OF TASK
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