TM 55-1520-240-23-9
11-88
INSTALL COCKPIT CONTROL TRANSFER BELLCRANKS
(Continued)
11-88
51.
Torque nuts (31, 37, 42, 47, 52, 58, 64, 68, 74,
80, 86, and 90) to 30 to 46 inch-pounds. Install
cotter pins (96, 97, 98, 99, 100, 101, 102, 103,
104, 105, 106, and 107).
52.
Check bolts (34, 40, 46, 60, 66, 61, 67, 72, 77,
83, 88, and 93). Bolts shall not rotate with torque
less than 10 inch-pounds. There shall be no
axial looseness. If bolts rotate or are loose, add
washer under nut and repeat step 51.
INSPECT
FOLLOW-ON MAINTENANCE:
Connect forward and aft connecting links to
servocylinders (Task 11-193).
Remove servocylinder safety blocks (Task 11-29).
Perform operational check of flight controls (TM
55-1520-240-T).
Install closet acoustic blanket (Task 2-108).
END OF TASK
11-477