TM 55-1520-240-23-9
11-42
RIG COCKPIT CONTROL ASSEMBLIES
(Continued)
11-42
15.
Remove two bolts (18 and 23) from bellcranks
(13 and 19). Slide link (14) right. Torque nut (24)
to 103 inch-pounds.
Bushings must be in bellcranks before
installing bolts; otherwise, damage to
components will result.
16.
Position link (14) in bellcranks (13 and 19). Install
two bolts (18 and 23), four washers (22 and 17),
and nuts (16 and 21) in bellcranks.
17.
Torque two nuts (16 and 21) to 30 to 45
inch-pounds. Install two cotter pins (15 and 20).
18.
Check two bolts (18 and 23). 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 17.
INSPECT
11-165