TM 55-1520-240-23-9
11-80
RIG PILOTS COCKPIT CONTROL ASSEMBLY
(Continued)
11-80
30.
Leave rigging pin (25) in bellcrank (27).
31.
Remove cotter pin (45), nut (46), two washers
(47 and 48), and bolt (49) from bellcrank (43)
and link (50).
32.
Insert rigging pin (41) fully through bellcrank (43)
connecting link and into hole (44).
33.
Loosen nut (51) of link (50).
34.
Turn rod end (52) until link can be positioned
in bellcrank (43) with pin (41) fully and freely
inserted through bellcrank, link, and hole.
35.
Connect link (50) to bellcrank (43). Install bolt
(49), two washers (48 and 47), and nut (46).
36.
Torque nut (46) to 30 to 45 inch-pounds. Install
cotter pin (45).
37.
Check bolts (49). Bolt 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 36.
38.
Torque nut (51) to 103 inch-pounds.
39.
Remove two pins (25 and 41) from bellcranks
(27 and 43).
INSPECT
11-418