TM 55-1520-240-23-9
11-42
RIG COCKPIT CONTROL ASSEMBLIES
(Continued)
11-42
28.
Working in cockpit, remove cotter pin (47),
nut (48), two washers (49), and bolt (50) from
bellcrank (51).
29.
Disconnect link (52) from bellcrank (51). Move
link aft.
30.
Loosen nut (53) on link (52).
31.
Lift yoke (27) and position between grip (28) and
first rivet (29) from grip of pilot’s control stick
(31). Install yoke pin (30) in yoke.
32.
Turn rod end (54) of link (52) until link can be
positioned in bellcrank (51) with bolt (50) installed
loosely.
33.
Torque nut (54) of link (52) to 103 inch-pounds.
34.
Install bolt (50), two washers (49), and nut (48)
in bellcrank (51).
35.
Torque nut (48) to 30 to 45 inch-pounds. Install
cotter pin (47).
36.
Check bolt (50). 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 35.
INSPECT
11-168
