TM 55-1520-240-23-9
11-42
RIG COCKPIT CONTROL ASSEMBLIES
(Continued)
11-42
37.
Working through left access (36), turn rod end
(55) of link (44) until link can be positioned in
bellcrank (45) with bolt (43) installed loosely.
38.
Torque nut (46) of link (44) to 103 inch-pounds.
39.
Install bolt (43), washer (42), and nut (40) in
bellcrank (45).
40.
Torque nut (41) to 30 to 45 inch-pounds. Install
cotter pin (40).
41.
Check bolt (43). 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 (40).
42.
Working in cockpit, check control stick position
indicator (56). Indicator must indicate 1 division
forward of N, if not adjust indicator (Task 11-45).
11-169