TM 55-1520-240-23-9
11-78
ASSEMBLE COPILOTS COCKPIT CONTROL ASSEMBLY
(Continued)
11-78
95.
If pitch connecting link (193) is a replacement,
loosen nut (194) of adjustable end. Turn bearing
(195) 90º to bearing (196). Torque nut to 100
inch-pounds.
96.
Position link (193) in socket (128), fixed end
toward socket. Install bolt (197) two washers
(198 and 199), and nut (200). Do not tighten nut
at this time.
97.
Position link (193) in bellcrank (18). Install bolt
(201), two washers (202 and 203), and nut (204).
Do not tighten nut at this time. Remove tag from
link.
11-397