TM 55-1520-240-23-9
11-158
INSTALL THRUST CCD ACTUATOR
(Continued)
11-158
8.
Position link (19) in arm (4). Install bolt (18), two
washers (17 and 16) and nut (15).
8.1.
Torque nut (15) to 30 inch-pounds. If necessary,
continue tightening to align cotter pin holes. Do
not exceed 45 inch-pounds. Install cotter pin
(19).
9.
Check bolt (18). 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 8.
10.
Connect spring (20) to forward end of arm (4)
(Task 11-132).
11.
Connect connector (21) to receptacle (22) of
actuator (1). Remove tag.
INSPECT
FOLLOW-ON MAINTENANCE:
Perform operational check of advance flight control
system (TM 55-1520-240-T).
Perform operational check of flight control system
(TM 55-1520-240-T).
Install closet backup panel (Task 2-2).
Install closet acoustic blanket (Task 2-108).
END OF TASK
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