TM 55-1520-240-23-9
11-244
REMOVE AFT FUSELAGE CONNECTING LINKS
(Continued)
11-244
NOTE
Procedure is same for forward end of
left and right connecting link. Right
side connecting link at sta. 444.5 is
shown here.
7.
Remove cotter pin (12), nut (13), two washers
(14), and bolt (15).
8.
Remove connecting links (1 or 7) from fuselage
idler bellcrank (16). Install bolt (15), two washers
(14), and nut (13) in bellcrank.
FOLLOW-ON MAINTENANCE:
None
END OF TASK
11-952
