REMOVE YAW, THRUST, PITCH OR ROLL INTERMEDIATE CONNECTING LINKS
Aircraft Mechanics Tool Kit, NSN 5180-00-323-4692
Medium Helicopter Repairer
Battery Disconnected (Task 1-39)
Electrical Power Off
Hydraulic Power Off
Servocylinder Safety Blocks (T31) Installed (Task
Closet Acoustic Blanket Removed (Task 2-107)
Closet Backup Panel Removed (Task 2-2)
Forward Transmission Drip Pan Removed (Task 2-3)
Procedure is same to remove yaw,
thrust, pitch or roll intermediate
connecting links. Pitch connecting link
is shown here.
Attaching bolts, washers, and nuts will
be temporarily installed after removing
If a crack in the intermediate
connecting link or bellcrank is
suspected during removal, refer to TM
Remove Cotter pin (1), nut (2), two washers
(3), and bolt (4) from lug (5) of bellcrank (6).
Disconnect pitch intermediate connecting link
(7) from bellcrank.
Install bolt (4), two washers (3), and nut (2)
loosely in lug (5) and bellcrank (6).
Remove cotter pin (8), nut (9), two washers (10),
and bolt (11) from bellcrank (12). Remove link
Install bolt (11), two washers (10), and nut (9)
loosely in bellcrank (12).
FOLLOW ON MAINTENANCE:
END OF TASK