REMOVE AFT LCT CONNECTING LINK
Aircraft Mechanics Tool Kit, NSN 5180-00-323-4692
Paper Tags (E264)
Medium Helicopter Repairer (2)
Battery Disconnected (Task 1-39)
Hydraulic Power Off
Electrical Power Off
Aft Pylon Work Platforms Open (Task 2-2)
Aft Rotor Pitch Links Disconnected (Task 5-97)
Safety Blocks (T31) Installed (Task 11-28)
Positive retention bolts are installed
in upper controls. Bolts have a pawl
which prevents nut or bolt removal
unless pawl is depressed (Task 1-13).
Attaching bolts, washers and nuts will
be temporarily installed after removing
connecting link and actuator.
If a crack in the connecting link or
yoke is suspected during removal,
refer to TM 1-1520-253-23.
Remove cotter pin (1), nut (2), washers (3), and
tilt (4) attaching LCT actuator (5) to yoke (6).
Support yoke (6) with wood block (7).