REMOVE FORWARD LCT CONNECTING LINK
Aircraft Mechanics Tool Kit, NSN 5180-00-323-4692
Dry Cleaning Solvent (E162)
Medium Helicopter Repairer
Battery Disconnected (Task 1-39)
Electrical Power Off
Hydraulic Power Off
Forward Pylon Work Platforms Open (Task 2-2)
Forward Rotor Pitch Links Disconnected (Task 5-97)
Servocylinder Safety Block (T31) Installed (Task
Do not use cadmium plated hardware
or tools while working on yoke
assembly. Titanium yoke could be
If general cleaning is required before
disassembly, use solvent (E162), cloth
(E120), gloves (E186).
Positive retention bolts are installed in
upper controls. Bolts have 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
actuator and connecting link.
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), washer (3),
and bolt (4) attaching connecting link (5) to