TM 55-1520-240-23-9
11-207
REMOVE FORWARD LCT CONNECTING LINK
11-207
INITIAL SETUP
Applicable Configurations:
All
Tools:
Aircraft Mechanic’s Tool Kit, NSN 5180-00-323-4692
Materials:
Dry Cleaning Solvent (E162)
Cloth (E120)
Gloves (E186)
Personnel Required:
Medium Helicopter Repairer
References:
TM 1-1520-253-23
Task 1-13
Equipment Condition:
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
11-28)
Do not use cadmium plated hardware
or tools while working on yoke
assembly. Titanium yoke could be
damaged.
NOTE
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.
NOTE
If a crack in the connecting link or
yoke is suspected during removal,
refer to TM 1-1520-253-23.
1.
Remove cotter pin (1), nut (2), washer (3),
and bolt (4) attaching connecting link (5) to
swashplate (6).
11-824
