TM 1-1520-238-23
3-66
Change 8
3.18.
MAIN LANDING GEAR SHOCK STRUT REMOVAL/INSTALLATION – continued
3.18.7. Installation
WARNING
To prevent injury to personnel or dam-
age to equipment, ensure that strut is
in fully extended position and the read
ring on the shock strut is visible. En-
sure fuse collar is in “LOCKED” posi-
tion and the “WARNING – REMOVE
ONLY FOR KNEELING” arrow is alined
with lock pin. Unpinned or improper
position of collar can result in sudden
helicopter tilt or drop when jack is re-
moved. If injury occurs, seek medical
aid.
a. Apply a thin coat of lubricant to the interior
surface of rod end bearing (21), spider mount
shaft (7), and washer (22) surfaces which
touch the rod end bearing. Use antiseize
compound (item 26, App F).
b. Install inboard washer (22) on shaft (7) with
chamfered surface of washer inboard against
landing gear mount (23).
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M04-053-11
FULLY
EXTENDED
INDICATOR
(RED STRIPE)
LOCK
PIN
FUSE COLLAR IN
LOCKED POSITION
FUSE COLLAR IN
UNLOCKED POSITION
7
22
23
M04-053-12B
CHAMFER
7
22
23
ADL
ADM
ADN
7
22
23
