INSPECT FORWARD LANDING GEAR
Technical Inspection Tool Kit, NSN 5180-00-323-5114
Magnetic Particle Method
Battery Disconnected (Task 1-39)
Electrical Power Off
Hydraulic Power Off
Access Panel Open (Task 2-2)
This procedure is same for left or right
Check seal of shock strut (1) for hydraulic leaks.
There shall be no leaks.
Check shock strut (1) air pressure and extension
Inspect shock strut piston tube (3) for corrosion.
Inspect tube (3). There shall be no cracks,
scoring or pitting. If a crack on the surface
of the strut piston is suspected, refer to TM
Inspect torque arm (4). There shall be no cracks
or excessive play. Permit up to 0.015 inch axial
play after lubrication. This play will not affect the
normal operation of the landing gear. If a crack
on the surface of the torque arm is suspected,
refer to TM 1-1520-253-23.
END OF TASK