MAIN LANDING GEAR INSPECTION continued
k. Check pivot landing gear bolts for broken torque stripe.
l. Check bore of main landing mounts for corrosion. Remove corrosion (para 1.49). Ensure that inside
diameter of bore does not exceed 0.950 INCH after removal of corrosion.
m. Check shock strut plated surface area for corrosion. Remove corrosion (para 3.18).
3.1.4. General (Fittings, Castings, Forgings)
a. Nicks, scratches, and gouges which do not develop into cracks are generally acceptable if sharp
edges can be blended and damage does not interfere with operational characteristics of the affected
b. Remove minimal material to smooth sharp edges if blending is required.
c. Check for cracks.
(1) If cracks are suspected, perform nondestructive inspection (TM 1-1520-264-23).
END OF TASK