U/a: nose landing gear cylinder; matl: alum alloy ams4111 7049-t73, anodize finish as noted, 52.500in. O/a lg, 7.500in. Od, 5.625in. Id; shot peen surfaces as noted, heat treat 72000psi tensile strength 61000psi yield strength
The main shock absorption portion of an aircraft landing gear, consisting of the main cylinder and piston and other associated parts. May be with or without axle(s). Excludes landing gear, fixed and landing gear, retractable.
Classification: Undercarriages and parts thereof, for use in military aircraft
NSN 5920-01-223-3734
NSN 5915-00-701-7150
NSN 5930-01-529-6866
NSN 4140-00-189-0235
NSN 5895-00-765-9615
NSN 5975-01-360-0688
NSN 5905-00-403-5793
NSN 5905-01-461-7684
NSN 5930-01-253-6421
NSN 5950-01-267-7780
NSN 4140-00-103-9728
NSN 6110-01-473-0426