U/a: cylinder, main landing gear strut; alum alloy 7075f, 28.820in o/a lg, 19.180in o/a wd, 4.120 in o/a h
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 5990-00-067-6791
NSN 5999-01-431-8589
NSN 6610-01-408-7827
NSN 5930-01-024-9382
NSN 6240-01-009-4665
NSN 5985-00-088-0695
NSN 5960-01-560-8461
NSN 6110-01-384-1309
NSN 5915-01-574-0214
NSN 6145-01-647-8838
NSN 5910-01-251-9592
NSN 5960-01-408-2062