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 6320-01-173-7950
NSN 5945-01-244-3948
NSN 5905-00-339-7225
NSN 6220-00-448-3522
NSN 5975-01-138-2591
NSN 2925-01-341-9400
NSN 6135-01-360-1620
NSN 5996-00-549-4258
NSN 5925-00-644-5546
NSN 6105-01-258-2314
NSN 5985-01-231-4254
NSN 5920-01-502-0874