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 6240-01-592-4068
NSN 7035-01-309-2219
NSN 6610-01-364-0294
NSN 6240-01-273-0193
NSN 6110-01-020-8153
NSN 5930-00-586-4712
NSN 5985-01-457-2957
NSN 6105-01-472-9147
NSN 5935-01-082-1001
NSN 5855-01-100-3272
NSN 5930-00-132-4403
NSN 6145-01-562-8155