24.56 in. Min; 24.62 in. Max retracted; 42.64 in. Min, 42.70 in. Max extended; finish steel qq-p-416, cres/qq-p-35, alum/mil-a-8625; tension and compression 1100 lbs limit .733 lbs limit; contains internal spring for reducing sudden impact load due to bottomingout at full extension and upon entering snubbing cycle
A spring loaded and/or gas filled mechanism designed to exert an opposite force which will be used to absorb, dampen, and/or neutralize applied force. Excludes shock absorber, direct action; and shock absorber, lever action.
Classification: Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts thereof)
NSN 6220-01-634-0660
NSN 6320-01-036-2598
NSN 5835-01-442-6482
NSN 6685-00-852-4824
NSN 5975-01-596-4936
NSN 6610-00-001-9683
NSN 5975-01-559-0656
NSN 5935-01-457-6304
NSN 6685-00-162-8077
NSN 6240-01-035-8525
NSN 7035-01-256-6705
NSN 5925-01-210-9765