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 2925-01-299-6967
NSN 5905-00-523-8458
NSN 2925-01-277-5882
NSN 5915-00-249-1641
NSN 6620-01-628-0171
NSN 5996-01-070-9677
NSN 6105-00-006-4184
NSN 6105-01-652-3856
NSN 6610-01-551-6425
NSN 6150-01-487-3818
NSN 4140-01-585-8374
NSN 5895-01-129-8749