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 6685-01-391-2611
NSN 7035-01-435-4009
NSN 6650-01-225-0176
NSN 6610-01-502-7820
NSN 5905-01-303-4909
NSN 5985-00-880-8856
NSN 5915-01-481-3999
NSN 5990-00-223-3258
NSN 6645-00-155-2398
NSN 6620-00-121-4632
NSN 5945-00-103-1767
NSN 5915-00-128-8808