Aluminum alloy, 24s-0, cond a, 17.406 in.Lg, first end, 1.229 in.Dia, second end, 1.728 in.Dia, 1 hole 0.687 in.Dia, 1 hole 0.375 in.Dia, 2 holes in line 0.242 in.Dia;
A lever used for maintaining control of an aircraft about its pitch and roll axis. Excludes operation of trim tabs or the like. It is distinguished from a control column in that its side to side movement controls the aircraft about its roll axis.
Classification: Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts thereof)
NSN 5920-01-464-4373
NSN 5855-00-688-9954
NSN 6620-00-452-5738
NSN 6610-00-269-4506
NSN 5930-00-070-5173
NSN 5985-00-673-5831
NSN 5930-00-064-2212
NSN 6145-01-452-7890
NSN 2925-00-497-7808
NSN 5910-01-519-3043
NSN 6320-00-164-4087
NSN 6145-01-332-3416