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 5910-00-334-6454
NSN 5965-00-265-7861
NSN 5990-00-356-8911
NSN 6150-01-040-3510
NSN 6150-00-959-9958
NSN 5905-01-261-5314
NSN 6320-01-362-9518
NSN 5915-01-106-7592
NSN 6320-00-538-2132
NSN 6110-01-606-3584
NSN 5915-00-911-9893
NSN 6105-00-311-0449