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unified fuel control, F100 eng
used on ignition switch lever shaft, outer body assy
cres, 0.94 in. l o/a; hex one end 0.10 in. across flats, 0.13 in. l; 0.164-32UNJC-3A rolled thd 0.19 in. from end 0.392 in. lg; other end 0.63 in. max od, 0.28 in. thk, cut thru 0.10 inw 0.09 in. parallel from end, flatted top and bottom w/0.15 in. w slot 0.41 in. dp from top
1EA
Schedule B number: 8803300060
nmfc 133320
Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts the
FSC 2915 ⁓ Engine fuel system components, aircraft and missile prime movers
Note-fuel components specially designed for propulsion fuel systems, aircraft and missiles are to be placed in this fsc.
Excluding aircraft fuel tanks (fsc 1560); in-flight refueling system fuel components (fsc 1680). fuel system components not specifically designed for use with aircraft engines or missile prime-movers.
Used on unified fuel control,f100 eng.
Nothing similar to this part number was found in our inventory
A regulating device threaded or unthreaded for the purpose of tuning the mechanism for which it is specifically designed. it may have a limiting collar, shoulder or slot. the rotating facility may be a hex head or collar, a slot or socket end. excludes bolt (as modified); screw (as modified); stud (as modified).