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unified fuel control for F100 aircraft eng
used with pla trim shaft in gas generator body assy
3cres, 1.84 in. l o/a; 0.18 in. od one end w/0.05 in. thk flange 0.43 in. dia 0.49 in. from end, slot 0.06 in.w x 0.22 in. dp; no.6-40UNJF-3A lh thd 0.83 in. l w/end tip 0.09 in. od, 0.19 in. l; hex 0.26 in. max across, 0.10 in. w 1.02 in. from tip
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 for f100 aircraft 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).