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unified fuel control for F100 aircraft engine
part of flow divider hsg and valve assy
cres, 1.53 in. l o/a; hex head one end 0.500 in. across flats, 0.22 in. h, cutout 0.19 in. w x 0.06 in. dp into slot thru hex side 0.28 in. w x 0.10 in. dp; 0.54 in. l tongue 0.19 in. wx 0.08 in. thk, 0.09 in. dia hole thru 0.10 in. CEN-TO-End; 0.250-28UNJF-3A rolled thd 0.29 in. l; 0.43 in. od collar 0.26 in. w with 0.094 in. w groove 0.32 in. dia 0.92 in. from tongue end
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 engine.
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).