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main fuel pump, 708000, for F100 aircraft engine
used on relief valve, p/n 217327
alum alloy 6061-T651 per AMS4129, anodized; 2.040 in. l; first end 1.045 in. od 0.190 in. dp, flatted 0.746 in. w, 0.070 in. dia hole thru side center; 1.250-16UNJ-3A thd; other end 1.120 in. od 0.76, external groove 0.136 - 0.142 in. w 0.968 - 0.972 in. dia 0.061 in. from end, center bore 0.855 in. dia 1.185 in. dp, 0.780 in. dia 0.205 in. dp, 0.435 in. dia 0.235 in. dp
1EA
Schedule B number: 8803300060
nmfc 013680
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 main fuel pump,708000,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).