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F100-PW100 aircraft turbofan engine
cres, o/a dim. approx 3.870 in. min to 3.891 in. max lg, circular eared flange w/6 inserts size 0.190-32 UNJF-3B, equally spaced, 3 inlets 1.250 in. dia, 1.120 in. dia and 2.3450 in. min to 2.3752 in. max dia
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 f100-pw100 aircraft turbofan engine.