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F111A aircraft engine fuel system
pressures, 12 psig operating, 24 psig proof and 36 psig burst, 2.500 in. o/a lg, flange w/2 EARED-Holes 0.228 in. min to 0.286 in. max dia spaced 1.405 inc c to c
1EA
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 f111a aircraft engine fuel system.
1. | C432-1 | Cage 81755 |