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F111A aircraft engine fuel system
aluminum alloy, cres, polytetrafluoroethylene, armalon and silicone rubber w/anodized and passivated finish, max flow rate 75000 pph, pressure regulation 17.5 to 19.5 psig, proof 120.0 psig, burst 180.0 psig, approx 6.900 in. o/a lg, 2 pressure ports per AND10050-6, includes protective caps and plugs, screen and ring, internal retainer
Schedule B number: 8481809050
nmfc 051080
Other taps, cocks, valves, etc.
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.