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F111 aircraft engine fuel system
aluminum alloy w/anodized finish, 2 gpm at 55 psid rated flow, pressures, operating 60 psi, proof 120 psi, burst 180 psi, 30 psi min reset pressure, 45 psi max cracking pressure, 0.810 in. o/a lg, 0.650 in. dia top end, 0.810 in. dia hex, end fitting inlet per MS33656E6, thd and 0.350 in. lg
Schedule B number: 8481809050
nmfc 127220
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 f111 aircraft engine fuel system.
1. | C491 | Cage 81755 |