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aircraft engine model R3350-93
X4.952 in. lg. o/a; mtg flange, TF1296, w/2 holes 0.265 - 0.275 in. dia, 2.031 in. nom C-TO-C; tang driver, TF2220, 0.145 - 0.150 in. w; relief valve cover, TF1146-2, 2.031 in. by 2.125 in; 2 ports 3/8 npt, 1.52 in. max l cen to flange base
engine fuel system components, aircraft
1EA
Schedule B number: 8803300060
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 aircraft engine model r3350-93.
Nothing similar to this part number was found in our inventory
A positive displacement pump specifically designed to force a measured amount of fuel to the intake manifold or combustion chamber of an internal combustion engine. it is designed for mounting to a bulkhead or panel. it may be furnished with attaching fittings and/or spacers which control capacity. excludes dispensing pump, hand driven.