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designed for fully and partially submerged operation; pos displacement type pump; pump data, 1 impeller, single stage, pump capacity rating, 600 phr, max rated capacity at min psi, 7 psi, min pressure at max rated capacity; horizontal design; horizontal design dim. data, 2.500 in. lg o/a between ends parallel to shaft axis, 5.650 in. h o/a from bottom of mount to top, 3.750 in. w o/a perpendicular to h; cw rotation; inlet opening w/strainer; outlet connection data, 1 connection /discharge port/, MS33649-10, external discharge, thd connections, 7/8 in.-14 UNF-3B thd designation, internal thd, rh thd, stationary design, not flanged connections, 1 connection /seal drain port/, MS33649-4, external discharge; outlet connection data, thd connections, 7/16-20 UNF-3B thd designation, internal thd, rh thd, stationary design, not flanged connections; mounting data, FIXED-Flanged mtg, no govt spec or std mating flange, 7 bolt holes, 0.287 in. max, 0.280 in. min dia bolt holes, 1.811 in. c to c between bolt holes; electr
1EA
Schedule B number: 8803300060
nmfc 011760
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.
Nothing similar to this part number was found in our inventory
A completely inclosed machine consisting of a positive or nonpositive displacement pump with a driving motor used to transmit or transfer fluid from an aircraft tank to an engine driven pump or to another tank. it is designed to be partially or completely submerged in the fluid it is intended to pump.