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pump, fuel transfer
boeing spec no. 10-2448-3
a mechanical/electrical device used to transfer fuel from acft fuel tank to another when installed will provide a positive volume fo fuel under pressure
t.o.1C-135A-4, figure 802
cpump unit, centrifugal; max. discharge flow rate 150.0 gpm; total head 135.0 ft; operating speed at rated capacity 2750.0 rpm; media for which designed hydrocarbon fuels and oils; pumping element operating position horizontal; pump rotation direction counterclockwise; pump design radial flow; impeller qty 1; impeller suction type double; stage qty 1; submersible with strainer; discharge connection 1 round flange; drive connection type close coupled
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.
boeing spec no. 10-2448-3 pump, fuel transfer
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.