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designed for partially submerged operation, non positive displacement, hydraulic motor driven, single stage impeller, 2600 psi input, 125 psi discharge hydraulic fluid pressures, 25000 phr at 10 psi rated output for JP4, JP5 fuel, 40.910 in. lg by 7.620 in. w by 5.550 in. h o/a dim., 8 holes 0.271 in. dia evenly spaced around a 7.620 in. by 5.550 in. oval slanted mtg flange, external sq flange discharge fitting for 1.375 in. id connection, modified clamp and tubes, carbon shaft seal
1EA
Schedule B number: 8803300060
nmfc 011790
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.
1. | 60-123CAX | Cage 81982 |
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.