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designed for partially submerged operation, electrically operated, 28 volts , 18 to 30 volts range, direct current, electrical leads 20 ga, 12.0 in. min, no external leakage, 35.0 gph at 23 to 24 psi, 100 psig proof pressure, 25 to 35 psig pressure relief range, 27.5 psig max no flow pressure, for use with airplane gasoline, JP-4 and 5 and/or stoddard solvent, o/a dim. 2.560 in. dia by 6.100 in. min to 6.220 in. max lg, single inlet and outlet ports, front flange has 4 thd mtg studs size 10-32 UNF-3B spaced 1.375 in. and 1.750 in. c to c, sq flange mtd on front flange with center opening approx 1.230 in. dia, used as an auxiliary pump
1EA
Schedule B number: 8803300060
nmfc 128000
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. | 4140-00-15 | Cage 09445 |
2. | 1426033-3 | Cage 71379 |
3. | 18000-B | Cage 71379 |
4. | 18000-B | Cage 71379 |
5. | 4140-00-15 | Cage 09445 |
6. | 1426033-3 | Cage 71379 |
Nothing similar to this part number was found in our inventory
A completely inclosed machine consisting of two or more positive or nonpositive displacement pumps with a common 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.