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this pump is to be stainless steel with a mechanical shaft seal of polytetrafluoroethylene. pump is to operate up to 100 psi, a motor speed to 1725 rpm, and a temperature to 450 degrees f. at 40 psi discharge, this pump is to be capable of .4 gpm at 400 rpm,
this pump is to be stainless steel with a mechanical shaft seal of polytetrafluoroethylene. pump is to operate up to 100 psi, a motor speed to 1725 rpm, and a temperature to 450 degrees f. at 40 psi discharge, this pump is to be capable of .4 gpm at 400 rpm, 1.62 gpm at 800 rpm, and 3.65 gpm at 1725 rpm. pump bushings are carbon.
1EA
Schedule B number: 8803300060
nmfc 127630
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.
this pump is to be stainless steel with a mechanical shaft seal of polytetrafluoroethylene. pump is to operate up to 100 psi, a motor speed to 1725 rpm, and a temperature to 450 degrees f. at 40 psi discharge, this pump is to be capable of .4 gpm at 400 rpm,
1. | 207146C | Cage 4K628 |
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3. | 2146 | Cage 4K628 |
4. | 2146C | Cage 4K628 |
Nothing similar to this part number was found in our inventory
A device specifically designed to (1) increase the pressure of, (2) meter the amount of, (3) control the distribution of liquid fuel received directly or indirectly from the tank, fuel, engine to the individual air inlet tubes or combustion chambers of gasoline or diesel engines.