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,
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.
Classification: Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts thereof)
NSN 5935-00-920-7981
NSN 6105-01-221-7685
NSN 5975-01-227-8968
NSN 5895-01-024-9573
NSN 5915-01-064-4220
NSN 6105-01-388-1926
NSN 5950-01-191-3313
NSN 5835-01-284-5689
NSN 6110-00-763-7152
NSN 6620-01-449-8743
NSN 5998-01-283-1153
NSN 5945-01-424-3298