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 6650-00-146-6485
NSN 5855-01-602-3270
NSN 5965-01-473-0825
NSN 5996-00-086-4774
NSN 6220-00-421-3508
NSN 5945-01-448-1691
NSN 2925-01-157-9204
NSN 5975-01-044-5419
NSN 5920-01-179-9739
NSN 6610-00-997-3436
NSN 7035-00-803-3056
NSN 4140-01-042-3494