Opr temp fuel: 65.0 to 135.0 degrees f; pressure fuel: 0 to 135 psig operating, 270 psig proof 7500 psig burst; 15.46 max. In. Lg., 7.43 max. In. W.; 23 gpm hydraulic oil supplies at 2700 psid max. To hydraulic motor on fuel pump will deliver 220 gpm of jet
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 5985-01-476-3138
NSN 5996-01-287-7464
NSN 5915-01-367-4614
NSN 5990-01-043-3400
NSN 6110-01-432-0003
NSN 5965-01-613-7134
NSN 6150-01-463-3087
NSN 5910-01-390-0883
NSN 5945-00-081-6453
NSN 5835-01-054-2094
NSN 6110-01-455-4245
NSN 6145-00-629-2801