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C-17A
115.0 ac
pump rating based on JP4 fuel, atmospheric pressure from sea level to 1 000 ft above sea level and at 110 degf fuel temp; materials compatible withfuel types, JP-4, JP-5, JP-8, jet a, jet A-1, or jet b, and comparable with nato fuels; nte 2.5 lbs in weight; environmental temp, -80 deg f to +240 degf; fuel temp range to operate, -65 degf to +135 deg f; subject to pressures equivalent to altitudes of -1800 ft to 50000 ft
1C-17A-4-28
pump rating based on JP4 fuel, atmospheric pressure from sea level to 1 000 ft above sea level and at 110 degf fuel temp; materials compatible withfuel types, JP-4, JP-5, JP-8, jet a, jet A-1, or jet b, and comparable with nato fuels; nte 2.5 lbs in weight; environmental temp, -80 deg f to +240 degf; fuel temp range to operate, -65 degf to +135 deg f; subject to pressures equivalent to altitudes of -1800 ft to 50000 ft
1EA
Schedule B number: 8803300060
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.
Used on C-17A. pump rating based on JP4 fuel, atmospheric pressure from sea level to 1 000 ft above sea level 115.0 ac voltage in volts and current type
1. | 17B2D1049-501 | Cage 88277 |
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.