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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
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 fuel at 135.5 psig pressure min.
as differentiated by source control no.
Schedule B number: 8803300060
nmfc 128020
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.
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
1. | 29340 | Cage 56231 |
2. | 29340 | Cage 72429 |
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.