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gfe
opr temp fuel: M65.0 to 135.0 degrees f; pressure fuel: 0 to 150 psig operating, 225 psig proof, 300 psig burst; 15.46 max. in. lg; 7.43 in. w
opr temp fuel: M65.0 to 135.0 degrees f; pressure fuel: 0 to 150 psig operating, 225 psig proof, 300 psig burst; 15.46 max. in. lg; 7.43 in. w
as differentiated by source control drawing no
Schedule B number: 8803300060
nmfc 127600
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 GFE. opr temp fuel: M65.0 to 135.0 degrees f; pressure fuel: 0 to 150 psig operating, 225 psig proof, 300 psig burst; 15.46 max. in. lg; 7.43 in. w
1. | 6179-1 | Cage 86090 |
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.