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F110-GE-100 aircraft engine
pump, fuel boost
fscap
boost fuel pump
o/a lg drive shaft to inlet side 8.295 in. nom, inlet dia 4.86 - 4.92 in.; mount 6.055 - 6.115 in. dia, 3 holls 0.64 in. thru one end 0.403 - 0.412 in. dia, 2 holes 0.64 in. thru other end 0.403 - 0.412 in. dia; rotation counterclock; main discharge 0.98 in. nom id, seal area 1.839 in. min od; aug discharge 1.78 in. nom id, seal area 2.745 in. min od; spline data: 16 teeth, pressure angle 30 deg, maj dia 0.845 - 0.850 in., minor dia 0.682 - 0.692 in.
source control dwg no. 1296M72
1EA
Schedule B number: 8803300060
nmfc 116480
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 f110-ge-100 aircraft engine. fscap pump, fuel boost
1. | RR54660D | Cage 51663 |
2. | 1296M72 | Cage 07482 |
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.