F103  
Initial Operational Capability (IOC): 1972
Total Production: ?
Also Known As: CF6-50
Origin: United States of America
Corporations: General Electric
Parent System: CF6
Initial Operational Capability (IOC): 1971
Total Production: 5,931
Family Members: CF6-80C2, CF6-80E1 and F138-GE-100
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Description: The CF6 engine was designed to power commercial airplanes. Its military version, called F103, has been provided to power large military aircraft like KC-10, B-767 AWACS, Air Force One, E-4B and the YAL-1A aircraft.

The F-103 engine has been selected to power the upgraded C-5 Galaxy under RER program, if finally this program is carried out. F-103s are also the engine-of-choice for current and future air refueling aircraft programs.

F103 Applications


Support Aircraft E-4B KC-10A Extender

F103 Specifications

Dimensions
Length: 4.39 meter (173 inch)
Weight
Dry Weight: 5,063 kilogram (11,162 pound)
Thrust: 40,000 pound (18.1 ton)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
 
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