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: 5,935
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, F103 military designation, has been provided to power large military aircraft like KC-10, B-767 AWACS, Air Force One, E-4B and the YAL-1A aircraft. In the early 2000s CF6 family engines have been selected to power KC-767 and A330 tanker/transport 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

Length: 4.39 meter (173 inch)
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


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