Initial Operational Capability (IOC):
Also Known As: TF39-GE-1C
Origin: United States of America
Parent System: TF39
Initial Operational Capability (IOC): 1978
Total Production: 213
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Description: The TF39 engine was introduced in 1965 powering the C-5A Galaxy transport aircraft.
The TF39-1C engine is a derivative of the TF39 incorporating many product improvements. The -1C engine took its improvements in terms of durability from CF6 commercial engine family.
Fan Diameter: 2.37 meter (93 inch)
Length: 4.80 meter (189 inch)
Dry Weight: 3,583 kilogram (7,899 pound)
Thrust: 41,100 pound (18.6 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)
Operators & Related Equipment
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