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AE 2100
IOC: 1990
Total Production: 1,078
AE 2100D3
Unitary Cost: USD$1.9 million
Origin United Kingdom
Contractor/s
Rolls-Royce
Applications
C-130J Super Hercules CC-130J Super Hercules EC-130J Commando Solo KC-130J Super Hercules WC-130J
Family Members
AE 2100D2
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Description:
The AE2100 engine is a derivative of the T406 turboshaft. It has been designed to power high-speed regional aircraft.
The AE2100D3 engine variant was selected to power the latest C-130 military transport aircraft model, known as the C-130J.
Specifications
Power: Power 4,590 shp
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)
Last Updated: Saturday, October 25, 2008
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