Thursday, November 20, 2008

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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

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

AE 2100D3 - Contracts, Orders & Sales

 



News

 

Operators

see operators map | see family operators map

Australia
Canada / 68
Denmark
Greece

Italy
Japan
Norway / 16

Engines powering four C-130Js

United Kingdom
United States of America



Image Gallery


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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