Initial Operational Capability (IOC): 1993
Total Production: ?
Origin: United Kingdom and United States of America
Corporations: Honeywell and Rolls-Royce
Parent System: T800
Initial Operational Capability (IOC): 1993
Total Production: ?
Family Members: CTS800 and T800-LHT-801
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Description: The T800 is a family of turboshaft engines developed jointly between Honeywell and Rolls Royce under the Light Helicopter Turbine Engine Company (LHTEC). These engines are rated between 1,300 - 1,800-shp featuring modular design and ease of maintenance. The T800 engine was developed to power high performance light/medium helicopters operating in the military range such as the US Army RAH-66 Comanche (now cancelled).

T800-LHT-800 was developed to power the US Army RAH-66 Comanche combat and scout helicopter. This program was cancelled by the Army in 2004. These engines are available for re-engining programs for existing helicopters.

T800-LHT-800 Applications

Combat Aircraft AW129 International Propulsion Systems T800-LHT-801

T800-LHT-800 Specifications

Max Power at TakeOff: 1,300 shp (970 kW)
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)

T800-LHT-800 News

There are 2 news between
31 Mar 2007 and 30 Nov 2018
Friday, November 30, 2018Turkish Searching for Engine Replace to Fit into Pakistani T129 Attack Helicopters
Saturday, March 31, 2007AgustaWestland Enters Negotiations with Turkey for the Supply of A129 as ATAK Helicopter

Operators & Related Equipment


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