Initial Operational Capability (IOC): 1998
Total Production: 40
Also Known As: T6A1
Origin: United States of America
Corporations: General Electric
Parent System: T700
Initial Operational Capability (IOC): 1978
Total Production: 20,100
Family Members: CT7, CT7-2, CT7-8, CT7-8C, CT7-8E, T700-GE-401, T700-GE-401C, T700-GE-700, T700-GE-701, T700-GE-701C, T700-GE-701D, T700-GE-701E, T700-T6A, T700-T6E, T700-T6E1 and T706-GE-700
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Description: The T700 engine was designed for the US Army's UH-60A Black Hawk helicopter as a result of lessons learned in Vietnam. The key requirements of this engine were reliability, operation under adverse environmental conditions and low maintainability.

The T6A1 engine is a derivative of T700 engine. In 1998 T6A1 was selected to power Canadian EH101 helicopters with up to 40 engines to be produced. T6A1 is the military designation/version of CT7-6 civil engine.

T700-T6A1 Applications

Private Aircraft EH101 Cormorant

T700-T6A1 Specifications

Diameter: 400 millimeter (15.7 inch)
Length: 1,190 millimeter (47 inch)
Max Continuous Power: 2,145 shp (1,600 kW)
Max Power at TakeOff: 2,180 shp (1,626 kW)
Dry Weight: 224 kilogram (494 pound)
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)

T700-T6A1 News

There is 1 news
on 3 Mar 2017
Friday, March 3, 2017First Canadian Air Force Cormorant Helicopter Powered by T700-T6A1 Engines Takes to the Air

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