T700-T6A  
Initial Operational Capability (IOC):
Total Production: ?
Also Known As: T6A
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-T6A1, 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 T6A engine is a derivative of T700 engine. T6A was selected to power Italian EH101 helicopters. T6A is a military variant of CT7-6 civil engine.

T700-T6A Specifications

Dimensions
Diameter: 400 millimeter (15.7 inch)
Length: 1,190 millimeter (47 inch)
Power
Max Power at TakeOff: 2,000 shp (1,492 kW)
Weight
Dry Weight: 220 kilogram (485 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-T6A News

There is 1 news
on 5 Nov 2015
Thursday, November 5, 2015GE Aviation Delivers 20,000th T700/CT7 Turboshaft Engine

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