Thursday, August 28, 2008

T700

IOC: 1978
Total Production: 13,212

T700-T6A1

IOC: 1998

Also Known As: T6A1

Origin:United States of America

Contractor/s: General Electric

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. T6A1 is the military designation/version of CT7-6 civil engine.

Specifications
Dimensions: Diameter 400 mm, Length 1,190 mm

Weights: Max Weight 224 kg (494 lb)

Power: Power 2,180 shp

Family Members:
CT7, 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-T6A, T700-T6E, T700-T6E1, T706-GE-700 Related Equipment
Derived from: T700-GE-700

Operators

Canada

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: Sunday, August 24, 2008

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