T700
IOC: 1978
Total Production: 13,212
T700-GE-701E
Roll-Out: Thursday, August 28, 2008
IOC: 2009
Origin
United States of America
Contractor/s
General Electric Aviation
Applications
UH-60M BlackHawk
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-T6A1
T700-T6E
T700-T6E1
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 T700-GE-701E is a derivative of the proven T700-GE-701D engine. The -701E model was selected to power the US Army's UH-60M helicopter in 2005 replacing the -701D as standard equipment. The first UH-60M helicopter took to the skies powered by -701E engines on August 28, 2008. Approximately 900 such helicopters will be produced for the US Army beginning in 2009.
The -701E engine incorporates an on-engine-mounted full authority digital engine control (FADEC), and includes fail-fixed control design that retains fixed engine power in the event both channels of the control should fail. The new engine has been designed to flawlessly integrate with the UH-60M's fly-by-wire flight control system to provide more precise handling as well as reduced maintenance requirements.
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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, March 07, 2010
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