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The Engine Specifications
The CFE738 was a joint project between General Electric and Garrett (now part of Honeywell).  This turbofan was designed to power long-range business aircraft.  First deliveries began in 1991.
Turbofan (two shaft)
Fan: single-stage
Compressor: 6-stage (5 axial and 1 centrifugal)
Turbine: 3-stage HP, 2-stage LP
Bypass ratio: 5.3
Pressure ratio: 23
Models Used by
CFE738-11B: 5,725 lb (25.6 kN)
Dassault Falcon 2000
Related Pages
more about CFE

page updated 21 April 2003



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Kenneth W Shanaberger 2000 - 2010