CFE738

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© Kenneth W Shanaberger 2000 - 2010

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