Initial Operational Capability (IOC): 1995
Total Production: 400
Origin: United States of America
Corporations: General Electric Aviation and Honeywell
Parent System: CFE738
Initial Operational Capability (IOC): 1995
Total Production: 400
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Description: The CFE738 is the result of General Electric (GE) and Honeywell, originally Garrett Engine Division of Allied Signal, partnership on commercial aviation engines development. This advanced efficient high-bypass turbofan engine builds upon GE27/GE38 gas generator developed in the 1980s. GE is responsible for the core of the engine and control system while Honeywell manages the front fan, low-pressure turbine and accessory gearbox. Each engine develops near 6,000-lb of thrust at sea level and is controlled by two Full Authority Digital Engine Controls (FADEC).

To date, CFE Company, a Honeywell and General Electric joint venture, has delivered approximately 400 CFE738 engines for the Dassault Falcon 2000 business jet program.

CFE738 Applications

Private Aircraft Falcon 2000

CFE738 Specifications

Bypass Ratio: 5.30
Fan Pressure Ratio: 23
Fan Diameter: 48 inch (1,219 millimeter)
Length: 99 inch (2,515 millimeter)
Dry Weight: 1,325 pound (601 kilogram)
Thrust: 5,918 pound (2.68 ton)
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)

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