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Initial Operational Capability (IOC): 1980
Total Production: ?
Origin: United States of America
Corporations: General Electric
Parent System: F404
Initial Operational Capability (IOC): 1980
Total Production: 3,700
Family Members: F404-GE-100D, F404-GE-102, F404-GE-102D, F404-GE-402, F404-GE-F1D2 and F404-GE-IN20
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Description: The F404 engine was developed to power the US Navy's F/A-18 Hornet. It has been proved as a reliable high performance engine. The F404 incorporates an array of new technologies, modular design and advanced materials.

This engine allows to carry out a wide spectrum of missions from low level attack to high altitude interceptors. The F404-GE-400 engine can be assembled/disassembled in short time, making it an easy to maintain engine.

F404-GE-400 Applications

Combat Aircraft F/A-18A Hornet F/A-18B Hornet T-7A Red Hawk Propulsion Systems F404-GE-100D F404-GE-402 F404-GE-F1D2 F414-GE-400 LM1600 RM12

F404-GE-400 Specifications

Fan Diameter: 890 millimeter (35.0 inch)
Length: 3.91 meter (154 inch)
Dry Weight: 991 kilogram (2,185 pound)
Thrust: 16,000 pound (7.26 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)

F404-GE-400 News

There are 2 news between
12 Jan 2009 and 27 Feb 2020
Thursday, February 27, 2020T-7A Training Jet Crew Shuts Off, Restarts Engine in Flight to Demonstrate Reliability
Monday, January 12, 2009GE Awarded Australian F404/F414 Engine Contract

Operators & Related Equipment


Grand Total ?4
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