Initial Operational Capability (IOC):
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-400, F404-GE-402 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.

The F404-GE-F1D2 was designed to power the USAF's F-117A stealth fighter. The main feature of -F1D2 by comparison with baseline F404 is the lack of afterburner to reduce aircraft's IR signature. The -F1D2 engine also has lower thrust due to the non-afterburning feature.

F404-GE-F1D2 Applications

Combat Aircraft F-117A Nighthawk

F404-GE-F1D2 Specifications

Fan Diameter: 890 millimeter (35.0 inch)
Length: 2.10 meter (83 inch)
Dry Weight: 785 kilogram (1,731 pound)
Thrust: 10,500 pound (4.76 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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