Initial Operational Capability (IOC):
Origin: United States of America
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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-100D engine is a non-afterburning derivative of the F404-GE-400. The -100D engine powers Singapore's A-4S Super Skyhawk providing dramatically improved performance.
Fan Diameter: 890 millimeter (35.0 inch)
Length: 2.26 meter (89 inch)
Dry Weight: 826 kilogram (1,821 pound)
Thrust: 11,000 pound (4.99 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)
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