Wednesday, December 03, 2008

F404

IOC: 1980
Total Production: 3,700

F404-GE-100D

Origin
United States of America

Contractor/s
General Electric

Applications
A-4 Skyhawk

Family Members
F404-GE-102
F404-GE-102D
F404-GE-400
F404-GE-402
F404-GE-F1D2
F404-GE-IN20

Derived from:
F404-GE-400

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.

Specifications
Dimensions: Diameter 890 mm, Length 2.3 m

Weights: Max Weight 826 kg (1,821 lb)

Engine/s Performance: Thrust 11,000 lb (4,990 kg)

Operators

Singapore

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)

Last Updated: Saturday, November 22, 2008

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