A-4 Skyhawk

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A-4 Skyhawk

Initial Operational Capability (IOC): 1962
Total Production: 3,000
Also Known As: A-4A, A-4AR, A-4B, A-4C, A-4D, A-4E, A-4F, A-4H, A-4K Kahu, A-4M Skyhawk II, A-4N, A-4P, A-4Q, A-4S Super Skyhawk, A-4SU Skyhawk, AF-1, AF-1A and TA-4
Origin: United States of America
Corporations: Boeing

Parent System: A-4 Skyhawk
Initial Operational Capability (IOC): 1962
Total Production: 3,000

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Description: A-4 Skyhawk is a light, single-engine, single-seater attack aircraft developed by McDonnell Douglas, now Boeing, to meet the requirements of the US Marine Corps. It is suitable for operation on aircraft carriers. With near 3,000 aircraft produced from the early 1960s through the 1980s, there are many variants of A-4 aircraft which may differ on equipment such as engine (J52/J65/F404-GE-100D) or radar system (APG-53/APG-66). TA-4 is a two-seat trainer based on A-4 aircraft. A-4M was an outstanding improved model introduced in the 1970s and the A-4AR is an improved variant of A-4M sold to Argentina.

A-4 Skyhawk Applications

Fighting Ships Sao Paulo

A-4 Skyhawk Specifications

Crew: 1
Number of Engines: 1
Dimensions
Height: 4.60 meter (15.1 foot)
Length: 12.3 meter (40 foot)
Main Gun Caliber: 20 millimeter
Wingspan: 8.40 meter (27.6 foot)
Performance
Max Range: 3,200 kilometer (1,728 nautical mile)
Speed
Top Speed at High Altitude: 302 mps (1,088 kph)
Weight
Max Takeoff Thrust: 11,220 pound (5,089 kilogram)
Max Takeoff Weight: 12,500 kilogram (27,557 pound)

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)