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McDonnell Douglas A-4 Skyhawk
 More pics at: zap16.com
| Developing Nation: | United States of America |
| Task: | Light Attack / multi-role |
| First Flight: | August 14th 1954 |
| First Delivery: | September 1956 |
| Crew: | 1 or 2 in tandem |
| Wing Span: | 8.38 m |
| Wing Area: | 24.2 m² |
| Length: | 12.27 m |
| Height: | 4.57 m |
| Engine (s): | (A-4M) non afterburning Pratt & Whitney J52-P-408 turbojet 1x |
| Weight: | 4747 kg |
| Max.Take off weight: | 11115 kg |
| Max. Speed: |
- 1100 km/h (sea-level) - 1038 km/h with a 1815 kg bomb load |
| Max. Range: |
- 3305 km (ferry range) - 545 km Combat-range with 1815 kg bomb load |
| Weapons: |
- Two 20 mm Colt Mk 12 cannons in wing roots. - A-4M max. ordnance of 4155 kg on one centerline and four underwing hardpoints including bombs, AIM-9′s, Bullpup and Maverick ASM’s |
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Countries that use(d) the A-4 Skyhawk |
|
Argentina |
| Brazil |
| Indonesia |
| Israel |
| Malaysia |
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Research M. van Leeuwen