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Four-seat carrierborne Command and Control Warfare aircraft development of A-6 Intruder.
Development contract issued autumn 1966; externally similar to basic A-6 except longer nose enclosing
four-seat cockpit and large pod on fin; first flight 25 May 1968; delivery of first 12 production aircraft started
January 1971; last of 170 delivered 29 July 1991.
| CREW | 4 |
| ENGINE | 2 x P+W J-52-P-8, 41.4kN |
| WEIGHTS |
| Take-off weight | 26535-28655 kg | 58500 - 63174 lb |
| Empty weight | 15686 kg | 34582 lb |
| DIMENSIONS |
| Wingspan | 16.2 m | 53 ft 2 in |
| Length | 16.3 m | 53 ft 6 in |
| Height | 5.0 m | 16 ft 5 in |
| Wing area | 49.1 m2 | 528.51 sq ft |
| PERFORMANCE |
| Max. speed | 965 km/h | 600 mph |
| Cruise speed | 850 km/h | 528 mph |
| Ceiling | 11600 m | 38050 ft |
| Range w/max.fuel | 4000 km | 2486 miles |
| W. Lehmann, lehmannw(@)optonline.net, 26.07.2008 What about the EA6A ?? I believe 12 were built for the Marines. | | fred creekmore, froggi(@)svs.net, 02.04.2008 Where is the EA6A? I was an avionics tech on this aircraft while in the Marines VMCJ-2 at Cherry Point NC, and VMCJ-1 in Iwakuni Japan. Lets not foreget this aircraft!! |
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