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Grumman A-6 Intruder Specifications
Grumman A-6 Intruder
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| Data for Aircraft | Grumman A-6 Intruder |
| Year Introduced | 1963 |
| Number Built | 693 |
| Rotor Diameter | |
| Wingspan | 53 ft (16.2 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 15 ft 7 in (4.75 m) |
| Wing Area | 529 ft² (49.1 m²) |
| Wing Loading | |
| Length | 54 ft 7 in (16.6 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Pratt & Whitney J52-P8B, 9,300 lbf (41.4 kN) |
| Country of Origin | USA |
| Empty Weight | 25,630 lb (11,630 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 60,626 lb (27,500 kg) |
| Useful Load | 34,996 lb (15,870 kg) |
| Seats | 2 |
| Crew | 2 (pilot, bombardier/navigator) |
| Power Loading | |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | 3 |
| Load Limit Positive | 6 |
| Fuel Capacity | |
| Oil Capacity |
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