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McDonnell Douglas F/A-18 Hornet Specifications
McDonnell Douglas F/A-18 Hornet
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| Data for Aircraft | McDonnell Douglas F/A-18 Hornet |
| Year Introduced | 1983 |
| Number Built | 1480 |
| Rotor Diameter | |
| Wingspan | 40 ft (12.3 m) -- with AIM-9 Sidewinders |
| Aspect Ratio | |
| Disc Loading | |
| Height | 15 ft 4 in (4.7 m) |
| Wing Area | 400 ft² (38 m²) |
| Wing Loading | 93 lb/ft² (454 kg/m²) |
| Length | 56 ft (17.1 m) |
| Lift-to-Drag Ratio | |
| Engine Type | General Electric F404-GE-402, 11,000 lbf (48.9 kN) |
| Country of Origin | USA |
| Empty Weight | 23,000 lb (10,400 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 51,900 lb (23,500 kg) |
| Useful Load | 28,900 lb |
| Seats | 1 |
| Crew | F/A-18C: 1, F/A-18D: 2 (pilot and weapons system officer) |
| Power Loading | |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | |
| Load Limit Positive | |
| Fuel Capacity | |
| Oil Capacity |
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