You are hereBoeing F/A-18E/F Super Hornet Specifications
Boeing F/A-18E/F Super Hornet Specifications
Boeing F/A-18E/F Super Hornet
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| Data for Aircraft | Boeing F/A-18E/F Super Hornet |
| Year Introduced | 1999 |
| Number Built | 400+ |
| Rotor Diameter | |
| Wingspan | 44 ft 8½ in (13.62 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 16 ft (4.88 m) |
| Wing Area | 500 ft² (46.45 m²) |
| Wing Loading | 94.0 lb/ft² (459 kg/m²) |
| Length | 60 ft 1¼ in (18.31 m) |
| Lift-to-Drag Ratio | |
| Engine Type | General Electric F414-GE-400, 14,000 lbf (62.3 kN) |
| Country of Origin | USA |
| Empty Weight | 30,600 lb (13,900 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 66,000 lb (29,900 kg) |
| Useful Load | 35,400 lb |
| Seats | 2 |
| Crew | F/A-18E: 1, F/A-18F: 2 |
| 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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