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BAE Hawk Specifications
BAE Hawk
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| Data for Aircraft | BAE Hawk |
| Year Introduced | 1976 |
| Number Built | 900 |
| Rotor Diameter | |
| Wingspan | 32 ft 7 in (9.94 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 900+ |
| Wing Area | 179.64 ft² (16.70 m²) |
| Wing Loading | |
| Length | 40 ft 9 in (12.43 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Rolls-Royce Adour Mk. 951, 6,500 lbf (29 kN) |
| Country of Origin | Britain |
| Empty Weight | 9,880 lb (4,480 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 20,000 lb (9,100 kg) |
| Useful Load | 6,600 lb (3,000 kg) |
| Seats | 2 |
| Crew | 2: student, instructor |
| 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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