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Beechcraft T-6 Texan II
Military
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BAE Systems Hawk
Military
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|---|---|---|
| Quick facts | ||
| Manufacturer | Beechcraft | BAE Systems |
| Type | Trainers | Trainers |
| Origin | 🇺🇸 United States | 🇬🇧 United Kingdom |
| First flight | 1998 | 1974 |
| Status | In production | In service |
| Units built | 1,000 | 1,000 |
| Unit cost | — | — |
| Dimensions | ||
| Length | 10.16 m | 12.43 m |
| Wingspan | 10.19 m | 9.39 m |
| Height | 3.25 m | 3.98 m |
| Wing area | 16.5 m² | 16.7 m² |
| Weights & fuel | ||
| Empty weight | 2,087 kg | 4,480 kg |
| Max. take-off weight | 2,948 kg | 9,100 kg |
| Performance | ||
| Max. speed | 585 km/h | 1,028 km/h |
| Range | 1,667 km | 2,520 km |
| Service ceiling | 9,450 m | 13,565 m |
| Rate of climb | 16.6 m/s | — |
| Crew & capacity | ||
| Crew | 2 | 2 |
| Hardpoints | — | 5 |
| Powerplant | ||
| Engines | 1 | 1 |
| Engine type | — | — |
| Engine model | Pratt & Whitney Canada PT6A-68 | Rolls-Royce Turbomeca Adour Mk 951 |
| Thrust (each) | — | 29.0 kN |
| Power (each) | 820 kW | — |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.