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Boeing Chinook (UK variants)
Military
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Bell Textron 412
Military
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|---|---|---|
| Quick facts | ||
| Manufacturer | — | Bell Textron |
| Type | Military helicopters | Military helicopters |
| Origin | — | 🇺🇸 United States |
| First flight | 1980 | 1979 |
| Status | — | In production |
| Units built | — | — |
| Unit cost | — | — |
| Dimensions | ||
| Length | — | 17.10 m |
| Wingspan | — | 14.02 m |
| Height | — | 4.60 m |
| Weights & fuel | ||
| Empty weight | — | 3,079 kg |
| Max. take-off weight | — | 5,397 kg |
| Performance | ||
| Max. speed | — | 259 km/h |
| Cruise speed | — | 226 km/h |
| Range | — | 745 km |
| Service ceiling | — | 6,096 m |
| Crew & capacity | ||
| Crew | — | 1–2 |
| Seats (typical) | — | 13 |
| Seats (max.) | — | 15 |
| Powerplant | ||
| Engines | — | 1 |
| Engine type | — | — |
| Engine model | — | Pratt & Whitney Canada PT6T-3BE Twin-Pac (two coupled power sections) |
| Power (each) | — | 1,342 kW |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.