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Bell Textron 212 Twin Huey
Military
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Bell Textron UH-1 Iroquois "Huey"
Military
|
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|---|---|---|
| Quick facts | ||
| Manufacturer | Bell Textron | Bell Textron |
| Type | Military helicopters | Military helicopters |
| Origin | 🇺🇸 United States | 🇺🇸 United States |
| First flight | 1968 | 1956 |
| Status | In service | In service |
| Units built | — | 16,000 |
| Unit cost | — | — |
| Dimensions | ||
| Length | 17.40 m | 17.40 m |
| Wingspan | 14.69 m | 14.63 m |
| Height | 4.53 m | 4.39 m |
| Weights & fuel | ||
| Empty weight | 2,787 kg | 2,365 kg |
| Max. take-off weight | 5,080 kg | 4,309 kg |
| Performance | ||
| Max. speed | 259 km/h | 220 km/h |
| Cruise speed | 230 km/h | 205 km/h |
| Range | 439 km | 510 km |
| Service ceiling | 5,300 m | 5,910 m |
| Crew & capacity | ||
| Crew | 1–2 | 1–4 |
| Seats (typical) | 14 | 11 |
| Seats (max.) | 14 | 14 |
| Powerplant | ||
| Engines | 1 | 1 |
| Engine type | — | — |
| Engine model | Pratt & Whitney Canada PT6T-3 Twin-Pac (two coupled power sections) | Lycoming T53-L-13 |
| Power (each) | 1,342 kW | 1,044 kW |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.