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Mil Mi-14
Military
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Bell Textron 212 Twin Huey
Military
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|---|---|---|
| Quick facts | ||
| Manufacturer | Mil Helicopters | Bell Textron |
| Type | Military helicopters | Military helicopters |
| Origin | 🇸🇺 Soviet Union | 🇺🇸 United States |
| First flight | 1969 | 1968 |
| Status | Retired | In service |
| Units built | 230 | — |
| Unit cost | — | — |
| Dimensions | ||
| Length | 18.15 m | 17.40 m |
| Wingspan | — | 14.69 m |
| Height | — | 4.53 m |
| Weights & fuel | ||
| Empty weight | — | 2,787 kg |
| Max. take-off weight | — | 5,080 kg |
| Performance | ||
| Max. speed | — | 259 km/h |
| Cruise speed | — | 230 km/h |
| Range | — | 439 km |
| Service ceiling | — | 5,300 m |
| Crew & capacity | ||
| Crew | — | 1–2 |
| Seats (typical) | — | 14 |
| Seats (max.) | — | 14 |
| Powerplant | ||
| Engines | — | 1 |
| Engine type | — | — |
| Engine model | Klimov TV3-117 | Pratt & Whitney Canada PT6T-3 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.