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Boeing CH-47 Chinook
Military
|
Bell Textron 212 Twin Huey
Military
|
|
|---|---|---|
| Quick facts | ||
| Manufacturer | Boeing | Bell Textron |
| Type | Military helicopters | Military helicopters |
| Origin | 🇺🇸 United States | 🇺🇸 United States |
| First flight | 1961 | 1968 |
| Status | In production | In service |
| Units built | 1,200 | — |
| Unit cost | — | — |
| Dimensions | ||
| Length | 30.10 m | 17.40 m |
| Wingspan | 18.29 m | 14.69 m |
| Height | 5.70 m | 4.53 m |
| Weights & fuel | ||
| Empty weight | 11,148 kg | 2,787 kg |
| Max. take-off weight | 22,680 kg | 5,080 kg |
| Max. payload | 10,886 kg | — |
| Performance | ||
| Max. speed | 315 km/h | 259 km/h |
| Cruise speed | 291 km/h | 230 km/h |
| Range | 370 km | 439 km |
| Ferry range | 2,252 km | — |
| Service ceiling | 6,100 m | 5,300 m |
| Crew & capacity | ||
| Crew | 3 | 1–2 |
| Seats (typical) | 33 | 14 |
| Seats (max.) | 55 | 14 |
| Cargo capacity | 12,700 kg | — |
| Powerplant | ||
| Engines | 2 | 1 |
| Engine type | — | — |
| Engine model | Honeywell T55-GA-714A | Pratt & Whitney Canada PT6T-3 Twin-Pac (two coupled power sections) |
| Power (each) | 3,529 kW | 1,342 kW |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.