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Aérospatiale / BAC SA 321 Super Frelon
Military
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Boeing CH-47 Chinook
Military
|
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|---|---|---|
| Quick facts | ||
| Manufacturer | Aérospatiale / BAC | Boeing |
| Type | Military helicopters | Military helicopters |
| Origin | — | 🇺🇸 United States |
| First flight | 1962 | 1961 |
| Status | In service | In production |
| Units built | 110 | 1,200 |
| Unit cost | — | — |
| Dimensions | ||
| Length | 23.00 m | 30.10 m |
| Wingspan | — | 18.29 m |
| Height | 4.93 m | 5.70 m |
| Weights & fuel | ||
| Empty weight | — | 11,148 kg |
| Max. take-off weight | — | 22,680 kg |
| Max. payload | — | 10,886 kg |
| Performance | ||
| Max. speed | — | 315 km/h |
| Cruise speed | — | 291 km/h |
| Range | 650 km | 370 km |
| Ferry range | — | 2,252 km |
| Service ceiling | — | 6,100 m |
| Crew & capacity | ||
| Crew | — | 3 |
| Seats (typical) | — | 33 |
| Seats (max.) | — | 55 |
| Cargo capacity | — | 12,700 kg |
| Powerplant | ||
| Engines | — | 2 |
| Engine type | — | — |
| Engine model | Turbomeca Turmo | Honeywell T55-GA-714A |
| Power (each) | — | 3,529 kW |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.