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DHC-2 Beaver
Aircraft type: Commuter aircraft
Manufacturer: DHC-2
Maiden flight year: 1947
Copyright John Olafson
DHC-2 Beaver Specifications
| Beaver I | Turbo Beaver | |
Dimensions | ||
|---|---|---|
| Length (m) | 9.2 | 10.7 |
| Wingspan (m) | 14.6 | 14.6 |
| Height (m) | 2.7 | 3.3 |
| Wing area (m2) | 23.2 | 23.2 |
Weight | ||
| Maximum take-off weight (kg) | 2 300 | 2 720 |
| Maximum zero fuel weight (kg) | 1 360 | |
| Maximum payload (kg) | 950 | 1100 |
Performance | ||
| Range with max payload (km) | 730 | 960 |
| Cruise speed (km/h) | 230 | 250 |
| Maximum speed (km/h) | 255 | 280 |
| Maximum operating altitude (m) | 4 580 | |
| Engines | Pratt&Whitney R-985, 1 x 450 x 600 hp | Pratt & Whitney PT6A-27, 1 x 680 hp |
Cabin Data | ||
| Passengers (1-class) | 6 | 8-10 |
DHC-2 Beaver Airplane
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