Airbus A220-300 vs. de Havilland Canada DHC-6 Twin Otter
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Airbus A220-300 |
versus |
de Havilland Canada DHC-6 Twin Otter |
38.7 m |
127 ft 0 in |
length |
15.32 m |
50 ft 3 in |
11.5 m |
37 ft 9 in |
height |
5.94 m |
19 ft 6 in |
35.1 m |
115 ft 2 in |
wingspan |
19.81 m |
65 ft |
2 x Pratt & Whitney PurePower PW1500G |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
21,000–23,000 lb |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
42,000–46,000 lb |
total thrust |
1100 to 1500 shaft horsepower |
70,900 kg |
156,300 lb |
MTOW |
5,670 kg |
12,500 lb |
6,297 km |
3,402 nm |
range |
1,389 km |
750 nm |
Mach 0.82 |
101,3 km/h |
cruise speed |
280 km/h |
174 mph |
Typical seating 2-class 120-150 |
capacity |
19 passengers |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.