Airbus A340-200 vs. de Havilland Canada DHC-6 Twin Otter
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Airbus A340-200 |
versus |
de Havilland Canada DHC-6 Twin Otter |
59.4 m |
194 ft 11 in |
length |
15.32 m |
50 ft 3 in |
16.8 m |
55 ft 1 in |
height |
5.94 m |
19 ft 6 in |
60.3 m |
197 ft 9 in |
wingspan |
19.81 m |
65 ft |
4 x CFM International CFM56-5C4 |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
34,000 lbf |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
136,000 lbf |
total thrust |
1100 to 1500 shaft horsepower |
275,000 kg |
606,300 lb |
MTOW |
5,670 kg |
12,500 lb |
12,400 km |
6,699 nm |
range |
1,389 km |
750 nm |
880 km/h |
547 mph |
cruise speed |
280 km/h |
174 mph |
Typical seating 3-class 210-250 |
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.