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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.