Airbus A340-500 vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A340-500 versus de Havilland Canada DHC-6 Twin Otter
67.93 m 222 ft 10 in length 15.32 m 50 ft 3 in
17.53 m 57 ft 6 in height 5.94 m 19 ft 6 in
63.45 m 208 ft 2 in wingspan 19.81 m 65 ft
4 Rolls-Royce Trent 500 engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
54,000 lbf (240 kN) thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
216,000 lbf (960 kN) total thrust 1100 to 1500 shaft horsepower
380,000 kg 837,800 lb MTOW 5,670 kg 12,500 lb
16,670 km 9,000 nm range 1,389 km 750 nm
475 knots 880 km/h cruise speed 280 km/h 174 mph
Typical seating 3-class 270-310 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.