Airbus A220-100 vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A220-100 versus de Havilland Canada DHC-6 Twin Otter
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 5,670 kg 12,500 lb
6,390 km 3,451 nm range 1,389 km 750 nm
871 km/h 541 mph cruise speed 280 km/h 174 mph
Typical seating 2-class 100-120 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.