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