Airbus A320-200 vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A320-200 versus de Havilland Canada DHC-6 Twin Otter
38.7 m 127 ft 0 in length 15.32 m 50 ft 3 in
17.4 m 57 ft 1 in height 5.94 m 19 ft 6 in
35.8 m 117 ft 5 in wingspan 19.81 m 65 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
Between 21,000 - 33,000 lbf thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
Between 42,000 - 66,000 lbf total thrust 1100 to 1500 shaft horsepower
77,000 kg 169,800 lb MTOW 5,670 kg 12,500 lb
5,700 km 3,078 nm range 1,389 km 750 nm
530 mph 853 km/h cruise speed 280 km/h 174 mph
Typically between 140-180 passengers 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.