Airbus A321-200 vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A321-200 versus de Havilland Canada DHC-6 Twin Otter
44.51 m 146 ft 0 in length 15.32 m 50 ft 3 in
11.76 m 38 ft 7 in height 5.94 m 19 ft 6 in
35.8 m 117 ft 5 in wingspan 19.81 m 65 ft
2 GE CFM56-5B3 engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
31,600 lbs thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
63,200 lbs total thrust 1100 to 1500 shaft horsepower
89,000 kg 196,200 lb MTOW 5,670 kg 12,500 lb
4,000 nmi 7,408 km range 1,389 km 750 nm
871 km/h 541 mph cruise speed 280 km/h 174 mph
185 to 220 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.