Airbus A320-200 vs. de Havilland Canada DHC-3 Otter

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Airbus A320-200 versus de Havilland Canada DHC-3 Otter
38.7 m 127 ft 0 in length 10.52 m 34 ft 6 in
17.4 m 57 ft 1 in height 3.84 m 12 ft 7 in
35.8 m 117 ft 5 in wingspan 17.68 m 58 ft
Choice between Pratt & Whitney GTFâ„¢ and the LEAP-1A from CFM International engines 1 x Pratt & Whitney R-1340 radial engine
Between 21,000 - 33,000 lbf thrust per engine 400 to 600 horsepower (298 to 447 kW)
Between 42,000 - 66,000 lbf total thrust 400 to 600 horsepower (298 to 447 kW)
77,000 kg 169,800 lb MTOW 5,670 kg 12,500 lb
5,700 km 3,078 nm range 1,296 km 700 nm
530 mph 853 km/h cruise speed 215 km/h 134 mph
Typically between 140-180 passengers capacity 10-11 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.