Airbus A320neo vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A320neo versus de Havilland Canada DHC-6 Twin Otter
37.57 m 123 ft 3 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 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 1100 to 1500 shaft horsepower
79,000 kg 174,200 lb MTOW 5,670 kg 12,500 lb
6,300 km 3,403 nm range 1,389 km 750 nm
M0.82 101,3 km/h cruise speed 280 km/h 174 mph
150-180 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.