Airbus A310-300 vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A310-300 versus de Havilland Canada DHC-6 Twin Otter
46.66 m 153 ft 1 in length 15.32 m 50 ft 3 in
15.8 m 51 ft 10 in height 5.94 m 19 ft 6 in
43.9 m 144 ft wingspan 19.81 m 65 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
52,000 lb thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
104,000 lb total thrust 1100 to 1500 shaft horsepower
148,768 kg 328,000 lb MTOW 5,670 kg 12,500 lb
8,050 km 4,348 nm range 1,389 km 750 nm
482 knots 279 mph cruise speed 280 km/h 174 mph
190-230 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.