Airbus A310-300 vs. de Havilland Canada DHC-3 Otter

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Airbus A310-300 versus de Havilland Canada DHC-3 Otter
46.66 m 153 ft 1 in length 10.52 m 34 ft 6 in
15.8 m 51 ft 10 in height 3.84 m 12 ft 7 in
43.9 m 144 ft wingspan 17.68 m 58 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Pratt & Whitney R-1340 radial engine
52,000 lb thrust per engine 400 to 600 horsepower (298 to 447 kW)
104,000 lb total thrust 400 to 600 horsepower (298 to 447 kW)
148,768 kg 328,000 lb MTOW 5,670 kg 12,500 lb
8,050 km 4,348 nm range 1,296 km 700 nm
482 knots 279 mph cruise speed 215 km/h 134 mph
190-230 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.