Airbus A300-600F vs. de Havilland Canada DHC-3 Otter

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Airbus A300-600F versus de Havilland Canada DHC-3 Otter
54.08 m 177 ft 5 in length 10.52 m 34 ft 6 in
17.05 m 55 ft 11 in height 3.84 m 12 ft 7 in
44.84 m 147 ft 1 in wingspan 17.68 m 58 ft
2 x General Electric CF6-80C2A5 turbofan engines engines 1 x Pratt & Whitney R-1340 radial engine
Approximately 59,000 lbf per engine thrust per engine 400 to 600 horsepower (298 to 447 kW)
Approximately 118,000 lbf total total thrust 400 to 600 horsepower (298 to 447 kW)
170,000 kg 374,786 lb MTOW 5,670 kg 12,500 lb
4,830 km 2,608 nm range 1,296 km 700 nm
860 km/h 534 mph cruise speed 215 km/h 134 mph
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.