Airbus A300-600 vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A300-600 versus de Havilland Canada DHC-6 Twin Otter
54.10 m 177 ft 6 in length 15.32 m 50 ft 3 in
16.5 m 54 ft 2 in height 5.94 m 19 ft 6 in
44.84 m 147 ft 1 in wingspan 19.81 m 65 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
56,000lb to 61,500lb thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
112,000–123,000 lb total thrust 1100 to 1500 shaft horsepower
171,700 kg 378,600 lb MTOW 5,670 kg 12,500 lb
7,500 km 4,052 nm range 1,389 km 750 nm
897 km/h 557 mph cruise speed 280 km/h 174 mph
210-250 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.