Airbus A300-600 vs. de Havilland Canada DHC-2 Beaver

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Airbus A300-600 versus de Havilland Canada DHC-2 Beaver
54.10 m 177 ft 6 in length 13.56 m 44 ft 6 in
16.5 m 54 ft 2 in height 5 m 16 ft 5 in
44.84 m 147 ft 1 in wingspan 16.56 m 54 ft 4 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
56,000lb to 61,500lb thrust per engine Approximately 3,100 hp (2,312 kW) each
112,000–123,000 lb total thrust Approximately 6,200 hp (4,624 kW) total
171,700 kg 378,600 lb MTOW 24,200 lb 10,977 kg
7,500 km 4,052 nm range 2,535 km 1,369 nm
897 km/h 557 mph cruise speed 228 mph 367 km/h
210-250 passengers capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.