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

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de Havilland Canada DHC-2 Beaver versus Airbus A300-600F
13.56 m 44 ft 6 in length 54.08 m 177 ft 5 in
5 m 16 ft 5 in height 17.05 m 55 ft 11 in
16.56 m 54 ft 4 in wingspan 44.84 m 147 ft 1 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 2 x General Electric CF6-80C2A5 turbofan engines
Approximately 3,100 hp (2,312 kW) each thrust per engine Approximately 59,000 lbf per engine
Approximately 6,200 hp (4,624 kW) total total thrust Approximately 118,000 lbf total
24,200 lb 10,977 kg MTOW 170,000 kg 374,786 lb
2,535 km 1,369 nm range 4,830 km 2,608 nm
228 mph 367 km/h cruise speed 860 km/h 534 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.