de Havilland Canada DHC-2 Beaver vs. Airbus A380-800F

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de Havilland Canada DHC-2 Beaver versus Airbus A380-800F
13.56 m 44 ft 6 in length 72.73 m 238 ft 7 in
5 m 16 ft 5 in height 24.09 m 79 ft
16.56 m 54 ft 4 in wingspan 79.75 m 261 ft 8 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 4 x Engine Alliance GP7200 turbofan engines
Approximately 3,100 hp (2,312 kW) each thrust per engine 70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons)
Approximately 6,200 hp (4,624 kW) total total thrust 280,000 to 320,000 pounds
24,200 lb 10,977 kg MTOW 590,000 kg 1,300,733 lb
2,535 km 1,369 nm range 14,800 km 7,992 nm
228 mph 367 km/h cruise speed 903 km/h 561 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.