Airbus A340-300X vs. de Havilland Canada DHC-2 Beaver

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Airbus A340-300X versus de Havilland Canada DHC-2 Beaver
63.60 m 208 ft 6 in length 13.56 m 44 ft 6 in
16.7 m 54 ft 9 in height 5 m 16 ft 5 in
60.3 m 197 ft 9 in wingspan 16.56 m 54 ft 4 in
4 Turbofan Engines engines 2 x Armstrong Siddeley Double Mamba turboprop engines
151.2 kN thrust per engine Approximately 3,100 hp (2,312 kW) each
604.8 kN total thrust Approximately 6,200 hp (4,624 kW) total
275,000 kg 606,300 lb MTOW 24,200 lb 10,977 kg
13,699 km 7,403 nm range 2,535 km 1,369 nm
915 km/h 569 mph cruise speed 228 mph 367 km/h
295 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.