Airbus A340-600 vs. de Havilland Canada DHC-2 Beaver

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Airbus A340-600 versus de Havilland Canada DHC-2 Beaver
75.36 m 247 ft 3 in length 13.56 m 44 ft 6 in
17.93 m 58 ft 10 in height 5 m 16 ft 5 in
63.45 m 208 ft 2 in wingspan 16.56 m 54 ft 4 in
4 x Rolls-Royce Trent 556 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
56,000 lbs thrust per engine Approximately 3,100 hp (2,312 kW) each
224,000 lbs total thrust Approximately 6,200 hp (4,624 kW) total
380,000 kg 837,800 lb MTOW 24,200 lb 10,977 kg
14,450 km 7,804 nm range 2,535 km 1,369 nm
890 km/h 553 mph cruise speed 228 mph 367 km/h
320-370 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.