Airbus A340-500 vs. de Havilland Canada DHC-2 Beaver

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Airbus A340-500 versus de Havilland Canada DHC-2 Beaver
67.93 m 222 ft 10 in length 13.56 m 44 ft 6 in
17.53 m 57 ft 6 in height 5 m 16 ft 5 in
63.45 m 208 ft 2 in wingspan 16.56 m 54 ft 4 in
4 Rolls-Royce Trent 500 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
54,000 lbf (240 kN) thrust per engine Approximately 3,100 hp (2,312 kW) each
216,000 lbf (960 kN) total thrust Approximately 6,200 hp (4,624 kW) total
380,000 kg 837,800 lb MTOW 24,200 lb 10,977 kg
16,670 km 9,000 nm range 2,535 km 1,369 nm
475 knots 880 km/h cruise speed 228 mph 367 km/h
Typical seating 3-class 270-310 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.