Airbus A340-200 vs. de Havilland Canada DHC-2 Beaver

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Airbus A340-200 versus de Havilland Canada DHC-2 Beaver
59.4 m 194 ft 11 in length 13.56 m 44 ft 6 in
16.8 m 55 ft 1 in height 5 m 16 ft 5 in
60.3 m 197 ft 9 in wingspan 16.56 m 54 ft 4 in
4 x CFM International CFM56-5C4 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
34,000 lbf thrust per engine Approximately 3,100 hp (2,312 kW) each
136,000 lbf total thrust Approximately 6,200 hp (4,624 kW) total
275,000 kg 606,300 lb MTOW 24,200 lb 10,977 kg
12,400 km 6,699 nm range 2,535 km 1,369 nm
880 km/h 547 mph cruise speed 228 mph 367 km/h
Typical seating 3-class 210-250 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.