Airbus A321-200 vs. de Havilland Canada DHC-2 Beaver

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Airbus A321-200 versus de Havilland Canada DHC-2 Beaver
44.51 m 146 ft 0 in length 13.56 m 44 ft 6 in
11.76 m 38 ft 7 in height 5 m 16 ft 5 in
35.8 m 117 ft 5 in wingspan 16.56 m 54 ft 4 in
2 GE CFM56-5B3 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
31,600 lbs thrust per engine Approximately 3,100 hp (2,312 kW) each
63,200 lbs total thrust Approximately 6,200 hp (4,624 kW) total
89,000 kg 196,200 lb MTOW 24,200 lb 10,977 kg
4,000 nmi 7,408 km range 2,535 km 1,369 nm
871 km/h 541 mph cruise speed 228 mph 367 km/h
185 to 220 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.