Airbus A321neo vs. de Havilland Canada DHC-2 Beaver

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Airbus A321neo 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 x Armstrong Siddeley Double Mamba turboprop engines
35,000 lb thrust per engine Approximately 3,100 hp (2,312 kW) each
70,000 lb total thrust Approximately 6,200 hp (4,624 kW) total
97,000 kg 213,800 lb MTOW 24,200 lb 10,977 kg
7,400 km 4,000 nm range 2,535 km 1,369 nm
828 km/h 514 mph cruise speed 228 mph 367 km/h
180 to 220 passengers 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.