Airbus A320neo vs. de Havilland Canada DHC-2 Beaver

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Airbus A320neo versus de Havilland Canada DHC-2 Beaver
37.57 m 123 ft 3 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 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Armstrong Siddeley Double Mamba turboprop engines
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine Approximately 3,100 hp (2,312 kW) each
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust Approximately 6,200 hp (4,624 kW) total
79,000 kg 174,200 lb MTOW 24,200 lb 10,977 kg
6,300 km 3,403 nm range 2,535 km 1,369 nm
M0.82 101,3 km/h cruise speed 228 mph 367 km/h
150-180 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.