Airbus A318 vs. de Havilland Canada DHC-2 Beaver

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Airbus A318 versus de Havilland Canada DHC-2 Beaver
31.44 m 103 ft 2 in length 13.56 m 44 ft 6 in
12.56 m 41 ft 3 in height 5 m 16 ft 5 in
34.1 m 111 ft 11 in wingspan 16.56 m 54 ft 4 in
2x CFM56-5B or 2x PW6000 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
23,300 lb thrust per engine Approximately 3,100 hp (2,312 kW) each
46,600 lb total thrust Approximately 6,200 hp (4,624 kW) total
59,000 kg 130,000 lb MTOW 24,200 lb 10,977 kg
5,750 km 3,106 nm range 2,535 km 1,369 nm
963km/h 598mph cruise speed 228 mph 367 km/h
107 to 132 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.