Airbus A310-300 vs. de Havilland Canada DHC-2 Beaver

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Airbus A310-300 versus de Havilland Canada DHC-2 Beaver
46.66 m 153 ft 1 in length 13.56 m 44 ft 6 in
15.8 m 51 ft 10 in height 5 m 16 ft 5 in
43.9 m 144 ft wingspan 16.56 m 54 ft 4 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Armstrong Siddeley Double Mamba turboprop engines
52,000 lb thrust per engine Approximately 3,100 hp (2,312 kW) each
104,000 lb total thrust Approximately 6,200 hp (4,624 kW) total
148,768 kg 328,000 lb MTOW 24,200 lb 10,977 kg
8,050 km 4,348 nm range 2,535 km 1,369 nm
482 knots 279 mph cruise speed 228 mph 367 km/h
190-230 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.