Airbus A330-200 vs. de Havilland Canada DHC-2 Beaver

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Airbus A330-200 versus de Havilland Canada DHC-2 Beaver
58.82 m 193 ft 0 in length 13.56 m 44 ft 6 in
17.39 m 57 ft 1 in height 5 m 16 ft 5 in
64 m 210 ft wingspan 16.56 m 54 ft 4 in
2 Turbofans engines 2 x Armstrong Siddeley Double Mamba turboprop engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine Approximately 3,100 hp (2,312 kW) each
Depends on the engine variant total thrust Approximately 6,200 hp (4,624 kW) total
251,000 kg 553,400 lb MTOW 24,200 lb 10,977 kg
15,094 km 8,150 nm range 2,535 km 1,369 nm
531 mph 855 km/h cruise speed 228 mph 367 km/h
220-260 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.