Airbus A330-300 vs. de Havilland Canada DHC-2 Beaver

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Airbus A330-300 versus de Havilland Canada DHC-2 Beaver
63.66 m 208 ft 9 in length 13.56 m 44 ft 6 in
16.79 m 55 ft 1 in height 5 m 16 ft 5 in
60.3 m 197 ft 9 in wingspan 16.56 m 54 ft 4 in
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine Approximately 3,100 hp (2,312 kW) each
Depends on the engine type total thrust Approximately 6,200 hp (4,624 kW) total
242,000 kg 533,600 lb MTOW 24,200 lb 10,977 kg
11,750 km 6,346 nm range 2,535 km 1,369 nm
900 km/h 559 mph cruise speed 228 mph 367 km/h
250-290 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.