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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.