Airbus A350-900ULR vs. de Havilland Canada DHC-2 Beaver
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Airbus A350-900ULR |
versus |
de Havilland Canada DHC-2 Beaver |
66.80 m |
219 ft 2 in |
length |
13.56 m |
44 ft 6 in |
17.05 m |
55 ft 11 in |
height |
5 m |
16 ft 5 in |
64.75 m |
212 ft 5 in |
wingspan |
16.56 m |
54 ft 4 in |
2 Rolls-Royce Trent XWB |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
84,000 lbs |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
168,000 lbs |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
280,000 kg |
617,300 lb |
MTOW |
24,200 lb |
10,977 kg |
17,964 km |
9,700 nm |
range |
2,535 km |
1,369 nm |
552 mph |
888 km/h |
cruise speed |
228 mph |
367 km/h |
300-350 passengers in three classes |
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.