Airbus A340-200 vs. de Havilland Canada DHC-2 Beaver
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Airbus A340-200 |
versus |
de Havilland Canada DHC-2 Beaver |
59.4 m |
194 ft 11 in |
length |
13.56 m |
44 ft 6 in |
16.8 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 |
4 x CFM International CFM56-5C4 |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
34,000 lbf |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
136,000 lbf |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
275,000 kg |
606,300 lb |
MTOW |
24,200 lb |
10,977 kg |
12,400 km |
6,699 nm |
range |
2,535 km |
1,369 nm |
880 km/h |
547 mph |
cruise speed |
228 mph |
367 km/h |
Typical seating 3-class 210-250 |
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.