Airbus A340-600 vs. de Havilland Canada DHC-2 Beaver
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Airbus A340-600 |
versus |
de Havilland Canada DHC-2 Beaver |
75.36 m |
247 ft 3 in |
length |
13.56 m |
44 ft 6 in |
17.93 m |
58 ft 10 in |
height |
5 m |
16 ft 5 in |
63.45 m |
208 ft 2 in |
wingspan |
16.56 m |
54 ft 4 in |
4 x Rolls-Royce Trent 556 |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
56,000 lbs |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
224,000 lbs |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
380,000 kg |
837,800 lb |
MTOW |
24,200 lb |
10,977 kg |
14,450 km |
7,804 nm |
range |
2,535 km |
1,369 nm |
890 km/h |
553 mph |
cruise speed |
228 mph |
367 km/h |
320-370 |
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.