Airbus A340-200 vs. North American B-25 Mitchell
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Airbus A340-200 |
versus |
North American B-25 Mitchell |
59.4 m |
194 ft 11 in |
length |
16.15 m |
53 ft 0 in |
16.8 m |
55 ft 1 in |
height |
5 m |
16 ft 4 in |
60.3 m |
197 ft 9 in |
wingspan |
20.58 m |
67 ft 6 in |
4 x CFM International CFM56-5C4 |
engines |
2 x Wright R-2600-92 Twin Cyclone |
34,000 lbf |
thrust per engine |
1,700 horsepower |
136,000 lbf |
total thrust |
3,400 horsepower |
275,000 kg |
606,300 lb |
MTOW |
7,484 kg |
16,500 lb |
12,400 km |
6,699 nm |
range |
1,350 mi |
1,175 nm |
880 km/h |
547 mph |
cruise speed |
233 MPH |
375 km/h |
Typical seating 3-class 210-250 |
capacity |
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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.