Airbus A340-300X vs. North American B-25 Mitchell

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Airbus A340-300X versus North American B-25 Mitchell
63.60 m 208 ft 6 in length 16.15 m 53 ft 0 in
16.7 m 54 ft 9 in height 5 m 16 ft 4 in
60.3 m 197 ft 9 in wingspan 20.58 m 67 ft 6 in
4 Turbofan Engines engines 2 x Wright R-2600-92 Twin Cyclone
151.2 kN thrust per engine 1,700 horsepower
604.8 kN total thrust 3,400 horsepower
275,000 kg 606,300 lb MTOW 7,484 kg 16,500 lb
13,699 km 7,403 nm range 1,350 mi 1,175 nm
915 km/h 569 mph cruise speed 233 MPH 375 km/h
295 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.