Airbus A340-600 vs. North American B-25 Mitchell

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Airbus A340-600 versus North American B-25 Mitchell
75.36 m 247 ft 3 in length 16.15 m 53 ft 0 in
17.93 m 58 ft 10 in height 5 m 16 ft 4 in
63.45 m 208 ft 2 in wingspan 20.58 m 67 ft 6 in
4 x Rolls-Royce Trent 556 engines 2 x Wright R-2600-92 Twin Cyclone
56,000 lbs thrust per engine 1,700 horsepower
224,000 lbs total thrust 3,400 horsepower
380,000 kg 837,800 lb MTOW 7,484 kg 16,500 lb
14,450 km 7,804 nm range 1,350 mi 1,175 nm
890 km/h 553 mph cruise speed 233 MPH 375 km/h
320-370 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.