Airbus A340-500 vs. North American B-25 Mitchell

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Airbus A340-500 versus North American B-25 Mitchell
67.93 m 222 ft 10 in length 16.15 m 53 ft 0 in
17.53 m 57 ft 6 in height 5 m 16 ft 4 in
63.45 m 208 ft 2 in wingspan 20.58 m 67 ft 6 in
4 Rolls-Royce Trent 500 engines 2 x Wright R-2600-92 Twin Cyclone
54,000 lbf (240 kN) thrust per engine 1,700 horsepower
216,000 lbf (960 kN) total thrust 3,400 horsepower
380,000 kg 837,800 lb MTOW 7,484 kg 16,500 lb
16,670 km 9,000 nm range 1,350 mi 1,175 nm
475 knots 880 km/h cruise speed 233 MPH 375 km/h
Typical seating 3-class 270-310 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.