Airbus A350-900ULR vs. North American B-25 Mitchell

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Airbus A350-900ULR versus North American B-25 Mitchell
66.80 m 219 ft 2 in length 16.15 m 53 ft 0 in
17.05 m 55 ft 11 in height 5 m 16 ft 4 in
64.75 m 212 ft 5 in wingspan 20.58 m 67 ft 6 in
2 Rolls-Royce Trent XWB engines 2 x Wright R-2600-92 Twin Cyclone
84,000 lbs thrust per engine 1,700 horsepower
168,000 lbs total thrust 3,400 horsepower
280,000 kg 617,300 lb MTOW 7,484 kg 16,500 lb
17,964 km 9,700 nm range 1,350 mi 1,175 nm
552 mph 888 km/h cruise speed 233 MPH 375 km/h
300-350 passengers in three classes 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.