Airbus A330-200 vs. North American B-25 Mitchell

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Airbus A330-200 versus North American B-25 Mitchell
58.82 m 193 ft 0 in length 16.15 m 53 ft 0 in
17.39 m 57 ft 1 in height 5 m 16 ft 4 in
64 m 210 ft wingspan 20.58 m 67 ft 6 in
2 Turbofans engines 2 x Wright R-2600-92 Twin Cyclone
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 1,700 horsepower
Depends on the engine variant total thrust 3,400 horsepower
251,000 kg 553,400 lb MTOW 7,484 kg 16,500 lb
15,094 km 8,150 nm range 1,350 mi 1,175 nm
531 mph 855 km/h cruise speed 233 MPH 375 km/h
220-260 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.