Airbus A330-300 vs. North American B-25 Mitchell

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Airbus A330-300 versus North American B-25 Mitchell
63.66 m 208 ft 9 in length 16.15 m 53 ft 0 in
16.79 m 55 ft 1 in height 5 m 16 ft 4 in
60.3 m 197 ft 9 in wingspan 20.58 m 67 ft 6 in
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 2 x Wright R-2600-92 Twin Cyclone
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 1,700 horsepower
Depends on the engine type total thrust 3,400 horsepower
242,000 kg 533,600 lb MTOW 7,484 kg 16,500 lb
11,750 km 6,346 nm range 1,350 mi 1,175 nm
900 km/h 559 mph cruise speed 233 MPH 375 km/h
250-290 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.