Airbus A310-300 vs. North American B-25 Mitchell

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Airbus A310-300 versus North American B-25 Mitchell
46.66 m 153 ft 1 in length 16.15 m 53 ft 0 in
15.8 m 51 ft 10 in height 5 m 16 ft 4 in
43.9 m 144 ft wingspan 20.58 m 67 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Wright R-2600-92 Twin Cyclone
52,000 lb thrust per engine 1,700 horsepower
104,000 lb total thrust 3,400 horsepower
148,768 kg 328,000 lb MTOW 7,484 kg 16,500 lb
8,050 km 4,348 nm range 1,350 mi 1,175 nm
482 knots 279 mph cruise speed 233 MPH 375 km/h
190-230 passengers 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.