North American B-25 Mitchell vs. Airbus A300-600F

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North American B-25 Mitchell versus Airbus A300-600F
16.15 m 53 ft 0 in length 54.08 m 177 ft 5 in
5 m 16 ft 4 in height 17.05 m 55 ft 11 in
20.58 m 67 ft 6 in wingspan 44.84 m 147 ft 1 in
2 x Wright R-2600-92 Twin Cyclone engines 2 x General Electric CF6-80C2A5 turbofan engines
1,700 horsepower thrust per engine Approximately 59,000 lbf per engine
3,400 horsepower total thrust Approximately 118,000 lbf total
7,484 kg 16,500 lb MTOW 170,000 kg 374,786 lb
1,350 mi 1,175 nm range 4,830 km 2,608 nm
233 MPH 375 km/h cruise speed 860 km/h 534 mph
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.