McDonnell-Douglas DC-9-30 vs. Airbus A300-600F

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McDonnell-Douglas DC-9-30 versus Airbus A300-600F
36.36 m 119 ft 3 in length 54.08 m 177 ft 5 in
8.5 m 27 ft 11 in height 17.05 m 55 ft 11 in
28.44 m 93 ft 4 in wingspan 44.84 m 147 ft 1 in
2x Pratt & Whitney JT8D engines 2 x General Electric CF6-80C2A5 turbofan engines
15,000 pound-force thrust per engine Approximately 59,000 lbf per engine
30,000 pound-force (2 engines) total thrust Approximately 118,000 lbf total
54,885 kg 121,000 lb MTOW 170,000 kg 374,786 lb
2,632 km 1,422 nm range 4,830 km 2,608 nm
898 km/h 558 mph cruise speed 860 km/h 534 mph
Up to 139 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.