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

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Airbus A300-600 versus McDonnell-Douglas DC-9-30
54.10 m 177 ft 6 in length 36.36 m 119 ft 3 in
16.5 m 54 ft 2 in height 8.5 m 27 ft 11 in
44.84 m 147 ft 1 in wingspan 28.44 m 93 ft 4 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2x Pratt & Whitney JT8D
56,000lb to 61,500lb thrust per engine 15,000 pound-force
112,000–123,000 lb total thrust 30,000 pound-force (2 engines)
171,700 kg 378,600 lb MTOW 54,885 kg 121,000 lb
7,500 km 4,052 nm range 2,632 km 1,422 nm
897 km/h 557 mph cruise speed 898 km/h 558 mph
210-250 passengers capacity Up to 139 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.