Airbus A300-600 vs. McDonnell-Douglas DC-10-30

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Airbus A300-600 versus McDonnell-Douglas DC-10-30
54.10 m 177 ft 6 in length 55.35 m 181 ft 8 in
16.5 m 54 ft 2 in height 17.8 m 58 ft 5 in
44.84 m 147 ft 1 in wingspan 50.39 m 165 ft 4 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 3x GE CF6-50C Turbofan
56,000lb to 61,500lb thrust per engine 54,000 lbf
112,000–123,000 lb total thrust 162,000 lbf
171,700 kg 378,600 lb MTOW 251,744 kg 555,000 lb
7,500 km 4,052 nm range 9,630 km 5,200 nm
897 km/h 557 mph cruise speed 507 knots 939 km/h
210-250 passengers capacity Up to 380 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.