Airbus A300-600 vs. McDonnell-Douglas MD-11

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Airbus A300-600 versus McDonnell-Douglas MD-11
54.10 m 177 ft 6 in length 61.20 m 200 ft 10 in
16.5 m 54 ft 2 in height 17.6 m 57 ft 9 in
44.84 m 147 ft 1 in wingspan 51.6 m 169 ft 4 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
56,000lb to 61,500lb thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
112,000–123,000 lb total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
171,700 kg 378,600 lb MTOW 285,990 kg 630,400 lb
7,500 km 4,052 nm range 13,231 km 7,147 nm
897 km/h 557 mph cruise speed 961 km/h 597 mph
210-250 passengers capacity Max 410 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.