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

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McDonnell-Douglas MD-11 versus Airbus A300-600F
61.20 m 200 ft 10 in length 54.08 m 177 ft 5 in
17.6 m 57 ft 9 in height 17.05 m 55 ft 11 in
51.6 m 169 ft 4 in wingspan 44.84 m 147 ft 1 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 x General Electric CF6-80C2A5 turbofan engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Approximately 59,000 lbf per engine
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Approximately 118,000 lbf total
285,990 kg 630,400 lb MTOW 170,000 kg 374,786 lb
13,231 km 7,147 nm range 4,830 km 2,608 nm
961 km/h 597 mph cruise speed 860 km/h 534 mph
Max 410 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.