Airbus A310-300 vs. McDonnell-Douglas MD-11

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Airbus A310-300 versus McDonnell-Douglas MD-11
46.66 m 153 ft 1 in length 61.20 m 200 ft 10 in
15.8 m 51 ft 10 in height 17.6 m 57 ft 9 in
43.9 m 144 ft wingspan 51.6 m 169 ft 4 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
52,000 lb thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
104,000 lb total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
148,768 kg 328,000 lb MTOW 285,990 kg 630,400 lb
8,050 km 4,348 nm range 13,231 km 7,147 nm
482 knots 279 mph cruise speed 961 km/h 597 mph
190-230 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.