Airbus A330-200 vs. McDonnell-Douglas MD-11

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Airbus A330-200 versus McDonnell-Douglas MD-11
58.82 m 193 ft 0 in length 61.20 m 200 ft 10 in
17.39 m 57 ft 1 in height 17.6 m 57 ft 9 in
64 m 210 ft wingspan 51.6 m 169 ft 4 in
2 Turbofans engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
Depends on the engine variant total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
251,000 kg 553,400 lb MTOW 285,990 kg 630,400 lb
15,094 km 8,150 nm range 13,231 km 7,147 nm
531 mph 855 km/h cruise speed 961 km/h 597 mph
220-260 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.