Airbus A350-900 vs. McDonnell-Douglas MD-11

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Airbus A350-900 versus McDonnell-Douglas MD-11
66.80 m 219 ft 2 in length 61.20 m 200 ft 10 in
17.05 m 55 ft 11 in height 17.6 m 57 ft 9 in
64.75 m 212 ft 5 in wingspan 51.6 m 169 ft 4 in
2 Rolls-Royce Trent XWB engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
84,000 lbs thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
168,000 lbs total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
283,000 kg 623,900 lb MTOW 285,990 kg 630,400 lb
15,372 km 8,300 nm range 13,231 km 7,147 nm
888 km/h 552 mph cruise speed 961 km/h 597 mph
300-350 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.