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

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Airbus A350-900ULR 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)
280,000 kg 617,300 lb MTOW 285,990 kg 630,400 lb
17,964 km 9,700 nm range 13,231 km 7,147 nm
552 mph 888 km/h cruise speed 961 km/h 597 mph
300-350 passengers in three classes 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.