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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.