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 |
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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.