Airbus A330-300 vs. McDonnell-Douglas MD-11
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Airbus A330-300 |
versus |
McDonnell-Douglas MD-11 |
63.66 m |
208 ft 9 in |
length |
61.20 m |
200 ft 10 in |
16.79 m |
55 ft 1 in |
height |
17.6 m |
57 ft 9 in |
60.3 m |
197 ft 9 in |
wingspan |
51.6 m |
169 ft 4 in |
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) |
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
thrust per engine |
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) |
Depends on the engine type |
total thrust |
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) |
242,000 kg |
533,600 lb |
MTOW |
285,990 kg |
630,400 lb |
11,750 km |
6,346 nm |
range |
13,231 km |
7,147 nm |
900 km/h |
559 mph |
cruise speed |
961 km/h |
597 mph |
250-290 |
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.