Airbus A340-500 vs. McDonnell-Douglas MD-11
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Airbus A340-500 |
versus |
McDonnell-Douglas MD-11 |
67.93 m |
222 ft 10 in |
length |
61.20 m |
200 ft 10 in |
17.53 m |
57 ft 6 in |
height |
17.6 m |
57 ft 9 in |
63.45 m |
208 ft 2 in |
wingspan |
51.6 m |
169 ft 4 in |
4 Rolls-Royce Trent 500 |
engines |
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) |
54,000 lbf (240 kN) |
thrust per engine |
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) |
216,000 lbf (960 kN) |
total thrust |
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) |
380,000 kg |
837,800 lb |
MTOW |
285,990 kg |
630,400 lb |
16,670 km |
9,000 nm |
range |
13,231 km |
7,147 nm |
475 knots |
880 km/h |
cruise speed |
961 km/h |
597 mph |
Typical seating 3-class 270-310 |
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.