Airbus A321XLR vs. McDonnell-Douglas MD-11
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Airbus A321XLR |
versus |
McDonnell-Douglas MD-11 |
44.51 m |
146 ft 0 in |
length |
61.20 m |
200 ft 10 in |
11.76 m |
38 ft 7 in |
height |
17.6 m |
57 ft 9 in |
35.8 m |
117 ft 5 in |
wingspan |
51.6 m |
169 ft 4 in |
CFM LEAP-1A and P&W PW1100G |
engines |
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) |
33,000 lbs (147 kN) |
thrust per engine |
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) |
66,000 lbs (294 kN) |
total thrust |
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) |
101,000 kg |
222,700 lb |
MTOW |
285,990 kg |
630,400 lb |
4,700 nmi |
8,704 km |
range |
13,231 km |
7,147 nm |
963km/h |
598mph |
cruise speed |
961 km/h |
597 mph |
180-220 seats (typical 2-class seating) |
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.