Airbus A321-200 vs. McDonnell-Douglas MD-11

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Airbus A321-200 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
2 GE CFM56-5B3 engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
31,600 lbs thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
63,200 lbs total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
89,000 kg 196,200 lb MTOW 285,990 kg 630,400 lb
4,000 nmi 7,408 km range 13,231 km 7,147 nm
871 km/h 541 mph cruise speed 961 km/h 597 mph
185 to 220 capacity Max 410 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.