Airbus A321LR vs. McDonnell-Douglas MD-11

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Airbus A321LR 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 International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
Over 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)
97,000 kg 213,800 lb MTOW 285,990 kg 630,400 lb
7,400 km 4,000 nm range 13,231 km 7,147 nm
832 km/h 517 mph cruise speed 961 km/h 597 mph
180-220 passengers 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.