Airbus A321LR vs. Boeing 747-8I

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Airbus A321LR versus Boeing 747-8I
44.51 m 146 ft 0 in length 76.25 m 250 ft 2 in
11.76 m 38 ft 7 in height 19.35 m 63 ft 6 in
35.8 m 117 ft 5 in wingspan 68.45 m 224 ft 7 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 4x General Electric GEnx 2B67 Turbofan
Over 33,000 lbs (147 kN) thrust per engine 66,500 pounds
66,000 lbs (294 kN) total thrust 266,000 pounds
97,000 kg 213,800 lb MTOW 443,613 kg 977,500 lb
7,400 km 4,000 nm range 8,000 nm 14,816 km
832 km/h 517 mph cruise speed Mach 0.86 1,062 km/h
180-220 passengers capacity 467 passengers (three-class configuration)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.