Airbus A300-600 vs. Airbus A321LR

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Airbus A300-600 versus Airbus A321LR
54.10 m 177 ft 6 in length 44.51 m 146 ft 0 in
16.5 m 54 ft 2 in height 11.76 m 38 ft 7 in
44.84 m 147 ft 1 in wingspan 35.8 m 117 ft 5 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM
56,000lb to 61,500lb thrust per engine Over 33,000 lbs (147 kN)
112,000–123,000 lb total thrust 66,000 lbs (294 kN)
171,700 kg 378,600 lb MTOW 97,000 kg 213,800 lb
7,500 km 4,052 nm range 7,400 km 4,000 nm
897 km/h 557 mph cruise speed 832 km/h 517 mph
210-250 passengers capacity 180-220 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.