Airbus A310-300 vs. Airbus A321XLR

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Airbus A310-300 versus Airbus A321XLR
46.66 m 153 ft 1 in length 44.51 m 146 ft 0 in
15.8 m 51 ft 10 in height 11.76 m 38 ft 7 in
43.9 m 144 ft wingspan 35.8 m 117 ft 5 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines CFM LEAP-1A and P&W PW1100G
52,000 lb thrust per engine 33,000 lbs (147 kN)
104,000 lb total thrust 66,000 lbs (294 kN)
148,768 kg 328,000 lb MTOW 101,000 kg 222,700 lb
8,050 km 4,348 nm range 4,700 nmi 8,704 km
482 knots 279 mph cruise speed 963km/h 598mph
190-230 passengers capacity 180-220 seats (typical 2-class seating)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.