Airbus A310-300 vs. Airbus A320-200

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Airbus A310-300 versus Airbus A320-200
46.66 m 153 ft 1 in length 38.7 m 127 ft 0 in
15.8 m 51 ft 10 in height 17.4 m 57 ft 1 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 Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International
52,000 lb thrust per engine Between 21,000 - 33,000 lbf
104,000 lb total thrust Between 42,000 - 66,000 lbf
148,768 kg 328,000 lb MTOW 77,000 kg 169,800 lb
8,050 km 4,348 nm range 5,700 km 3,078 nm
482 knots 279 mph cruise speed 530 mph 853 km/h
190-230 passengers capacity Typically between 140-180 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.