Airbus A310-300 vs. Airbus A318

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Airbus A310-300 versus Airbus A318
46.66 m 153 ft 1 in length 31.44 m 103 ft 2 in
15.8 m 51 ft 10 in height 12.56 m 41 ft 3 in
43.9 m 144 ft wingspan 34.1 m 111 ft 11 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2x CFM56-5B or 2x PW6000
52,000 lb thrust per engine 23,300 lb
104,000 lb total thrust 46,600 lb
148,768 kg 328,000 lb MTOW 59,000 kg 130,000 lb
8,050 km 4,348 nm range 5,750 km 3,106 nm
482 knots 279 mph cruise speed 963km/h 598mph
190-230 passengers capacity 107 to 132 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.