Airbus A220-300 vs. Airbus A310-300

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Airbus A220-300 versus Airbus A310-300
38.7 m 127 ft 0 in length 46.66 m 153 ft 1 in
11.5 m 37 ft 9 in height 15.8 m 51 ft 10 in
35.1 m 115 ft 2 in wingspan 43.9 m 144 ft
2 x Pratt & Whitney PurePower PW1500G engines 2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan
21,000–23,000 lb thrust per engine 52,000 lb
42,000–46,000 lb total thrust 104,000 lb
70,900 kg 156,300 lb MTOW 148,768 kg 328,000 lb
6,297 km 3,402 nm range 8,050 km 4,348 nm
Mach 0.82 101,3 km/h cruise speed 482 knots 279 mph
Typical seating 2-class 120-150 capacity 190-230 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.