Airbus A310-300 vs. Boeing 717-200HGW

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Airbus A310-300 versus Boeing 717-200HGW
46.66 m 153 ft 1 in length 37.80 m 123 ft 11 in
15.8 m 51 ft 10 in height 8.87 m 29 ft 1 in
43.9 m 144 ft wingspan 28.44 m 93 ft 4 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 Rolls-Royce BR715
52,000 lb thrust per engine 82.3kN (18,500lb) to 93.4kN (21,000lb)
104,000 lb total thrust 164.6kN (37,000lb) to 186.8kN (42,000lb)
148,768 kg 328,000 lb MTOW 54,885 kg 121,000 lb
8,050 km 4,348 nm range 2,060 nm 3,814 km
482 knots 279 mph cruise speed 811 km/h 504 mph
190-230 passengers capacity 106 passengers in a 2 class configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.