Airbus A310-300 vs. Bombardier CS100

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Airbus A310-300 versus Bombardier CS100
46.66 m 153 ft 1 in length 35.00 m 114 ft 10 in
15.8 m 51 ft 10 in height 11.5 m 37 ft 9 in
43.9 m 144 ft wingspan 35.1 m 115 ft 2 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Pratt & Whitney PurePower PW1500G
52,000 lb thrust per engine 84.1 kN
104,000 lb total thrust 168.2 kN
148,768 kg 328,000 lb MTOW 54,931 kg 121,100 lb
8,050 km 4,348 nm range 4,074 km 2,200 nm
482 knots 279 mph cruise speed 871 km/h 541 mph
190-230 passengers capacity 110 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.