Airbus A310-300 vs. Bombardier CRJ900

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Airbus A310-300 versus Bombardier CRJ900
46.66 m 153 ft 1 in length 36.2 m 118 ft 11 in
15.8 m 51 ft 10 in height 7.5 m 24 ft 7 in
43.9 m 144 ft wingspan 24.9 m 81 ft 8 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 Turbofans (fuselage mounted)
52,000 lb thrust per engine 13,360 pounds force
104,000 lb total thrust 26,720 pounds force
148,768 kg 328,000 lb MTOW 38,330 kg 84,500 lb
8,050 km 4,348 nm range 2,871 km 1,550 nm
482 knots 279 mph cruise speed 515 mph 829 km/h
190-230 passengers capacity Up to 90 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.