Airbus A310-300 vs. Bombardier CRJ1000

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Airbus A310-300 versus Bombardier CRJ1000
46.66 m 153 ft 1 in length 39.1 m 128 ft 5 in
15.8 m 51 ft 10 in height 7.5 m 24 ft 7 in
43.9 m 144 ft wingspan 26.2 m 86 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 GE CF34-8C5A1 turbofans
52,000 lb thrust per engine 13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve
104,000 lb total thrust 27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve
148,768 kg 328,000 lb MTOW 41,640 kg 91,800 lb
8,050 km 4,348 nm range 3,004 km 1,623 nm
482 knots 279 mph cruise speed 515 mph 829 km/h
190-230 passengers capacity 100 (common)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.