Airbus A320-200 vs. Bombardier CRJ1000

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Airbus A320-200 versus Bombardier CRJ1000
38.7 m 127 ft 0 in length 39.1 m 128 ft 5 in
17.4 m 57 ft 1 in height 7.5 m 24 ft 7 in
35.8 m 117 ft 5 in wingspan 26.2 m 86 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 GE CF34-8C5A1 turbofans
Between 21,000 - 33,000 lbf 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
Between 42,000 - 66,000 lbf 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
77,000 kg 169,800 lb MTOW 41,640 kg 91,800 lb
5,700 km 3,078 nm range 3,004 km 1,623 nm
530 mph 853 km/h cruise speed 515 mph 829 km/h
Typically between 140-180 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.