Airbus A220-100 vs. Bombardier CRJ1000

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Airbus A220-100 versus Bombardier CRJ1000
35.0 m 114 ft 10 in length 39.1 m 128 ft 5 in
11.5 m 37 ft 9 in height 7.5 m 24 ft 7 in
35.1 m 115 ft 2 in wingspan 26.2 m 86 ft
2 Turbofans (wing mounted) engines 2 GE CF34-8C5A1 turbofans
21,000–23,000 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
42,000–46,000 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
63,100 kg 139,100 lb MTOW 41,640 kg 91,800 lb
6,390 km 3,451 nm range 3,004 km 1,623 nm
871 km/h 541 mph cruise speed 515 mph 829 km/h
Typical seating 2-class 100-120 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.