Airbus A220-300 vs. Bombardier CRJ1000

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Airbus A220-300 versus Bombardier CRJ1000
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 41,640 kg 91,800 lb
6,297 km 3,402 nm range 3,004 km 1,623 nm
Mach 0.82 101,3 km/h cruise speed 515 mph 829 km/h
Typical seating 2-class 120-150 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.