Airbus A321LR vs. Bombardier CRJ1000

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Airbus A321LR versus Bombardier CRJ1000
44.51 m 146 ft 0 in length 39.1 m 128 ft 5 in
11.76 m 38 ft 7 in height 7.5 m 24 ft 7 in
35.8 m 117 ft 5 in wingspan 26.2 m 86 ft
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 GE CF34-8C5A1 turbofans
Over 33,000 lbs (147 kN) 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
66,000 lbs (294 kN) 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
97,000 kg 213,800 lb MTOW 41,640 kg 91,800 lb
7,400 km 4,000 nm range 3,004 km 1,623 nm
832 km/h 517 mph cruise speed 515 mph 829 km/h
180-220 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.