Airbus A220-100 vs. Airbus A321neo

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Airbus A220-100 versus Airbus A321neo
35.0 m 114 ft 10 in length 44.51 m 146 ft 0 in
11.5 m 37 ft 9 in height 11.76 m 38 ft 7 in
35.1 m 115 ft 2 in wingspan 35.8 m 117 ft 5 in
2 Turbofans (wing mounted) engines CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM
21,000–23,000 lb thrust per engine 35,000 lb
42,000–46,000 lb total thrust 70,000 lb
63,100 kg 139,100 lb MTOW 97,000 kg 213,800 lb
6,390 km 3,451 nm range 7,400 km 4,000 nm
871 km/h 541 mph cruise speed 828 km/h 514 mph
Typical seating 2-class 100-120 capacity 180 to 220 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.