Airbus A220-100 vs. Cessna Citation Mustang

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Airbus A220-100 versus Cessna Citation Mustang
35.0 m 114 ft 10 in length 12.37 m 40 ft 7 in
11.5 m 37 ft 9 in height 4.11 m 13 ft 6 in
35.1 m 115 ft 2 in wingspan 13.17 m 43 ft 2 in
2 Turbofans (wing mounted) engines 2 x Pratt & Whitney Canada PW615F
21,000–23,000 lb thrust per engine 1460 lbs
42,000–46,000 lb total thrust 2920 lbs
63,100 kg 139,100 lb MTOW 8,625 lb 3,912 kg
6,390 km 3,451 nm range 1167 nm 2,161 km
871 km/h 541 mph cruise speed 340 kts 211 mph
Typical seating 2-class 100-120 capacity 4
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.