Airbus A220-100 vs. Nanchang CJ-6

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Airbus A220-100 versus Nanchang CJ-6
35.0 m 114 ft 10 in length 8.48 m 27 ft 10 in
11.5 m 37 ft 9 in height 2.67 m 8 ft 9 in
35.1 m 115 ft 2 in wingspan 10.49 m 34 ft 5 in
2 Turbofans (wing mounted) engines 1 x Ivchenko AI-14RA radial engine
21,000–23,000 lb thrust per engine Approximately 260 hp
42,000–46,000 lb total thrust Approximately 260 hp
63,100 kg 139,100 lb MTOW 3,858 lb 1,751 kg
6,390 km 3,451 nm range 800 km 432 nm
871 km/h 541 mph cruise speed 155 mph 249 km/h
Typical seating 2-class 100-120 capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.