Airbus A220-100 vs. Polikarpov I-16

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Airbus A220-100 versus Polikarpov I-16
35.0 m 114 ft 10 in length 6.13 m 20 ft 1 in
11.5 m 37 ft 9 in height 3.25 m 10 ft 8 in
35.1 m 115 ft 2 in wingspan 9 m 29 ft 6 in
2 Turbofans (wing mounted) engines 1x Shvetsov M-25 radial engine
21,000–23,000 lb thrust per engine 1000 hp
42,000–46,000 lb total thrust 1000 hp
63,100 kg 139,100 lb MTOW 2,060 kg 4,540 lb
6,390 km 3,451 nm range 248 mi 216 nm
871 km/h 541 mph cruise speed 180 mph 290 km/h
Typical seating 2-class 100-120 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.