Airbus A220-100 vs. PZL TS-11 Iskra

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Airbus A220-100 versus PZL TS-11 Iskra
35.0 m 114 ft 10 in length 11.15 m 36 ft 7 in
11.5 m 37 ft 9 in height 3.5 m 11 ft 6 in
35.1 m 115 ft 2 in wingspan 10.06 m 33 ft
2 Turbofans (wing mounted) engines 1 (WSK PZL Rzeszow SO-3W)
21,000–23,000 lb thrust per engine 10.8 kN
42,000–46,000 lb total thrust 10.8 kN
63,100 kg 139,100 lb MTOW 3,840 kg 8,466 lb
6,390 km 3,451 nm range 1,250 km 675 nm
871 km/h 541 mph cruise speed 770 km/h 478 mph
Typical seating 2-class 100-120 capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.