Airbus A220-300 vs. PZL TS-11 Iskra

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Airbus A220-300 versus PZL TS-11 Iskra
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 3,840 kg 8,466 lb
6,297 km 3,402 nm range 1,250 km 675 nm
Mach 0.82 101,3 km/h cruise speed 770 km/h 478 mph
Typical seating 2-class 120-150 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.