Airbus A300-600 vs. PZL TS-11 Iskra

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Airbus A300-600 versus PZL TS-11 Iskra
54.10 m 177 ft 6 in length 11.15 m 36 ft 7 in
16.5 m 54 ft 2 in height 3.5 m 11 ft 6 in
44.84 m 147 ft 1 in wingspan 10.06 m 33 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 (WSK PZL Rzeszow SO-3W)
56,000lb to 61,500lb thrust per engine 10.8 kN
112,000–123,000 lb total thrust 10.8 kN
171,700 kg 378,600 lb MTOW 3,840 kg 8,466 lb
7,500 km 4,052 nm range 1,250 km 675 nm
897 km/h 557 mph cruise speed 770 km/h 478 mph
210-250 passengers 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.