Airbus A310-300 vs. PZL TS-11 Iskra

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Airbus A310-300 versus PZL TS-11 Iskra
46.66 m 153 ft 1 in length 11.15 m 36 ft 7 in
15.8 m 51 ft 10 in height 3.5 m 11 ft 6 in
43.9 m 144 ft wingspan 10.06 m 33 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 (WSK PZL Rzeszow SO-3W)
52,000 lb thrust per engine 10.8 kN
104,000 lb total thrust 10.8 kN
148,768 kg 328,000 lb MTOW 3,840 kg 8,466 lb
8,050 km 4,348 nm range 1,250 km 675 nm
482 knots 279 mph cruise speed 770 km/h 478 mph
190-230 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.