PZL TS-11 Iskra vs. Airbus H225 Super Puma

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PZL TS-11 Iskra versus Airbus H225 Super Puma
11.15 m 36 ft 7 in length 14.06 m 46 ft 2 in
3.5 m 11 ft 6 in height 4.38 m 14 ft 4 in
10.06 m 33 ft wingspan
1 (WSK PZL Rzeszow SO-3W) engines 2 x Turbomeca Makila 2A turboshaft engines
10.8 kN thrust per engine 2,778 hp
10.8 kN total thrust 5,556 hp
3,840 kg 8,466 lb MTOW 11,000 kg 24,251 lb
1,250 km 675 nm range 857 km 463 nm
770 km/h 478 mph cruise speed 242 km/h 150 mph
2 capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.