Cessna 172 vs. Airbus H225 Super Puma

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Cessna 172 versus Airbus H225 Super Puma
8.28 m 27 ft 2 in length 14.06 m 46 ft 2 in
2.72 m 8 ft 11 in height 4.38 m 14 ft 4 in
11 m 36 ft 1 in wingspan
1 x Lycoming IO-360-L2A flat-4 piston engine engines 2 x Turbomeca Makila 2A turboshaft engines
180 to 200 horsepower (134 to 149 kW) thrust per engine 2,778 hp
180 to 200 horsepower (134 to 149 kW) total thrust 5,556 hp
1,040 kg 2,293 lb MTOW 11,000 kg 24,251 lb
1,056 km 570 nm range 857 km 463 nm
226 km/h 140 mph cruise speed 242 km/h 150 mph
4 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.