Auster AOP.9 vs. Airbus H225 Super Puma

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Auster AOP.9 versus Airbus H225 Super Puma
7.23 m 23 ft 9 in length 14.06 m 46 ft 2 in
2.72 m 8 ft 11 in height 4.38 m 14 ft 4 in
11.1 m 36 ft 5 in wingspan
1 x Blackburn Cirrus Bombardier 203 engines 2 x Turbomeca Makila 2A turboshaft engines
134 kW (180 hp) thrust per engine 2,778 hp
134 kW (180 hp) (As it has only one engine) total thrust 5,556 hp
966 kg 2,130 lb MTOW 11,000 kg 24,251 lb
628 km 339 nm range 857 km 463 nm
177 km/h 110 mph cruise speed 242 km/h 150 mph
3 (pilot and two passengers) 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.