Brewster F2A Buffalo vs. Airbus H225 Super Puma

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Brewster F2A Buffalo versus Airbus H225 Super Puma
8.03 m 26 ft 4 in length 14.06 m 46 ft 2 in
3.66 m 12 ft height 4.38 m 14 ft 4 in
10.67 m 35 ft wingspan
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines 2 x Turbomeca Makila 2A turboshaft engines
950 horsepower thrust per engine 2,778 hp
950 horsepower total thrust 5,556 hp
3,247 kg 7,159 lb MTOW 11,000 kg 24,251 lb
1,664 km 900 mi range 857 km 463 nm
259 km/h 161 mph cruise speed 242 km/h 150 mph
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.