de Havilland Canada DHC-3 Otter vs. Airbus H225 Super Puma

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de Havilland Canada DHC-3 Otter versus Airbus H225 Super Puma
10.52 m 34 ft 6 in length 14.06 m 46 ft 2 in
3.84 m 12 ft 7 in height 4.38 m 14 ft 4 in
17.68 m 58 ft wingspan
1 x Pratt & Whitney R-1340 radial engine engines 2 x Turbomeca Makila 2A turboshaft engines
400 to 600 horsepower (298 to 447 kW) thrust per engine 2,778 hp
400 to 600 horsepower (298 to 447 kW) total thrust 5,556 hp
5,670 kg 12,500 lb MTOW 11,000 kg 24,251 lb
1,296 km 700 nm range 857 km 463 nm
215 km/h 134 mph cruise speed 242 km/h 150 mph
10-11 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.