de Havilland Canada DHC-6 Twin Otter vs. Airbus H225 Super Puma

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de Havilland Canada DHC-6 Twin Otter versus Airbus H225 Super Puma
15.32 m 50 ft 3 in length 14.06 m 46 ft 2 in
5.94 m 19 ft 6 in height 4.38 m 14 ft 4 in
19.81 m 65 ft wingspan
2 x Pratt & Whitney Canada PT6A-27 turboprop engines engines 2 x Turbomeca Makila 2A turboshaft engines
550 to 750 shaft horsepower (410 to 560 kW) thrust per engine 2,778 hp
1100 to 1500 shaft horsepower total thrust 5,556 hp
5,670 kg 12,500 lb MTOW 11,000 kg 24,251 lb
1,389 km 750 nm range 857 km 463 nm
280 km/h 174 mph cruise speed 242 km/h 150 mph
19 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.