Airbus H225 Super Puma vs. Bell 412

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Airbus H225 Super Puma versus Bell 412
14.06 m 46 ft 2 in length 17,10 m 56 ft 1 in
4.38 m 14 ft 4 in height 3,48 m 11 ft 5 in
wingspan
2 x Turbomeca Makila 2A turboshaft engines engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
2,778 hp thrust per engine 1,800 hp
5,556 hp total thrust 3,600 hp
11,000 kg 24,251 lb MTOW 5,400 kg 11,905 lb
857 km 463 nm range 659 km 356 nm
242 km/h 150 mph cruise speed 259 km/h 161 mph
24-28 capacity 13
16.2 m 53 ft 2 in rotor diameter 14.0 m 45 ft 11 in
10.7 m/s 2,106 ft/min rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.