Piper PA-34 Seneca vs. Airbus H225 Super Puma

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Piper PA-34 Seneca versus Airbus H225 Super Puma
8.71 m 28 ft 7 in length 14.06 m 46 ft 2 in
2.99 m 9 ft 10 in height 4.38 m 14 ft 4 in
11.64 m 38 ft 2 in wingspan
2 x Continental IO-360 engines 2 x Turbomeca Makila 2A turboshaft engines
220 lbs thrust per engine 2,778 hp
440 lbs total thrust 5,556 hp
4,750 lb 2,155 kg MTOW 11,000 kg 24,251 lb
980 nm 1,815 km range 857 km 463 nm
165 kts 103 mph cruise speed 242 km/h 150 mph
5 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.