Max Holste M.H.1521 Broussard vs. Airbus H225 Super Puma

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Max Holste M.H.1521 Broussard versus Airbus H225 Super Puma
10.46 m 34 ft 4 in length 14.06 m 46 ft 2 in
2.74 m 9 ft height 4.38 m 14 ft 4 in
12.86 m 42 ft 2 in wingspan
1 x Lycoming GSO-480-B1A6 flat-six engine engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 295 hp thrust per engine 2,778 hp
Approximately 295 hp total thrust 5,556 hp
1,900 kg 4,189 lb MTOW 11,000 kg 24,251 lb
1,030 km 556 nm range 857 km 463 nm
145 mph 233 km/h cruise speed 242 km/h 150 mph
5-7 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.