North American BT-9 vs. Airbus H225 Super Puma

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North American BT-9 versus Airbus H225 Super Puma
8.79 m 28 ft 10 in length 14.06 m 46 ft 2 in
2.82 m 9 ft 3 in height 4.38 m 14 ft 4 in
10.97 m 36 ft wingspan
1 x Wright R-975-3 radial engine engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 440 hp thrust per engine 2,778 hp
Approximately 440 hp total thrust 5,556 hp
4,300 lb 1,950 kg MTOW 11,000 kg 24,251 lb
917 km 495 nm range 857 km 463 nm
150 mph 241 km/h cruise speed 242 km/h 150 mph
Pilot and one passenger 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.