Fairchild PT-19 Cornell vs. Airbus H225 Super Puma

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Fairchild PT-19 Cornell versus Airbus H225 Super Puma
8.79 m 28 ft 10 in length 14.06 m 46 ft 2 in
2.26 m 7 ft 5 in height 4.38 m 14 ft 4 in
10.97 m 36 ft wingspan
1 x Ranger L-440-5 inline engine engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 175 hp thrust per engine 2,778 hp
Approximately 175 hp total thrust 5,556 hp
2,450 lb 1,111 kg MTOW 11,000 kg 24,251 lb
660 km 356 nm range 857 km 463 nm
125 mph 201 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.