Percival Provost vs. Airbus H225 Super Puma

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Percival Provost versus Airbus H225 Super Puma
9.0 m 29 ft 6 in length 14.06 m 46 ft 2 in
3.02 m 9 ft 11 in height 4.38 m 14 ft 4 in
12.19 m 40 ft wingspan
1 x Alvis Leonides Major 755/1 inline engine engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 550 hp thrust per engine 2,778 hp
Approximately 550 hp total thrust 5,556 hp
5,500 lb 2,495 kg MTOW 11,000 kg 24,251 lb
1,127 km 608 nm range 857 km 463 nm
175 mph 282 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.