Percival Provost vs. Mil Mi-26

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Percival Provost versus Mil Mi-26
9.0 m 29 ft 6 in length 40.03 m 131.3 ft
3.02 m 9 ft 11 in height 8.15 m 26.7 ft
12.19 m 40 ft wingspan
1 x Alvis Leonides Major 755/1 inline engine engines 2 x Lotarev D-136 turboshaft engines
Approximately 550 hp thrust per engine 8,380 kW
Approximately 550 hp total thrust 16,760 kW
5,500 lb 2,495 kg MTOW 56,000 kg 123,459 lb
1,127 km 608 nm range 800 km 432 nm
175 mph 282 km/h cruise speed 255 km/h 158 mph
Pilot and one passenger capacity Up to 90 passengers
rotor diameter 32.00 m 105 ft 0 in
rate of climb 8 m/s 1,574 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.