Fouga CM.170 Magister vs. Mil Mi-26

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Fouga CM.170 Magister versus Mil Mi-26
10.06 m 33 ft 0 in length 40.03 m 131.3 ft
2.8 m 9 ft 2 in height 8.15 m 26.7 ft
12.15 m 39 ft 1 wingspan
Two Turbomeca Marboré IIA turbojets engines 2 x Lotarev D-136 turboshaft engines
3.9 kN thrust per engine 8,380 kW
7.8 kN total thrust 16,760 kW
3,200 kg 7,050 lb MTOW 56,000 kg 123,459 lb
924 km 499 nm range 800 km 432 nm
715 km/h 444 mph cruise speed 255 km/h 158 mph
2 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.