Auster AOP.9 vs. Mil Mi-26

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Auster AOP.9 versus Mil Mi-26
7.23 m 23 ft 9 in length 40.03 m 131.3 ft
2.72 m 8 ft 11 in height 8.15 m 26.7 ft
11.1 m 36 ft 5 in wingspan
1 x Blackburn Cirrus Bombardier 203 engines 2 x Lotarev D-136 turboshaft engines
134 kW (180 hp) thrust per engine 8,380 kW
134 kW (180 hp) (As it has only one engine) total thrust 16,760 kW
966 kg 2,130 lb MTOW 56,000 kg 123,459 lb
628 km 339 nm range 800 km 432 nm
177 km/h 110 mph cruise speed 255 km/h 158 mph
3 (pilot and two passengers) 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.