Avro 652 Anson vs. Mil Mi-26

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Avro 652 Anson versus Mil Mi-26
12.88 m 42 ft 3 in length 40.03 m 131.3 ft
2.9 m 9 ft 6 in height 8.15 m 26.7 ft
17.22 m 56 ft 6 in wingspan
2 × Armstrong Siddeley Cheetah VI engines 2 x Lotarev D-136 turboshaft engines
290 hp (220 kW) thrust per engine 8,380 kW
580 hp (440 kW) total thrust 16,760 kW
7,500 lb 3,402 kg MTOW 56,000 kg 123,459 lb
1,267 km 684 nm range 800 km 432 nm
165 mph 266 km/h cruise speed 255 km/h 158 mph
4 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.