AgustaWestland AW109 vs. Mil Mi-26

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AgustaWestland AW109 versus Mil Mi-26
13,04 m 42 ft 9 in length 40.03 m 131.3 ft
3,40 m 11 ft 2 in height 8.15 m 26.7 ft
wingspan
2 × Pratt & Whitney Canada PW206C or 2 × Pratt & Whitney Canada PW207C engines 2 x Lotarev D-136 turboshaft engines
638 shp (476 kW) thrust per engine 8,380 kW
1276 shp (952 kW) total thrust 16,760 kW
3,175 kg 7,000 lb MTOW 56,000 kg 123,459 lb
932 km 503 nm range 800 km 432 nm
285 km/h 177 mph cruise speed 255 km/h 158 mph
1 or 2 pilots + up to 7 passengers capacity Up to 90 passengers
11.00 m 36 ft 1 in rotor diameter 32.00 m 105 ft 0 in
651 m/min 2,136 ft/min 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.