Fairey Gannet vs. Mil Mi-26

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Fairey Gannet versus Mil Mi-26
10.87 m 35 ft 8 in length 40.03 m 131.3 ft
3.76 m 12 ft 4 in height 8.15 m 26.7 ft
13.87 m 45 ft 6 in wingspan
1 x Bristol Pegasus XVIII radial engine engines 2 x Lotarev D-136 turboshaft engines
Approximately 690 hp (515 kW) thrust per engine 8,380 kW
Approximately 690 hp (515 kW) total thrust 16,760 kW
7,005 lb 3,178 kg MTOW 56,000 kg 123,459 lb
840 km 454 nm range 800 km 432 nm
139 mph 224 km/h cruise speed 255 km/h 158 mph
Pilot, Observer, and Air Gunner 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.