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Helicopter
Mi-8
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TECHNICAL SPECIFICATIONS | ||
Crew
3
Maximum speed, km/h: - with normal takeoff weight 250 - with maximum takeoff weight 230 Cruise speed with normal takeoff weight, km/h 225 Maximum altitude, m 4500 Range of flight in the transport version, km: - with normal takeoff weight 465 - with maximum takeoff weight 445 Range of flight with 28 passengers (fuel reserve for 200 minutes of flight), km 500 Normal takeoff weight, kg 11100 Maximum takeoff weight during the vertical takeoff, kg 12000 Maximum payload, kg 4000 Cargo weight at external suspension, kg 3000 Maximum weight of cargo lifted by board boom, kg 150 Base weight of empty helicopter, kg: - in transport version 6624 - in passenger version 6799 Weight of fuel, kg: - in main tanks 1450 - in main and two extra tanks 2870 Helicopter's length with rotating propellers, m 25,24 Dimensions, m: - cargo cabin of transport helicopter 5,34x2,34x1,80 - passenger cabin 6,36x2,34x1,80 - entrance door 0,825x1,405 - cargo hatch in the tail part of the fuselage 1,82x2,34 |
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document maintained by [email protected].
Material Copyright (C) 2000 Stanislav Bogomolov, Adnan Al-Moosawi, Acvilon-Avia |