Mil Mi-8 AMT— (export code Mil Mi-171) – modern modification of a helicopter Mil Mi-8/Mil Mi-17 with improved powerplant (2 engines TV3-117), auxiliary power unit and reducing gear unit VR-14.
Aircraft performance data:
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Manufacturer: Ulan-Ude aircraft plant (since 1991)
Engines: ÒV3-117VM series 2
Takeoff output, h.p.: 2õ1950
Rotary wing diameter, m: 21,288
- Helicopter length with propellers
- fuselage length (without antitorque
- fuselage width: 2,5
- height up to main rotor head: 4,38
- height with ñ rotating antitorque
Dimensions of cargo compartment, m:
- length: 5,34
- width: 2,34
- height: 1,8
- Empty helicopter: 7200
- takeoff normal weight: 11100
- takeoff maximum weight: 13000
- maximum speed near ground: 250
- cruise speed: 220
Crew, men: 3
Number of passengers: 13
Maximum flight range, km: 1000
Mil Mi-8 AMT - (Mil Mi-171) repeats the construction of a helicopter Mil Mi-8T. Upon developing this type vast experience of more than 12 000 Mil Mi-8 helicopters operation in all the climatic and natural zones was taken into account. «Comfort and safety!» – this is the motto, under which this helicopter was being created.
Is assigned for performing a scope of functions: passenger and cargo transportation, abnormal undersling cargo transportation, search and rescue operations, injured people evacuation. A helicopter can fly up to 13 passengers in comfortable conditions: low vibration and noise level, cosy arm-chairs, broad illuminators, conditioner, information and emergency indicating panels, fluorescent lighting. A helicopter is equipped with additional external fuel tanks, a lavatory is available.
A helicopter Mil Mi-8 AMT has a type certificate in Russia and also a certificate of a type acknowledgement in People’s Republic of China, South Korea and Slovakia, is operated in all regions of the Russian Federation.