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Mi-171 Russian Medium Transport Helicopter

Mi-171M

Utility & Transport Helicopters
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Basic Information
Name
Mi-171 Russian Medium Transport Helicopter
Designation
Mi-171M
Alternate Designation
Mi-171
Equipment Type
Utility & Transport Helicopters
Manufacturer
Russian Helicopters, KRET, Mil Helicopter, Ulan-Ude Aviation Plant
Date of Introduction
2015
Description

The Mi-171M is a cost effective advanced version of the Mi-171 helicopter and is intended as the replacement for aging Mi-8 and Mi-17 aircraft. Russian Helicopters launched the Mi-171M program in 2009 with flight testing and certification slated for completion by the end of 2012. The first prototype should roll-off the production plant in 2011. Serial production is expected to start in 2013 at Ulan-Ude Aviation Plant (UUAP). The Mi-171M will be certified according to AP-29 norms, and it is planned to receive foreign certifications to enter the export market where high demand is forecast. Over 80 innovations are planned to be used on the Mi-171M helicopter achieving improved performance over previous Mi-8/17 models. The helicopter will be fitted with two more powerful VK-2500 engines than the current TV3-117 turboshafts, an Auxiliary Power Unit (APU) with launch altitude up to 6,000 meters, a modernized main gearbox, swash plate, main rotor head, transmission, composite main rotor blades, and X-shaped tail rotor. The aircraft's crew will be brought down to two. The Mi-171M will be fitted with a digital autopilot in standard configuration, and will offer a glass cockpit as option. The range without additional fuel tanks will reach 850 km, the helicopter will carry up to 5,000 kg externally and fly at a higher cruise speed. The Mi-171M will be more stable in flight and will be able to hover at higher side wind speeds. It will have a -50 to +50 Celsius operating temperature range in all climate zones. The cost of flight hour on the highly affordable Mi-171M will be less than on the Mi-17/171 helicopters keeping a key advantage in the export market. Its service life will greatly increase as well as the time between overhauls (TBO) with future growth to make possible multifunctional test and control checks with modern on-ground maintenance equipment. The operating manuals will meet the best international standards.

Air & Air Defense Specifications
Crew 2
Engine Turboshaft (2070 hp)
Max Speed 250.0 km/h
Range 850.0 km
Service Ceiling 4500 m
Overview (Deagel)
Group Utility & Transport Helicopters
Status Cancelled
Origin Russia
Contractors Russian Helicopters*, KRET, Mil Helicopter, Ulan-Ude Aviation Plant
Initial Operational Capability (IOC) 2015
First Flight 2014
Total Production ?
Specifications (Deagel)
Crew 2
Main Rotor Blades 5
Number of Engines 2
Tail Rotor Blades 3
Mass — Payload 5,000 kilogram
Performance — Max Range 850 kilometer
Power — Max Power at TakeOff 4,800 shp
Temperature — Max Operating Temperature 50 ° Celsius
Temperature — Min Operating Temperature -50.00 ° Celsius
Gear (Deagel)
Item 1 Turboshaft Engines: VK-2500 (2)
Variants
Variant 1 Mi-8
Variant 2 Mi-14
Variant 3 Mi-171A1
Variant 4 Mi-171Sh
Variant 5 Mi-17V-5
Variant 6 Mi-171M
Variant 7 Mi-8AMTSh-V
Variant 8 Mi-8MTPR1
Variant 9 Mi-8AMTSh-VA
Variant 10 Mi-171A2
Variant 11 Mi-171Sh-VN
Variant 12 Mi-171A3
Details
Country of Origin Russia
Category Transport Helicopter
Air > Transport Helicopter
Filter Label
M
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
25.2 m
Width
2.5 m
Height
5.65 m
Weight
13000 kg
Related Equipment (2)
Operators (21)
Russia
China
Ukraine
Iran
Pakistan
Czech Republic
Algeria
Argentina
Bangladesh
Burkina Faso
Chad
Croatia
Ghana
Indonesia
Iraq
Kazakhstan
Mongolia
Nepal
Nigeria
Peru
Sudan
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