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Mi-17V-5

Mi-17V-5

Utility & Transport Helicopters
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Basic Information
Name
Mi-17V-5
Designation
Mi-17V-5
Alternate Designation
Mi-17V5, Mi-8MTV-5, Mi-8MTV5-1, Mi-8MTV-5M
Equipment Type
Utility & Transport Helicopters
Manufacturer
Kazan Helicopters, Mil Helicopter, Russian Helicopters
Date of Introduction
2006
Description

The Mi-17V-5, Mi-8MTV-5 Russian Armed Forces designation, is a military transport helicopter optimized for operations in hot climates and high altitudes powered by VK-2500 turboshaft engines. The aircraft is also suitable for day/night operations in all weather conditions and very low altitude using special cabin equipment. Its state-of-the-art navigation system shows all the flight information to the pilot on four multifunctional display screens thus reducing crew's workload. The Mi-17V-5 helicopters are manufactured at the Kazan Helicopter Plant. The Mi-8MTV-5-1 is a version intended to serve with the Russian Armed Forces and law enforcement agencies. It can also serve for search and rescue (SAR) and other specialized tasks. The first Mi-8MTV5-1 was delivered to Russia in October 2014. The Mi-17V-5 entered service in 2006 and is intended as a replacement for aging Mi-8 helicopters. The Indian Armed Forces have ordered more than 150 Mi-17V-5 helicopters so far.

Air & Air Defense Specifications
Crew 2
Max Speed 250.0 km/h
Range 580.0 km
Service Ceiling 6000 m
Overview (Deagel)
Group Utility & Transport Helicopters
Status Active
Also Known As Mi-17V5, Mi-8MTV-5, Mi-8MTV5-1, Mi-8MTV-5M
Origin Russia
Contractors Kazan Helicopters, Mil Helicopter, Russian Helicopters
Initial Operational Capability (IOC) 2006
Total Production 788
Specifications (Deagel)
Crew 2
Main Rotor Blades 5
Number of Engines 2
Stretchers 12
Tail Rotor Blades 3
Troops 37
Area — Main Rotor Disc Area 356 square meter
Dimensions — Cabin Height 1.8 meter
Dimensions — Cabin Length 5.3 meter
Dimensions — Cabin Width 2.3 meter
Dimensions — Height 5.7 meter
Dimensions — Length 18.2 meter
Dimensions — Main Gun Caliber 23 millimeter
Dimensions — Main Rotor Diameter 21.3 meter
Mass — External Payload 4,000 kilogram
Mass — Max Takeoff Weight 13,000 kilogram
Mass — Payload 4,000 kilogram
Performance — Ceiling 6,000 meter
Performance — Max Range 580 kilometer
Power — Max Power at TakeOff 5,400 hp
Speed — Top Speed at High Altitude 250 kph
Volume — Cabin Volume 23 metric ton
Gear (Deagel)
Item 1 Optronic Systems: GOES-321MK (1)
Item 2 Turboshaft Engines: TV3-117VM (2)
Item 3 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
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
18.2 m
Width
Height
5.7 m
Weight
13000 kg
Related Equipment (1)
Operators (13)
Russia
Ukraine
India
Serbia
Belarus
Afghanistan
Egypt
Indonesia
Kenya
Mexico
Nepal
Thailand
Venezuela
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