There are 17 images added between 25 March 2013 and 5 November 2015
1  2  3  
Mi-171A2  
Initial Operational Capability (IOC): 2017
Maiden Flight: 23 September 2014
Total Production: 7
Origin: Russia
Corporations: KRET, Mil Helicopter, Russian Helicopters* and Ulan-Ude Aviation Plant   (*) lead contractor
Parent System: Mi-8
Initial Operational Capability (IOC): 1967
Maiden Flight: 7 July 1961
Total Production: 12,632
Family Members: Mi-14, Mi-171A1, Mi-171M, Mi-171Sh, Mi-171Sh-VN, Mi-17V-5, Mi-8, Mi-8AMTSh-V, Mi-8AMTSh-VA and Mi-8MTPR1
Reviews
There are no reviews so far

Description: The MIL Mi-8, dubbed Hip by NATO, is a twin-engine, multi-role, medium transport helicopter capable of transporting troops and equipment or conducting ground attack missions. Besides, the aircraft is also suitable for civilian operators related to a variety of transportation roles. The Mi-8 was developed in the late 1950s and 1960s by the Soviet Union, first flew on July 7, 1961, entering service in 1967. The five-bladed main rotor is driven by either two TV2-117 or TV3-117 turboshaft engines rated from 1,700-shp to 2,200-shp allowing a top speed of 230-250 kilometers per hour. In addition to its crew of two/three men, the standard Mi-8 can transport as many as 24/28 troops. The Mi-17 was the export designation for the Soviet Mi-8. The Mi-171 refers to the modern production standard introduced in 1991. The aircraft design and technologies evolved over 60 years with the current production standards (various models) being far more sophisticated and performant than early models. More than 12,000 Mi-8/17/171 helicopters of all models were produced or are in production for the Soviet Union, Russia and international customers. As of November 2013, roughly 2,400 Mi-8/Mi-17 helicopters remain in service worldwide. In January 2015 that figure had increased to 2,469 aircraft with several models remaining in production beyond 2020.

The Mi-171A2 is the civil market version of the Mi-171M military transport helicopter. Over 80 innovations are planned to be used on the Mi-171A2 helicopter achieving improved performance over previous Mi-8/17 models. The cost of flight hour on the highly affordable Mi-171A2 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. The first aircraft is expected to get airborne in 2014 and enter serial production with first customer deliveries in 2015.

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-171A2 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-171A2 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.

Mi-171A2 Specifications

Crew: 2
Main Rotor Blades: 5
Number of Engines: 2
Tail Rotor Blades: 3
Performance
Max Range: 850 kilometer (459 nautical mile)
Power
Max Power at TakeOff: 4,800 shp (3,581 kW)
Temperature
Max Operating Temperature: +50 � Celsius
Min Operating Temperature: -50 � Celsius
Weight
Payload: 5,000 kilogram (11,023 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Mi-171A2 News

There are 11 news between
23 Jan 2012 and 13 Nov 2017
1  2  
Monday, November 13, 2017Vectra Group Orders a Mi-171A2 Helicopter
Thursday, July 20, 2017United Helicopters Orders Five Ansat, Three Mi-171A2 and Two Ka-32A11BC Helicopters
Sunday, February 19, 2017Mi-171A2 Helicopter Enters Serial Production
Wednesday, November 2, 2016Jiangsu Baoli Aviation Equipment Orders Mi-171A, Ansat and Ka-32 Helicopters
Tuesday, November 1, 2016Chinese Company Becomes First Export Customer of Ansat Helicopter
Thursday, May 21, 2015Russian Helicopters Successfully Conclude Flight Tests on the Mi-171A2 Flying Laboratory
Tuesday, November 25, 2014Mi-171A2 Helicopter Enters Flight Testing Phase
Tuesday, September 23, 2014Mi-171A2 Helicopter Enters Flight Testing Phase with KBO-17 Cockpit
Thursday, March 13, 2014Rosoboronexport and Russian Helicopters Deliver 3,500th Mi-17 Helicopter
Wednesday, August 21, 2013Russian Helicopters Delivers 750th Mi-8AMT/Mi-171 Production Helicopter

Operators & Related Equipment


OperatorsItems
China6
Aircraft ordered by Wuhan Rand Aviation (2); Jiangsu Baoli Aviation Equipment (1); United Helicopters (3)
India1
Aircraft ordered by Vectra Group (1)

Grand Total 73
Propulsion Systems
VK-2500PS-03x2
Copyright © 2003-2017 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.