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Mi-171A1  
Initial Operational Capability (IOC): 2002
Total Production: ?
Unitary Cost: USD$12 million
Also Known As: Mi-171E and Mi-171E Salon
Origin: Russia
Corporations: Mil Helicopter, Russian Helicopters and Ulan-Ude Aviation Plant
Parent System: Mi-8
Initial Operational Capability (IOC): 1967
Maiden Flight: 7 July 1961
Total Production: 12,629
Family Members: Mi-14, Mi-171A2, Mi-171M, Mi-171Sh, Mi-171Sh-VN, Mi-17V-5, Mi-8, Mi-8AMTSh-V, Mi-8AMTSh-VA and Mi-8MTPR1
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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-171A1 is a transport helicopter intended for use by civilian operators carrying up to 26 passengers over ranges of 610 kilometers. In addition to the transport role, the Mi-171A1 is suitable for search and rescue (SAR) missions, geological surveying, patrolling, fire-fighting and offshore transportation. The helicopter is powered by two TV3-117VM turboshaft engines rated at 2,200-hp. The Mi-171E variant is fitted with cabin equipment allowing for operations at night and is powered by two VK-2500-03 engines rated at 2,700-hp for operations in hot climates and at high altitude including mountainous terrain. The Mi-171A1/Mi-171E are manufactured at the Ulan-Ude Aviation Plant (UUAP). The civilian Mi-171A1/E leverage designs, technologies and features from the Mi-8AMT, Mi-8MTV-1, Mi-171 and Mi-172 models produced previously.

Mi-171A1 Specifications

Crew: 3
Main Rotor Blades: 5
Number of Engines: 2
Passengers: 26
Tail Rotor Blades: 3
Area
Main Rotor Disc Area: 356 square meter (3,832 square foot)
Dimensions
Cabin Height: 1.80 meter (71 inch)
Cabin Length: 5.34 meter (210 inch)
Cabin Width: 2.34 meter (92 inch)
Height: 5.65 meter (222 inch)
Length: 18.2 meter (715 inch)
Main Rotor Diameter: 21.3 meter (838 inch)
Performance
Ceiling: 6,000 meter (19,685 foot)
Hovering Ceiling: 3,980 meter (13,058 foot)
Max Range: 610 kilometer (329 nautical mile)
Power
Max Power at TakeOff: 4,400 hp (3,282 kW)
Speed
Cruise Speed: 230 kph (124 KTAS)
Top Speed at High Altitude: 250 kph (135 KTAS)
Volume
Cabin Volume: 27 metric ton (953 cu ft)
Weight
Cargo Hook Capacity: 4,000 kilogram (8,818 pound)
Max Takeoff Weight: 13,000 kilogram (28,660 pound)
Payload: 4,000 kilogram (8,818 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-171A1 News

There are 12 news between
6 Dec 2010 and 21 Jul 2017
1  2  
Friday, July 21, 2017Russia to Supply China With 4 Mi-171E Helicopters
Monday, January 16, 2017Pakistan Orders a Mi-171 Helicopter
Tuesday, February 16, 2016China Buys Seven Ka-32A11BC and Two Mi-171 Helicopters
Wednesday, February 10, 2016Government of Uganda Takes Delivery of a Mi-171E Helicopter
Monday, October 26, 2015Russian Helicopters to Supply Rosneft with Two Mi-171s and Two Mi-8AMTs
Saturday, April 25, 2015Argentina to Buy Three Mi-171E Helicopters
Tuesday, October 7, 2014Russian Helicopters delivers Mi-8AMT to Kazakhstan
Wednesday, August 6, 2014Ulan-Ude Aviation Plant Produces 850th Mi-171 Series Helicopter
Wednesday, October 23, 2013Almaty Rescue Service Orders Mi-8AMT and Ka-226T Helicopters
Tuesday, August 27, 2013Vertical de Aviacion Orders Five Mi-171A1 and Five Ka-62 Helicopters

Operators & Related Equipment


OperatorsItems
Angola?
A new batch of Mi-17 aircraft ordered in October 2013
Argentina5
Two Mi-171E ordered by Ministry of Defense for the Air Force in 2010 and an additional three ordered in 2015
YearHoldings
20132Mi-171E
20112
Brazil2
Aircraft ordered by Petrobras (2 Mi-171A1); Atlas Taxi Aereo (?)
Cameroon?
Undisclosed number of Mi-17 helicopters ordered in August 2013
China90
Aircraft ordered by Poly Technologies (84 Mi-171E); private customers (4)
Colombia5
Aircraft ordered by Vertical de Aviacion (5 Mi-171A1)
Ecuador2
Two Mi-17 helicopters purchased in October 2009
Kazakhstan1
Aircraft ordered by Almaty Rescue Service (1 Mi-8AMT)
YearHoldings
20124Mi-8AMTSh
Pakistan2
Aircraft ordered by Balochistan provincial government (1); Punjab province government (1)
Russia?
Aircraft ordered by RN-Aerokraft (4)
Sri Lanka?
Mi-17
Thailand3
Mi-17 helicopters purchased for civil use
Uganda1
Aircraft ordered by the government Mi-171E (1)

Grand Total 11216
Propulsion Systems
TV3-117VMx2
VK-2500-03x2
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