There are 10 images added between 22 November 2006 and 2 July 2015
1  2  
Initial Operational Capability (IOC): 1970
Maiden Flight: 1968
Total Production: ?
Also Known As: Haze, Mi-14BT, Mi-14GP, Mi-14P, Mi-14PL, Mi-14PS and Mi-14PW
Origin: Russia
Corporations: Mil Helicopter
Parent System: Mi-8
Initial Operational Capability (IOC): 1967
Maiden Flight: 7 July 1961
Total Production: 12,629
Family Members: Mi-171A1, Mi-171A2, Mi-171M, Mi-171Sh, Mi-171Sh-VN, Mi-17V-5, Mi-8, Mi-8AMTSh-V, Mi-8AMTSh-VA and Mi-8MTPR1
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-14, dubbed Haze by NATO, is an anti-submarine warfare (ASW) amphibious helicopter derived from the Mi-8 military transport helicopter and developed as the replacement for the Soviet Mi-4 helicopter. It is suitable for shore-based and ship-based operations as well as for mine countermeasures and search and rescue (SAR) missions. The Mi-14PL is equipped with dipping sonar, sonobuoys and a magnetic anomaly detector (MAD) in order to hunt down submerged submarines. The Mi-14's internal weapons bay can be fitted with torpedoes, bombs and depth charges in order to take out submarines. Powered by two TV3-117MT engines, each rated at 1,874-shp, the aircraft has a maximum range of 1,100+ kilometers and can achieve a top speed of 230 kilometers per hour. The Mi-14 prototype first flew in 1968 entering service in the 1970s. The surviving aircraft are deemed obsolete and may be replaced in the near future.

Mi-14 Specifications

Crew: 4
Main Rotor Blades: 5
Number of Engines: 2
Tail Rotor Blades: 3
Main Rotor Disc Area: 356 square meter
Height: 6.93 meter (22.7 foot)
Length: 18.4 meter (60 foot)
Main Rotor Diameter: 21.3 meter
Ceiling: 11,500 foot (3,505 meter)
Max Range: 1,135 kilometer (613 nautical mile)
Max Power at TakeOff: 3,748 shp (2,796 kW)
Cruise Speed: 230 kph (143 mph)
Top Speed at High Altitude: 215 kph (116 KTAS)
Flight Endurance: 6 hour (0.25 day)
Empty Weight: 8,900 kilogram (19,621 pound)
Max Takeoff Weight: 14,000 kilogram (30,864 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-14 News

There are 2 news between
2 Jul 2015 and 24 Jun 2016
Friday, June 24, 2016Russian Navy to Integrate Zagon-2 Bomb onto Mi-14 ASW Helicopter
Thursday, July 2, 2015Russian Helicopters Showcases Plans for Renewed Production of Mi-14PS ASW Helicopter

Operators & Related Equipment


Grand Total ?12
Defensive Weapons
Propulsion Systems
Copyright © 2003-2017 website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.