Rahul Sharma (Editor)

Mil Mi 14

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Top speed
  
230 km/h

Length
  
18 m

Engine type
  
Klimov TV3-117

Wingspan
  
21 m

Introduced
  
1975

First flight
  
September 1969

Mil Mi-14 Mil Mi14 Haze Helicopter Database

Mil mi 14


The Mil Mi-14 (Russian: Миль Ми-14, NATO reporting name: Haze) is a Soviet shore-based nuclear-capable amphibious anti-submarine helicopter derived from the earlier Mi-8.

Contents

Mil Mi-14 Mil Mi14 Haze Naval Helicopter Family MilitaryTodaycom

Landing on rough seas mil mi 14 japan 2016


Design and development

Mil Mi-14 httpsuploadwikimediaorgwikipediacommonsthu

Formal development of an anti-submarine warfare (ASW) version of the Mil Mi-8 transport helicopter was authorised by the Soviet Communist Party Central Committee and Council of Ministers in April 1965, with the objective of replacing the Mil Mi-4 in the short-range, shore based anti-submarine role. The new helicopter was required to have an endurance of 2 hours on station at a radius of 222 kilometres (120 nmi; 138 mi) from base.

Mil Mi-14 Mil Mi14 WOWcom

The new design (with the internal designation V-14) differed from the Mi-8 in having a boat-like hull similar to the Sea King, allowing it to operate off the water, and a retractable four-point undercarriage, with the mainwheels retracting into large sponsons on the rear of the fuselage. The helicopter was to be powered by two Klimov TV3-117MT turboshaft engines. A watertight weapons bay is fitted to the centreline of the fuselage allowing internal carriage of a single torpedo or eight depth charges, while a radome housing a search radar is fitted beneath the nose.

Mil Mi-14 FileMil Mi14 7790728252jpg Wikimedia Commons

The first prototype V-14, converted from a Mi-8 and powered by the older and less powerful Klimov TV2-117 engines, flew on 1 August 1967. Development was slowed by problems with the helicopter's avionics and due to reliability problems with the TV3-117 engines, with production at Kazan not starting until 1973, and the helicopter (now designated Mi-14) entering service on 11 May 1976.

Mil Mi-14 FileMil Mi14 1876473973jpg Wikimedia Commons

Allegedly due to the strong pressure from the United States, all Russian antisubmarine Mi-14 helicopters were decommissioned in 1996. In May 2015, RT has reported that Mi-14 is being highly sought after by the Russian Black Sea and the Northern Fleets, and that Kazan Helicopter Works (KVZ) is preparing to return 10 previously decommissioned helicopters to active Russian Navy service with the production of new units beginning within five years. The initial demand was estimated at 100 helicopters.

In January 2016, Russian Helicopters confirmed to Russian News Agency TASS that no final decision to revive production had been taken, but market demand, feasibility studies – including with Moscow’s defence ministry – and funding sources were under review. The programme remains a “priority” for Russian Helicopters. The company suggested the Mi-14 would appeal to civil operators in Russia’s far north and those supplying the oil and gas industry, alongside the nation’s armed forces. Out of the almost 300 Mi-14s produced at Kazan Helicopters between 1973 and 1986, it is estimated that just 44 examples remain in active service.

Variants

V-14
Prototype of the Mi-14 helicopter.
Mi-14PL (NATO Haze-A)
Anti-submarine warfare helicopter, equipped with towed APM-60 MAD, OKA-2 sonobuoys and a retractable Type 12-M search radar, armed with a single AT-1 or APR-2 torpedo, one Skat nuclear depth bomb, eight depth charges. A single Mi-14PL was used to carry out trials with the Kh-23 (NATO designation AS-7 Kerry) air-to-surface missile but this modification does not seem to have entered service.
Mi-14PLM
Improved anti-submarine warfare version with Os'minog ASW suite, with new search radar, dipping sonar and digital computer. Limited use.
Mi-14PŁ/R
Polish conversion of two Mi-14PŁ (Polish designation for Mi-14PL) to search and rescue version, with ASW equipment removed, developed in 2010.
Mi-14BT (NATO Haze-B)
Mine sweeping helicopter with ASW systems removed and equipped for towing Mine Countermeasures sleds. 25–30 built, with six exported to East Germany and two to Bulgaria.
Mi-14PS (NATO Haze-C)
Search and rescue version with search lights and sliding doors with hoist.
Mi-14PX
Search and rescue training helicopter for the Polish Navy (unofficial designation). One Polish Mi-14PŁ helicopter was temporarily converted into the Mi-14PX, then converted back in 1996.
Mi-14PZh
Amphibious firebuster version of Mi-14BT. Conversion price about USD1M.
Mi-14PZh Eliminator III
Mi-14BT helicopters converted into fire fighting aircraft.
Mi-14GP
Conversion of Mi-14PL to 24–26 seat civil passenger transport.
Mi-14P
24-seat civilian transport helicopter.

Operators

By 1991, about 230 had been delivered, with exports to many Soviet allies including Bulgaria, Cuba, East Germany, Libya, Poland, and Syria.

Current operators

 Georgia
  • Georgian Air Force – 2
  •  Libya
  • Libyan Air Force – 4
  •  North Korea
  • Korean People's Army Air Force – 8
  •  Pakistan
  • Pakistan Navy – 2
  •  Poland
  • Polish Navy – 9
  •  Republic of the Congo
  • Congolese Navy – 1
  •  Syria
  • Syrian Air Force – 11
  •  Ukraine
  • Ukrainian Navy – 3
  •  Yemen
  • Yemen Air Force – 2
  • Former operators

     Bulgaria
  • Bulgarian Navy
  •  Cuba
  • Cuban Air Force
  •  East Germany
  • East German Navy
  •  Germany
  • German Navy
  •  Russia
  • Russian Naval Aviation
  •  Soviet Union
  • Soviet Naval Aviation
  •  Yugoslavia
  • Yugoslav Navy
  • Specifications (Mi-14PL)

    Data from Jane's All The World's Aircraft 1992–93 & http://fas.org

    General characteristics

  • Crew: 4
  • Length: 18.38 m (60 ft 3 in)
  • Rotor diameter: 21.29 m (69 ft 10 in)
  • Height: 6.93 m (22 ft 9 in)
  • Disc area: 356 m² (3,832 ft²)
  • Empty weight: 11,750 kg (25,900 lb)
  • Max. takeoff weight: 14,000 kg (30,865 lb)
  • Powerplant: 2 × Klimov TV3-117MT turboshafts, 1,454 kW (1,950 shp) each
  • Performance

  • Maximum speed: 230 km/h (124 kt)
  • Ferry range: 1,135 km (705 mi)
  • Service ceiling: 3,500 m (11,500 ft)
  • Endurance with max fuel: 4 h
  • Armament

  • torpedoes, bombs and depth charges
  • References

    Mil Mi-14 Wikipedia