Mil Mi-14 Haze

Summary

Category Military Helicopters
Origin country 🇨🇳 Ex-USSR
ManufacturerMil
First flight1 August 1967
Year introduced1975
Number produced273 units

Technical specifications

Version: Mi-14PL Haze-A
Crew4 members
Operational range1,135 km (705 mi)
Maximum speed 230 km/h (143 mph)
Height6.9 m (22.7 ft)
Length18.4 m (60.3 ft)
Service ceiling3,500 m (11,483 ft)
Empty weight11,750 kg (25,904 lbs)
Max. takeoff weight14,000 kg (30,865 lbs)
Powerplant2 x turboprops Klimov TV3-117MT delivering 1454 kW each

Current operating countries

Country Units
Syria Syria 10
North Korea North Korea 8
Poland Poland 4
Ukraine Ukraine 4
Libya Libya 3
Georgia Georgia 2
Pakistan Pakistan 2
Yemen Yemen 2
Congo Congo 1

All operators

🇧🇬 Bulgaria • 🇨🇬 Congo • 🇨🇺 Cuba • 🇩🇪 Ex-East Germany • 🇩🇪 Germany • 🇪🇹 Ethiopia • 🇬🇪 Georgia • 🇱🇾 Libya • 🇵🇰 Pakistan • 🇵🇱 Poland • 🇰🇵 North Korea • 🇷🇺 Russia • 🇸🇾 Syria • 🇺🇦 Ukraine • 🇨🇳 Ex-USSR • 🇾🇪 Yemen • 🇳🇱 Ex-Yugoslavia

Armament

Bombs payload:

  • Anti-Submarine PLAB-250-120

Profile drawing of Mil Mi-14 Haze

Description

Formal development of an anti-submarine warfare (ASW) version of the Mil Mi-8 transport helicopter was authorized in April 1965, with the objective of replacing the Mil Mi-4 in the short-range, shore-based anti-submarine role. Designated as V-14 internally, the new design differed from the Mi-8 by featuring a boat-like hull, enabling it to operate off the water, and a retractable four-point undercarriage. Power was provided by two Klimov TV3-117MT turboshaft engines. The first prototype V-14, converted from a Mi-8, flew on 1 August 1967. Development was slowed by problems with the avionics and reliability issues with the TV3-117 engines. Production at Kazan started in 1973, and the helicopter, now designated Mi-14, entered service on 11 May 1976. Between 1973 and 1986 almost 300 Mi-14s were produced at Kazan Helicopters.

The Mil Mi-14 features a distinctive boat-like hull, enabling amphibious operation. This design is complemented by a retractable four-point undercarriage, with mainwheels that retract into large sponsons located on the rear fuselage. Power is supplied by two Klimov TV3-117MT turboshaft engines. The helicopter is equipped with a watertight weapons bay along the fuselage's center line, facilitating the internal carriage of a single torpedo or up to eight depth charges. A radome, which houses a search radar, is situated beneath the nose, enhancing its detection capabilities. The Mi-14PL anti-submarine version includes specialized equipment such as a retractable Type 12-M search radar, a dipping sonar, a towed APM-60 Magnetic Anomaly Detector (MAD), and OKA-2 sonobuoys to locate underwater targets. For engaging detected submarines, it could be armed with either a single AT-1 or APR-2 torpedo, or a single Skat nuclear depth bomb, or up to eight conventional depth charges. One Mi-14PL was experimentally fitted to carry the Kh-23 air-to-surface missile, though this modification was not adopted for operational service.

The Mi-14 saw operational use across various theaters and with numerous air forces. By 1991, approximately 230 units had been delivered to countries including Bulgaria, Cuba, East Germany, Libya, Poland, and Syria. Syrian Navy Mi-14 helicopters were deployed during the Syrian civil war from 2013 onwards, being employed to drop naval mines and barrel bombs. One such helicopter crashed in March 2015, resulting in the pilot's death and the capture of the remaining crew. A Ukrainian Mi-14PS was shot down by a Russian Su-35 in May 2022, leading to the death of Colonel Ihor Bedzay, the deputy head of the Ukrainian Navy.

Main Variants:

  • V-14: This was the prototype of the Mi-14 helicopter.

  • Mi-14PL (NATO Haze-A): This anti-submarine warfare helicopter was equipped with towed APM-60 MAD, OKA-2 sonobuoys, and a retractable Type 12-M search radar, and was armed with torpedoes, depth bombs, or depth charges.

  • Mi-14PLM: This improved anti-submarine warfare version featured the Os'minog ASW suite, which included a new search radar, dipping sonar, and digital computer, though it saw only limited use.

  • Mi-14BT (NATO Haze-B): This mine sweeping helicopter had its ASW systems removed and was equipped for towing Mine Countermeasures sleds.

  • Mi-14PS (NATO Haze-C): This was a search and rescue version equipped with search lights and sliding doors with a hoist.

Frequently Asked Questions

What type of aircraft is the Mi-14 Haze?
The Mil Mi-14 Haze is a military helicopters aircraft developed by Mil and entered service in 1975.
What is the maximum speed of the Mi-14 Haze?
The Mil Mi-14 Haze has a maximum speed of 230 km/h (142 mph).
What is the range of the Mi-14 Haze?
The Mil Mi-14 Haze has an operational range of 1,135 km (705 miles). This range can vary based on payload, altitude, and mission profile.
When did the Mi-14 Haze first fly?
The Mil Mi-14 Haze made its first flight on August 01, 1967. It entered operational service in 1975.
How many Mi-14 Haze have been built?
Approximately 273 units of the Mil Mi-14 Haze have been produced since it entered service in 1975.
Which countries operate the Mi-14 Haze?
The Mil Mi-14 Haze is operated by 9 countries with approximately 36 aircraft in active service. The largest operators include Syria, North Korea, and Poland.
What is the service ceiling of the Mi-14 Haze?
The Mil Mi-14 Haze has a service ceiling of 3,500 meters (11,482 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Wikipedia and other open sources. Suggest a change