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Mil Mi-14

Mil Mi-14 © Mariusz Adamski
Photo ©: Mariusz Adamski http://air2air.net

Mi-14

Naval Utility Helicopter

The Mil Mi-14 is a twin-engined medium naval utility helicopter developed by the Soviet manufacturer Mil OKB, today MIL Moscow helicopter plant, JSC (Russia). The main purposes of the Mi-14 are anti-submarine warfare, mine countermeasures and search and rescue operations (SAR).

Crew4
 
Propulsion2 Turboshaft Engines
Engine ModelKlimow / Klimov TW3-117MT / TV3-117MT
Engine Power (each)1435 kW1924 shp
 
Speed230 km/h124 kts
  143 mph
Service Ceiling4.000 m13.123 ft
Range800 km432 NM
497 mi.
 
Empty Weight8.900 kg19.621 lbs
max. Takeoff Weight14.000 kg30.865 lbs
 
Rotor Blades (main/tail)5/35/3
Main Rotor Diameter21,29 m69,8 ft
Tail Rotor Diameter3,91 m12,8 ft
Rotor Disc Area356,0 m²3832 ft²
Length18,38 m60,3 ft
Height6,93 m22,7 ft
 
First Flight09/1969
Production Statusout of production
Total Productionca. 230
Developed fromMil Mi-8
 
NATO CodeHaze
Data for (Version)Mil Mi-14PL

Remarks
The Mil Mi-14 is an amphibious development of the Mil Mi-8.


WeblinksExtras
MIL Moscow helicopter plant, JSC

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