
In numbers Through the lens Video
The Mi-14 is a medium multirole amphibious helicopter powered by two TV3-117M 1.950-hp turboshaft engines. Its first prototype, V-14, made its maiden flight on 1 August 1967 and was in production at the Kazan Helicopter Plant in 1973-1986 in several versions.
A total of 273 machines were manufactured, of which around 120 were exported to 11 nations around the globe. The machine has been fielded with the Russian Navy from 1976.
Its primary versions are as follows: Mi-14PL ASW helicopter featuring the Kalmar search/sighting system as well as torpedo and bomb ordnance (1969), Mi-14PS 19-seat search-and-rescue (SAR) helicopter (1974), Mi-14BT mine sweeper (1973), Mi-14PG passenger/transport helicopter (1995), etc.
Technical specifications
DESIGNER | OKB Mil |
COUNTRY | Russia |
TYPE |
Anti-submarine helicopter
|
CREW | 2-3 (+3 system operators) |
POWER-PLANT | Two turboshaft engines Klimov TV3-117MT |
Power, h.p. | 2x1.980 |
DIMENSIONS | |
Length, m | 18,38 |
Main rotor diameter, m | 21,29 |
Tail rotor diameter, m | 3,91 |
Height, m | 6,93 |
WEIGHT | |
Maximum take-off, kg | 14.400 |
Normal take-off, kg | 13.000 |
Empty, kg | 8.902 |
Internal fuel, l | 3.795 |
Weight of transported fuel with external tanks, l | - |
Warload, kg | |
- internal bombs bay | 3.000 |
Payload, kg | - |
PERFORMANCE | |
Maximum speed, km/h | 230 |
Cruising speed, km/h | 215 |
Range, km | 915 |
Ferry range, km | 1.135 |
Combat range, km | 200 |
Service ceiling, m | 3.500 |
Static ceiling, m | 1.600 |
Rate of climb, m/s | - |
Maximum overload, g | - |
ARMAMENT | Anti-submarine torpedos and depth bombs. |