TV3-117VM Series 02 Engine Mi-8 Mi-17
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TV3-117VM Series 2

ENGINE

AvailabilityOut of stock
Availability
Out of stock
Warranty
6 Months
Condition
Repairable
Price on request

Price and lead time are confirmed before payment.

Description

TV3-117VM Series 02 turboshaft engine for civil helicopters

TV3-117VM Series 02 is a turboshaft aircraft engine with a free turbine, designed mainly for civil helicopters of the Mi-8 / Mi-17 family. The engine works as part of the helicopter powerplant system and supplies mechanical power to the transmission. It is intended for long-term helicopter operation with stable output, controlled fuel consumption and reliable response in normal and emergency flight conditions. The Series 02 version is especially associated with civil helicopter applications where continued safe flight after one engine failure is an important operational requirement.

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OEI safety function of TV3-117VM Series 02

The TV3-117VM Series 02 supports one-engine-inoperative operation. In the event of one engine failure on a twin-engine helicopter, the remaining engine must provide increased power for a limited time so the crew can continue flight, perform an approach or land safely. The engine supports short-term and extended OEI power modes, giving the helicopter an additional safety margin under abnormal operating conditions. These modes must be used strictly according to the aircraft and engine operating documentation, because duration, temperature limits and power setting are controlled parameters.

Power modes of the TV3-117VM Series 02 engine

The TV3-117VM Series 02 provides high output in emergency and takeoff-related regimes and maintains efficient operation in cruise. Power data are normally referenced to sea level, zero Mach number and ISA conditions. The engine can deliver emergency power, extended OEI power and cruise power depending on operating mode and permitted duration. These characteristics allow Mi-8 / Mi-17 family helicopters to perform civil transport, utility and support missions while retaining the power margin required for safety-critical situations. Actual available power depends on ambient temperature, altitude, installation and aircraft configuration.

Free-turbine layout and installed accessories

The TV3-117VM Series 02 uses a free-turbine configuration, allowing the gas generator and power turbine to operate as part of the helicopter engine and transmission system. The engine is fitted with accessory equipment for starting, fuel supply, control, lubrication and electrical support. Main installed units may include the accessory gearbox, NR-3VM fuel control / pump-regulator, SV-78BA air starter or equivalent starter configuration, ERD-3VM electronic engine regulator, high-pressure fuel pump, oil system units, centrifugal breather, generator and sensors for pressure, gas temperature and vibration control.

Application of TV3-117VM Series 02 on Mi-8 / Mi-17 helicopters

The TV3-117VM Series 02 is used on helicopters of the Mi-8 / Mi-17 family, depending on aircraft modification and approved powerplant configuration. It is suitable for civil helicopter service where the aircraft documentation permits installation of this engine type. The engine may be interchangeable with other TV3-117 family engines within approved limits, but this must be checked by configuration, aircraft records, service bulletins and installation documentation. Interchangeability should not be assumed only from the engine family name, because installed accessories, control system configuration and operating limits may differ.

Identification and documentation for TV3-117VM Series 02

Before ordering or installing TV3-117VM Series 02, the exact engine designation, series, accessory configuration, condition and documentation set should be confirmed. Dry weight, power limits and installed equipment depend on the specified configuration and should be checked against the passport or technical records. For operational acceptance, the engine logbook, passport, maintenance history, storage records and remaining life are as important as the physical condition of the unit. For supply, it is useful to specify helicopter type, required condition, remaining resource, included accessories and documentation availability.

Technical details

Product Type
Turboshaft aircraft engine with free turbine
Engine Designation
TV3-117VM Series 02
Alternative Designations
TV3-117VM Series 2, TV3-117VM Ser. 02, TV3-117 VM Series 02, TV3-117VM seriya 02
Function
Primary helicopter powerplant for civil Mi-8 / Mi-17 family helicopters
Application / Where Used
Helicopter powerplant system
All specificationsCollapse specifications
System / Installation Area
Engine installation / helicopter propulsion system
Compatible Aircraft / Equipment
Mi-8 / Mi-17 family helicopters, depending on approved configuration
Engine Type
Gas-turbine turboshaft engine
Turbine Arrangement
Free turbine
Operating Conditions Reference
Sea level, zero Mach number, ISA
Emergency Power Mode
2400 hp / 1765 kW
Emergency Power Mode, 2.5 min OEI
2200 hp / 1618 kW
Extended OEI Power Mode, 30 min
2000 hp / 1471 kW
Takeoff Power
2000–2200 hp / 1471–1618 kW
Cruise Power
1500 hp / 1103 kW
Specific Fuel Consumption
0.210 kg/hp·h / 0.286 kg/kW·h
Free Turbine Speed
15,000 rpm at 100%
Dry Weight
294 kg
Length with Exhaust Pipe
2055 mm
Height
728 mm
Width
660 mm
Accessory Gearbox
Installed, for driving engine accessories
Fuel Control Unit
NR-3VM pump-regulator
Electronic Engine Regulator
ERD-3VM
Starter
SV-78BA air starter or approved starter configuration
Lubrication System Equipment
Oil pressure and scavenge units, centrifugal breather
Electrical Equipment
AC generator, depending on configuration
Sensors and Signalling Units
Pressure, gas temperature and vibration monitoring devices
Interchangeability
Compatible with TV3-117 family engines within approved limits
Technical Documentation
Technical and operational documentation, passport, engine logbook and maintenance records, if available

Payment & delivery

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TV3-117VM Series 2