Wednesday, December 03, 2008

TV3-117

TV3-117VMA-SBM1

IOC: 2002

Origin
Russia

Contractor/s
Ivchenko-Progress
Motor Sich

Applications
An-140

Family Members
TV3-117

Description: The Ivchenko-Progress TV3-117VMA-SBM1 is a turboprop based on the gas generator of TV3-117VMA helicopter turbine designed by Klimov plant. In addition, the TV3-117VMA-SBM1 also incorporates the reduction gear from the AI-24 turbine. This reliable and cost effective engine is intended to power regional turboprop aircraft. The engine responds to a two-shaft, modular design with advanced monitoring and diagnostic system.

The TV3-117VMA-SMB1 engine has been selected to power the Antonov An-140 twin-engine turboprop passenger aircraft.

Specifications
Dimensions: Height 1,209 mm, Length 2,953.50 mm, Propeller Diameter 3.7 m, Width 988.30 mm

Weights: Dry Weight 570 kg (1,257 lb)

Power: Emergency Power 2,800 hp, Max Continuous Power 1,750 hp, Max Power at TakeOff 2,500 hp

Other: Service Life (Flight Hours) 30,000

Operators

see operators map | see family operators map

Azerbaijan

Iran

Russia

Ukraine

Image Gallery

Internet Resources
ivchenko-progress.com

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)

Last Updated: Saturday, November 22, 2008

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