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TV3-117VMA-SBM1  
Initial Operational Capability (IOC): 2002
Total Production: ?
Origin: Russia
Corporations: Ivchenko-Progress and Motor Sich
Parent System: TV3-117
Initial Operational Capability (IOC):
Total Production: ?
Family Members: TV3-117 and VK-2500
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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.

TV3-117VMA-SBM1 Applications


Airliners An-140 Support Aircraft An-140T

TV3-117VMA-SBM1 Specifications

Service Life Flight Hours: 30,000
Dimensions
Height: 1,209 millimeter (48 inch)
Length: 2,954 millimeter (116 inch)
Propeller Diameter: 3.72 meter
Width: 988 millimeter (38.9 inch)
Power
Emergency Power: 2,800 hp (2,089 kW)
Max Continuous Power: 1,750 hp (1,306 kW)
Max Power at TakeOff: 2,500 hp (1,865 kW)
Weight
Dry Weight: 570 kilogram (1,257 pound)
CEP: Circular Error Probable
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)

Operators & Related Equipment


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Grand Total ?4
 
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