D-136-2  
Initial Operational Capability (IOC): 2012
Total Production: 52
Origin: Russia
Corporations: Ivchenko-Progress
Parent System: D-136
Initial Operational Capability (IOC): 1983
Total Production: 672
Family Members: D-136
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Description: The D-136-2 is an upgraded version of the D-136 turboshaft engine intended to power the Mi-26T2 ultra-heavy helicopter. The D-136-2 engine features Full Authority Digital Electronic Control (FADEC), an emergency power output of 12,500-hp at temperatures above +30 Celsius, and a maximum takeoff power increased by 250-hp to 11,650-hp.

D-136-2 Applications


Support Aircraft Mi-26T2

D-136-2 Specifications

Power
Emergency Power: 12,500 hp (9,325 kW)
Max Power at TakeOff: 11,650 hp (8,691 kW)
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


OperatorsItems

Grand Total 521
 
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