Makila 1K2  
Initial Operational Capability (IOC): 1999
Total Production: ?
Origin: France
Corporations: Turbomeca
Parent System: Makila
Initial Operational Capability (IOC): 1978
Total Production: 2,266
Family Members: Makila 1A1, Makila 1A2, Makila 2A and Makila 2B
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Description: The Turbomeca Makila is a turboshaft family designed to power medium-size twin-engine helicopters such as Super Puma, Cougar, EC725, EC225 and Rooivalk.The engine rated at 1,700-shp to 2,400-shp has been designed based on five modules for a better maintainability with a time between overhaul (TBO) of 3,000 hours. More than 2,200 Makilas have been produced for 90 operators in 50 countries logging more than 8 million flight hours.

Basically, the Makila 1K2 engine is a modified Makila 1A2 turboshaft engine. This modification allows Makila 1K2 to be installed on South Africa's Rooivalk attack helicopter.

Makila 1K2 Applications

Combat Aircraft Rooivalk

Makila 1K2 Specifications

Number of Components: 5
Emergency Power: 2,109 shp (1,573 kW)
Max Continuous Power: 1,657 shp (1,236 kW)
Max Power at TakeOff: 1,845 shp (1,376 kW)
OEI 2 min: 1,967 shp (1,467 kW)
OEI Continuous: 1,904 shp (1,420 kW)
Time Between Overhaul: 3,000 hour
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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