Turbomeca Makila

The Turbomeca Makila is a family of French turboshaft engines for helicopter use, first run in 1976 and flown in 1977.

Typical power output is around 1,300 kW (1,700 hp). As of 2012, some 2,200 had been built.
 
Applications:
Puma HC Mk 2
Aérospatiale Super Puma
Denel Rooivalk
Eurocopter AS532 Cougar
Eurocopter EC225 Super Puma
Eurocopter EC725
IAR 330 SM

Variants:
Makila 1A
Makila 1A1
Makila 1A2
Makila 1A4
Makila 2A
Makila 2A1

Specifications:
Makila 2A
Type: Free-turbine turboshaft
Length: 1,836 mm (72 in)
Diameter: 498 mm (20 in)
Dry weight: 278,9 kg (including FADEC)
Compressor: 3-stage axial flow LP, single-stage centrifugal flow HP
Combustors: Annular
Turbine: 2-stage axial flow free turbine
Maximum power output: 1,801kW (2,415 shp)