TM333 2B2 / TM333 2M2 Turbo shaft engine powers ALH MK I, II & Cheetal Helicopter respectively. These engines are repaired / overhauled under license from M/s. Turbomeca, France.
- Modular construction with annular air intake, two stage axial compressor together with a centrifugal compressor driven by a single stage turbine.
- Annular reverse flow combustion chamber.
- Single stage free turbine with a through shaft driving a reduction gear unit.
- Full authority digital engine control. (FADEC).
- Simple installation and easy access for maintenance.
- Low specific fuel consumption.