TM333 2B2 /TM333 2M2 (ALH MK I II / CHEETAL)
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.