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TM333 2B2  
Initial Operational Capability (IOC): December 2001
Total Production: 300
Also Known As: TM333 2M2 and TM333-2B2
Origin: France
Corporations: Turbomeca
Parent System: TM333
Initial Operational Capability (IOC): December 2001
Total Production: 300
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Description: The Turbomeca TM333 engine is a modular turboshaft designed to power the Hindustan Aeronautics Limited (HAL) Advanced Light Helicopter (ALH) Dhruv multipurpose twin-engine helicopter. The engine is rated at 1,100-shp and is fitted with an Electronic Engine Control Unit (EECU). It was certified in December 2001. As of early 2011, more than 300 TM333 engines have been produced in support of the ALH program.

The TM333 2B2 engine was selected to power India's Dhruv medium-size, twin-engine, multipurpose helicopter weighing five-to-six tons. The TM333 2M2 is intended to power single engine helicopters such as Chetan and Cheetal which are modernized versions of the Alouette III and Lama aircraft respectively.

TM333 2B2 Applications

Combat Aircraft Rudra Support Aircraft Dhruv

TM333 2B2 Specifications

RPM: 6,000
Height: 745 millimeter (29.3 inch)
Length: 1,045 millimeter (41 inch)
Width: 493 millimeter (19.4 inch)
Emergency Power: 1,219 shp (909 kW)
Max Continuous Power: 986 shp (736 kW)
Max Power at TakeOff: 1,105 shp (824 kW)
OEI 2 min: 1,126 shp (840 kW)
OEI Continuous: 1,081 shp (806 kW)
Time Between Overhaul: 2,000 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)

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