DESCRIPTION
Turbonycoil 210 A is based on a blend of synthetic hydrocarbons and esters with a
viscosity of 3.7 cSt at 100°C. It contains a carefully selected package of anti-oxidant and
anti-wear additives. It offers a unique combination of high resistance to oxidati
APPLICATIONS
Turbonycoil 210 A has been designed for the lubrication of the latest generation of gas
turbines of Russian design.
It has been approved by CIAM (Central Institute of Aircraft engines) as an analog to the
Russian type IPM-10.
Turbonycoil 210 A is validated for use on the following engines/aircraft (military and civil)