Description
Mobil Turbo 319A-2 is a fully synthetic lubricant developed to meet the
performance requirements of Russian gas turbine aircraft engines which operate
on mineral-oil-based lubricants. Formulated from a synthetic hydrocarbon
combination of polyalphaolefin (PAO) and hindered ester based stock, Mobil
Turbo 319A-2 is fortified with a unique chemical additive system. The
resulting product has far superior thermal and oxidation stability than
mineral-oil-based lubricants. The ability of Mobil Turbo 319A-2 to resist
deterioration and deposit formation allows the potential for extended oil
drain intervals and less frequent maintenance.
The closely
controlled viscosity of Mobil Turbo 319A-2 at -51º C, along with a -60ºC pour
point, ensure good low-temperature fluidity, permitting engine starting and
lubrication at low temperatures. Mobil Turbo 319A-2 exhibits excellent bulk
oil stability at temperatures up to 200º C (392º F). The evaporation rate of
Mobil Turbo 319A-2 at high temperatures is significantly lower than
mineral-oil-based products, and helps minimize oil consumption. The lubricant
has excellent resistance to foaming.
Mobil Turbo 319A-2 is
compatible with existing seal materials, including F Rubber (Viton A), H
Rubber (Buna N), and silicone, as well as 11 metals used in gas turbine
construction.
Features and Benefits
Mobil Turbo 319A-2 offers the following advantages and benefits:
- Low evaporation loss and oil consumption
- Reduced sludge and carbon deposits
- Improved bulk oil oxidation stability and extended oil drain intervals
- Compatible with existing seal materials
- Reduced engine maintenance, including potential for extended drain intervals
Applications
Mobil Turbo 319A-2 is recommended for aircraft gas turbine engines that
normally operate on mineral-oil-based lubricants, as well as engines approved
to operate on oils meeting the specifications listed below.
Mobil Turbo 319A-2 is approved against the following specification of the
Russian Central Institute of Aeronatutical Motors (CIAM):
- IMP-10
- MS, 8P, MS-8RK
- 36/1 Ku-A
- VNII NP 50-1-4f and -4u
- B3V and LZ-240
- Mobil Turbo 319A-2 also meets U.S. Military Specification MIL-L-6081C, as well as the essential performance requirements of U.S. MIL-L-7808K, Grade 3.
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Typical Characteristics

Mobil Turbo 319A-2
| 
|
| Physical properties are listed in the table below. Values shown are typical and may vary slightly. | |
| Viscosity | |
| cSt at 40º C | 16.2 |
| cSt at 100º C | 3.70 |
| cSt at -40º C | 2917 |
| cSt at -51º C | 12545 |
| Flash point, º C (ºF) | 234 (453.2) |
| Pour point, º C (ºF) | -60 (-76) |
| Specific Gravity | 0.852 |
| TAN | 0.03 |
| Evaporation Loss, % | 0.999 |
| 5 hr at 175 ºC (347ºF) | 2.4 |
| Foam, ml | |
| Sequence 1, 24ºC (75ºF) | 30 |
| Foam Stability, after 1 min settling, ml | 0 |
| Rubber Swell, % | |
| NBR-H, 168 hr at 70ºC (158ºF) | 11.9 |
| FKM, 72 hr at 175ºC (347ºF) | 3.0 |
Health and Safety
Based on available toxicological information, this product is not expected to
produce adverse effects on health when used and handled properly. Information
on use and handling, as well as health and safety information, can be found in
the Material Safety Data Sheet (MSDS) which can be obtained from your local
distributor or via the Internet on http://www.exxonmobil.com/lubes.
The ExxonMobil logotype, Mobil and Mobil Turbo 319A are trademarks of Exxon Mobil Corporation, or one of its subsidiaries. PDSAV-11
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