Specifications
- Brand
- Mobil (ExxonMobil)
- Category
- Aviation turbine oils
- Manufacturer code
- 201550101050
- Availability
- On order
Manufacturer's description
Mobil Turbo 319A-2 is a fully synthetic lubricant developed to meet the performance requirements of Russian gas turbine aircraft engines that normally operate on mineral-oil-based lubricants. Formulated from a synthetic hydrocarbon combination of polyalphaolefin (PAO) and hindered ester base stock, fortified with a unique chemical additive system, it offers far superior thermal and oxidation stability than mineral-oil-based lubricants, resisting deterioration and deposit formation and offering the potential for extended oil drain intervals and less frequent maintenance. Closely controlled viscosity at -51°C and a -60°C pour point ensure good low-temperature fluidity for engine starting and lubrication, while the lubricant exhibits excellent bulk oil stability at temperatures up to 200°C with a significantly lower evaporation rate than mineral-oil-based products, helping minimise oil consumption. It also offers excellent resistance to foaming and is compatible with existing seal materials (Viton A, Buna N, silicone) and the metals used in gas turbine construction. Mobil Turbo 319A-2 is approved against Russian Central Institute of Aeronautical Motors (CIAM) specifications IMP-10, MS, 8P, MS-8RK, 36/1 Ku-A, VNII NP 50-1-4f and -4u, B3V and LZ-240, and also meets U.S. Military Specification MIL-L-6081C, as well as the essential performance requirements of MIL-L-7808K, Grade 3.
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 Aeronautical 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. Typical Characteristics 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 234 (453.2 Flash point, º C (ºF) ) 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
Performance & 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
Approved for
Complete documentation
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- TDS