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ExxonMobil Mobil Turbo 319A-2

Category Fluid , Lubricant , Polyalphaolefin (PAO)
Manufacturer
Trade Name
Port Shanghai port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF ExxonMobil Mobil Turbo 319A-2.pdf
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Material Notes:
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.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.
Physical Properties Metric English Comments
Specific Gravity 0.852 g/cc
0.852 g/cc
Viscosity Measure 2917 cSt

@Temperature -40.0 °C
2917 cSt

@Temperature -40.0 °F
Kinematic Viscosity
12545 cSt

@Temperature -51.0 °C
12545 cSt

@Temperature -59.8 °F
Kinematic Viscosity
Kinematic Viscosity at 40°C (104°F) 16.2 cSt
16.2 cSt
Kinematic Viscosity at 100°C (212°F) 3.7 cSt
3.7 cSt
Evaporation Loss 2.4 %
2.4 %
5 hr @ 175°C
Thermal Properties Metric English Comments
Pour Point -60.0 °C
-76.0 °F
Flash Point 234 °C
453 °F
Chemical Properties Metric English Comments
Total Acid Number 0.030
0.030
Descriptive Properties Value Comments
Foam Sequence I, ASTM D1135 30/0
Foam Stability, after 1 min settling, mL 0
Rubber Swell, % 11.9
H Rubber, 168 hr @ 70°C
3
F Rubber, 72 hr @ 175°C
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