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Mobil Turbo 319A-2

Type:  Lubricating oil

Implementation Standards:  MIL-L-7808K, Grade 3 / MIL-L-6081C

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Use:  aircraft gas turbine engines that normally operate on mineral-oil-based lubricants

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.

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.

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 C16.2
cSt at 100º C3.70
cSt at -40º C2917
cSt at -51º C12545
Flash point, º C (ºF)234 (453.2)
Pour point, º C (ºF)-60 (-76)
Specific Gravity0.852
TAN0.03
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, ml0
Rubber Swell, % 
NBR-H, 168 hr at 70ºC (158ºF)11.9
FKM, 72 hr at 175ºC (347ºF)3.0


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