Brand
Mobil (ExxonMobil)
Type
Aviation turbine oils
Primary standard
MIL-PRF-23699-HTS
Manufacturer code
201550101010

Mobil Jet Oil 254

Synthetic ester oil for aircraft gas turbines, MIL-PRF-23699 HTS

Specifications

Manufacturer code
201550101010
Availability
On order

Manufacturer's description

Mobil Jet Oil 254 is a third-generation, extra-high-performance synthetic aircraft gas turbine lubricant formulated from a specially prepared hindered-ester base stock fortified with a unique chemical additive package. Compared with typical Type II lubricants, it reduces bulk oil oxidation by up to 50 percent and shows deposit control capability 50°F higher, while operating effectively between -40°C and 232°C. Its closely controlled low-temperature viscosity and pour point below -54°C ensure good fluidity for starting and lubrication down to -40°C, while extensive laboratory and in-flight testing confirm excellent bulk oil stability at temperatures up to 232°C with low evaporation loss. The synthetic base stock viscosity, rather than shear-prone VI additives, provides load-carrying ability, and the lubricant offers excellent resistance to foaming. Mobil Jet Oil 254 is recommended for turbo-jet, turbo-fan, turbo-prop and turbo-shaft (helicopter) gas turbine engines in commercial and military service, as well as industrial and marine gas turbine applications. It is approved against the High Thermal Stability (HTS) classification of MIL-PRF-23699 and carries builder approvals from engine and accessory manufacturers including Honeywell/Lycoming, Rolls-Royce/Allison, CFM International, General Electric, International Aero Engines, Pratt & Whitney, SNECMA, Hamilton Sundstrand and others (specific engine approval must be verified with the builder).

Applications

  • Mobil Jet Oil 254 is recommended for aircraft gas turbine engines of the turbo-jet, turbo-fan, turbo-prop, and turbo-shaft (helicopter) types used in commercial and military service. It is also suitable for aircraft-type gas turbine engines used in industrial or marine applications.Mobil Jet Oil 254 is approved against the High Thermal Stability (HTS) classification of U.S. Military Specification MIL-PRF-23699. It is also compatible with other synthetic gas turbine lubricants meeting MIL-PRF-23699. However, mixing with other products is not recommended because the blend would result in some loss of the superior performance characteristics of Mobil Jet Oil 254.Mobil Jet Oil 254 is completely compatible with all metals used in gas turbine construction, as well as with F Rubber (Viton A), H Rubber (Buna N), and other commonly used seal materials. Mobil Jet Oil 254 has the following builder approvals * Engines • Honeywell/Lycoming-Turbines • Rolls-Royce/Allison Engine Company • CFM International • General Electric Company • International Aero Engines • Pratt and Whitney Group • Pratt and Whitney, Canada • Rolls-Royce Limited • SNECMA • Honeywell/Garrett Turbine Engine Company Accessories • Honeywell-Auxiliary power units and air cycle machines • Hamilton Standard-Starters • Hamilton Sundstrand Corp.-APUs, constant-speed drives and integrated-drive generators * Specific engine or equipment approval must be verified with the builder

Performance & benefits

  • Chemically stable at high operating temperaturesReduces evaporation losses and lowers oil consumption
  • Excellent resistance to foaming Good low temperature fluidityMaintains film strength under rigorous operating conditions Permits start-up and ensures effective lubrication of critical components at temperatures as low as -40 °F

Standards & approvals

  • MIL-PRF-23699-HTS

Approved for

  • Allison
  • MIL

Typical characteristics

PropertyTypical valueMethod
Autogenous-ignition Temperature Test, deg.C, 30 CFR 35.20399
change in Kinematic viscosity, 72 h @ -40 C%-2.2ASTM D2532
Elastomer compatibility, AMS-3217/4 (72hrs @204C), % swell, FTMS 791-360420.8
Elastomer compatibility, AMS-3217/1(72hr @70C), % swell, FTMS 791-360420
Evaporation loss, 6.5 h, 204 C, mass%7.4ASTM D972(mod)
Evaporation loss, 6.5 hr @ 232 C, 5.5" Hg, mass %25.2ASTM D972(mod)
Fire point°C288ASTM D92
Flash point, Cleveland Open Cup°C254ASTM D92
Foam, Sequence I, Tendencyml0ASTM D892
Foam, Sequence II, Tendencyml10ASTM D892
Foam, Sequence III, Tendencyml0ASTM D892
Kinematic viscosity @ 100 Cmm2/s5.3ASTM D445
Kinematic viscosity @ 40 Cmm2/s26.4ASTM D445
Kinematic viscosity @ -40 Cmm2/s11500ASTM D445
Pour point°C-62ASTM D5950
Shear stability, %KV loss0.7ASTM D2603
Specific gravity 60 F / 60 F1.0044ASTM D1429
Total acid number, mgKOH/g, ARP 50880.08
Ryder Gear Load carrying, % vs ref., FTMS 791-6508114

Complete documentation

We email you the sheets listed below in a single archive. No account, no order required.

  • SDSEN
  • SDSRO
  • TDSEN

Where should the files go?

We send the archive to the address below. It is the only field we need — the rest only help us reach you if a sheet is missing.

What you get

    Str. Soporului, nr. 12, Cluj-NapocaContactAbout us
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