MOBILJET254-CASE24 Mobil Jet 254, MIL-PRF-23699, (Case of 24 Quarts)

This third-generation, high thermal stability (HTS) oil was formulated to deliver exceptional high-temperature thermal stability and improved resistance to deterioration and deposit control versus Standard Type II oils. ExxonMobil Research and Engineering testing showed Mobil Jet Oil 254 lubricant offers excellent resistance to coking and deposit control, and provides exceptional oxidation and corrosion protection. Laboratory tests indicate Mobil Jet Oil 254 provides a 40 percent advantage in higher-temperature bulk oil stability vs. competitive HTS oils tested.

Overall, Mobil Jet Oil 254 delivers improved resistance to deterioration and deposit formation compared to standard Type II oils and can offer.

Reasons to trust Mobil Jet Oil 254

1. Offers exceptional resistance to carbon coking and deposit formation, helping operators reduce shop visits and maintenance costs
2. Helps operators reduce consumption costs due to its outstanding evaporative loss properties
3. Offers outstanding engine protection, even under extremely high operating temperatures
4. Provides excellent low-temperature fluidity in startups as low as -40 degrees Fahrenheit
   

   Features and Benefits

   Mobil Jet Oil 254 is formulated to meet the demanding requirements of latest technology  aircraft-type gas turbines operating over a wide range of severe operating conditions.  When compared to a typical Type II lubricant, Mobil Jet Oil 254 reduces bulk oil oxidation by up to 50 percent and shows deposit control capability 50 F higher.  These properties have been confirmed in various laboratory tests including; the Corrosion-Oxidation Stability Test,  Alcor Deposition Test, Vapor Phase Coker, Erdco High-Temperature Bearing Test, Ryder Gear and the Mobil Thin Film Oxidation Test.The closely controlled low-temperature viscosity of Mobil Jet Oil 254, along with its low pour point (below -54 ºC), ensure good low-temperature fluidity to permit starting and lubrication at temperatures as low as -40 ºC.  In extensive laboratory testing and in-flight experience, Mobil Jet Oil 254 also exhibits excellent bulk oil stability at temperatures up to 232 ºC (450 ºF) for extended periods.  The evaporation rate at these temperatures is low enough to prevent excessive loss of volume.  The load-carrying ability of Mobil Jet Oil 254 comes from its synthetic base stock viscosity and, therefore, is not subject to loss from viscosity index additive shear.  The lubricant has excellent resistance to foaming.Key features and benefits include:

    

   Features	Advantages and Potential Benefits
   Excellent thermal and oxidation stability	Reduces the formation of carbon and sludge deposits Maintains engine efficiency and extends engine life Reduces bulk oil oxidation by 50% and increases deposit control by 50 ºF
   Excellent wear and corrosion protection	Extends seal, gear and bearing life Reduces engine maintenance
   Viscosity and shear stability across wide temperature range	Provides effective lubrication at high operating temperatures
   Chemically stable at high operating temperatures	Reduces evaporation losses and lowers oil consumption
   Excellent resistance to foaming	Maintains film strength under rigorous operating conditions
   Good low temperature fluidity	Permits start-up and ensures effective lubrication of critical components at temperatures as low as -40 °F

    

   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

    

   Specifications and Approvals

   This product has the following approvals:

   MIL-PRF-23699-HTS

    

   Properties and Specifications

   Property
   Autogenous-ignition temperature test, deg.C, 30 CFR 35.20	399
   Change in Kinematic Viscosity, 72 h @ -40 C, %, ASTM D2532	-2.2
   Elastomer Compatibility, AMS-3217/4 (72hrs @204C), % swell, FTMS 791-3604	20.8
   Elastomer Compatibility,AMS-3217/1(72hr @70C), % swell, FTMS 791-3604	20
   Evaporation Loss, 6.5 h, 204 C, mass%, ASTM D972(mod)	7.4
   Evaporation Loss, 6.5 hr @ 232 C, 5.5″ Hg, mass %, ASTM D972(mod)	25.2
   Fire Point, °C, ASTM D92	288
   Flash Point, Cleveland Open Cup, °C, ASTM D92	254
   Foam, Sequence I, Tendency, ml, ASTM D892	0
   Foam, Sequence II, Tendency, ml, ASTM D892	10
   Foam, Sequence III, Tendency, ml, ASTM D892	0
   Kinematic Viscosity @ 100 C, mm2/s, ASTM D445	5.3
   Kinematic Viscosity @ 40 C, mm2/s, ASTM D445	26.4
   Kinematic Viscosity @ -40 C, mm2/s, ASTM D445	11500
   Pour Point, °C, ASTM D5950	-62
   Shear Stability, %KV loss, ASTM D2603	0.7
   Specific Gravity 60 F / 60 F, ASTM D1429	1.0044
   Total Acid Number, mgKOH/g, ARP 5088	0.08
   Ryder Gear Load Carrying, % vs ref., FTMS 791-6508	114