Aircraft-TypeGasTurbineLubricantProductDescriptionMobilJetOilIIisahighperformanceaircraft-typegasturbinelubricantformulatedwithacombinationofahighlystablesyntheticbasefluidandauniquechemicaladditivepackage.Thecombinationprovidesoutstandingthermalandoxidativestabilitytoresistdeteriorationanddepositformationinboththeliquidandvapourphases,aswellasexcellentresistancetofoaming.TheeffectiveoperatingrangeofMobilJetOilIIisbetween-40ºC(-40ºF)and204ºC(400ºF).MobilJetOilIIisengineeredforaircraftgasturbineenginesusedincommercialandmilitaryservicerequiringMIL-PRF-23699F-STDlevelperformance.Italsoisrecommendedforaircraft-typegasturbineenginesinindustrialormarineserviceapplicati***FeaturesandBenefitsMobilJetOilIIisformulatedtomeetthedemandingrequirementsofaircraft-typegasturbinesoperatingoverawiderangeofsevereoperatingconditi***.Theproducthasahighspecificheatinordertoensuregoodheattransferfromoil-cooledengineparts.Inextensivelaboratorytestingandin-flightperformance,MobilJetOilIIexhibitsexcellentbulkoilstabilityattemperaturesupto204ºC(400ºF).Theevaporationrateatthesetemperaturesislowenoughtopreventexcessivelossofvolume.Keyfeaturesandbenefitsinclude:FeaturesAdvantagesandPotentialBenefitsExcellentthermalandoxidationstabilityReducestheformationofcarbonandsludgedepositsMaintainsengineefficiencyandextendsenginelifeExcellentwearandcorrosionprotectionExtendsgearandbearinglifeReducesenginemaintenanceRetainsviscosityandfilmstrengthacrosswidetemperaturerangeProvideseffectivelubricationathighoperatingtemperaturesChemicallystableReducesevaporationlossesandlowersoilc***umptionLowpourpointEasesstart-upinlowambienttemperatureconditi***Applicati***MobilJetOilIIisrecommendedforaircraftgasturbineenginesoftheturbo-jet,turbo-fan,turbo-prop,andturbo-shaft(helicopter)typesincommercialandmilitaryservice.Itisalsorecommendedforaircraft-typegasturbineenginesusedinindustrialormarineapplicati***.MobilJetOilIIisapprovedagainsttheStandardPerformance(STD)classificationofU.S.MilitarySpecificationMIL-PRF-23699.ItisalsocompatiblewithothersyntheticgasturbinelubricantsmeetingMIL-PRF-23699.However,mixingwithotherproductsisnotrecommendedbecausetheblendwouldresultinsomelossoftheperformancecharacteristicsofMobilJetOilII.MobilJetOilIIiscompatiblewithallmetalsusedingasturbinec***truction,aswellaswithFRubber(VitonA),HRubber(BunaN),andsiliconesealmaterials.Specificati***andApprovalsMobilJetOilIIhasthefollowingbuilderapprovalsEngines-Honeywell/Lycoming-TurbineenginesX-Rolls-Royce/AllisonEngineCompanyX-CFMInternationalX-GeneralElectricCompanyX-IAEInternationalX-PrattandWhitneyGroupX-SNECMAX-PrattandWhitney,CanadaX-Rolls-RoyceLimitedX-Honeywell/Garrett-TurbineEngineCompanyX-TurbomecaXAccessories-Honeywell-AuxiliarypowerunitsandaircyclemachinesX-HamiltonStandard-StartersX-HamiltonSundstrandcorp.-APUs,C***tant-speeddrivesandintegrated-drivegeneratorsXMobilJetOilIIApprovedagainstMil-PRF-23699F-STDXPRI-QPL-AS5780/SPCXTypicalPropertiesViscositycSt@40ºC(102ºF)27.6cSt@100ºC(212ºF)5.1cSt@-40ºC(-40ºF)11,000%change@-40ºCafter72hours0.15PourPoint,ºC(ºF),ASTMD97-59(-74)FlashPoint,ºC(ºF),ASTMD92270(518)FirePoint,ºC(ºF)285(545)AutogenousIgnitionTemp,ºC(ºF)404(760)TAN(mgKOH/gsample)0.03Density@15ºC,kg/l,A***TD40521.0035EvaporationLoss,%6.5hr@204ºC,29.5"Hg3.06.5hr@232ºC,29.5"Hg10.96.5hr@232ºC,5.5"Hg33.7(Equalspressure@40,000Ft.altitude)Foam,mlSequenceI,24ºC8SequenceII,93.5ºC10SequenceIII,75ºC(after200Ftest)8FoamStability,after1minsettling,ml0RubberSwellFRubber,72hr@204ºC,%15.6HRubber,72hr@70ºC,%16.4SonicShearStability,KV@40ºC,change,%0.9RyderGear,***e.lb/in%HercolubeA2750,115HealthandSafetyBasedon***ailabletoxicologicalinformation,thisproductisnotexpectedtoproduceadverseeffectsonhealthwhenusedandhandledproperly.Informationonuseandhandling,aswellashealthandsafetyinformation,canbefoundintheMaterialSafetyDataSheet(MSDS)whichcanbeobtainedfromyourlocaldistributororviatheInternetonhttp:///lubes.)