AC 33-2B - Aircraft Engine Type Certification Handbook
uU.S.Departmentof TransportationFederal AviationAdministrationCircularFAR GUIDANCE MATERIALSubject:AIRCRAFT ENGINE TYPECERTIFICATION HANDBOOKDate: 06/30/93Initiated by:ANE-110AC No:change:33-28circular(AC) provides methods1.PURPOSE. This advisoryacceptableto the Administratorfor showing compliance with thetype certificationrequirementsof aircraftengines in Part 33,inclusivethrough amendment 12, of the Federal AviationRegulations(FAR).The procedures and guidance materialprovidedseeking issuance of a typein this AC may be used by an applicantcertificate,an amended type certificate,or a supplementaltypecertificatefor the initialapproval of a new type design, or achange in the type design.Considerationwillbe given to anyother method of compliance the applicantelects to present.Thisinformationis not in itselfmandatory,but serves as a guide toengine manufacturers,engine modifiers,and Federal AviationAdministration(FAA) engine type certificationengineers.Individualsshould be guided by the intentof the methods providedin this AC.2. CANCELLATION. ThisEngine Type Certificationrevisionsupersedes AC 33-2A, "AircraftHandbook,tt dated June 5, 1972.3. RELATED FAR SECTIONS.45.FAR Parts21, 23, 25, 27,29, 33, and4.RELATED READING MATERIAL. FAA Order 8100.5, d October 1, 1982; andFAA Order 8110.4, "Type Certification,"dated December 28, 1967(Consolidatedwith Changes 1 through 23, June 1985).5.BACKGROUND.AC 33-2A, dated June 5 1972, was publishedas thellAir%aftEngine Type CertificAtionHandbook."The materialthereinprincipallyaddressed guidance on the proceduralaspectsof Part 21, but offeredvery littleguidance for Part 33.However, the last sentence of the l@PURPOSEIVparagraph did state,'IThe remainingchapters of the handbook pertainingto the designand testingof turbineand reciprocatingengines willbe issued asthey become available.n-b.This revisionupdates and presents the existinginformationwithinChapter 2, and incorporates,withinproceduralChapter 3,
AC 33-2B06/30/93engine type certificationrules and guidance materialwhich hassince been developed.The appendixes provide turbineandreciprocatingengine model descriptions,an index of guidancematerialand references,and a glossaryof acronyms andJA’C;;’f. SAIN-c1-pManager, EngineAircraftand PropellerDirectorateCertificationService-ii
AC 33-2B06/30/93CONTENTSPaqeParaqraphCHAPTER 1.INTRODUCTION1General12Guidance1CHAPTER 2.GENERAL TYPE PTER 3.SECTIONof hangesinand MaterialsType21Design21PlateTYPE CERTIFICATION1.3Engines23GUIDANCE MATERIALSUBPART sInstructions(Amendment17Section33.5,and OperatingInstructionthe llingiii
AC gsRatingsofSUBPART B--DESIGNEnginePower30andAND CONSTRUCTION;34GENERAL20Section33.14,Cycle 33.37,Ignition32Section33.39,LubricationSUBPART d Induction333743AND PreventionSECTION 3.SUBPART C--DESIGNAIRCRAFT ENGINESivand Operating52SystemRECIPROCATING52AIRCRAFT53Test53
-AC eneral55TestsComponent60Tests61Down InspectionSUBPART E--DESIGNSECTION 5.AIRCRAFT ENGINESConductofBlockAND on33.63,Vibration44Section33.65,Surgeand ustAugmenterSUBPART Thrust71Systems71Response7273Ingestion80ENGINES81
AC eUnit(APU) 8Inspection99Containmentand gAPPENDIX3.Index of erAPPENDIX92DescriptionMaterialand Abbreviationsand
AC 33-2B06/30/93CHAPTER 1.wINTRODUCTIONThis advisorycircular(AC) providesproceduraland1.GENERAL.guidancematerialfor the type certification(TC) of aircraftengines.The AC coverscertainsectionsof Parts21 and 33 ofSubchapterC, Chapter1, Title14, of the Code of FederalThis AC is consideredto be a livingdocument.Regulations(CFR).be amended on an as-neededbasisto maintainAs such, it willcurrency,such as withthe issuanceof Part 33 ruleschanges,orthe developmentof substantivenew guidancematerial.2.GUIDANCE.The TC guidancepresentedis referredto thespecificregulatoryrequirementto which it applies.As aconvenienceto the user,the FAR Part 33 regulatoryrequirements,presentedin Chapter3, are reprintedhereinto providea cohesivesingle-sourcebook for enginetype certification;i.e.,procedures,rules,and associatedguidance.Followingeach Part33 section,under "Guidance,"is a briefstatementof the intent,followedby a listingof documentsincorporatedas pertinentguidancematerial;and a second listingof relatedbibliographicmaterial,followedby specificdiscussions,where applicable.-Chap 1Par 11 (and2)
AC 33-2B06/30/93CHAPTER 2.GENERAL TYPE CERTIFICATIONPROCEDURESThis chapterprovidesinformationand guidance3.PURPOSE.materialon the certificationproceduresof FAR Part 21 whichbe employedfor enginetype certificationprojects.TYPE CERTIFICATE.4.Section21.41.The typecertificateis5.TYPE CERTIFICATIONSections21.13,21.15,Part 33).OF AIRCRAFT enceFAR21.27,21.29,and FARa.EnqinesComplyinqwithParts21 and 33.Enginestestedand approvedto the airworthinessstandardsof FAR Part 33 areeligibleto receivea type certificate.Section21.13 coversapplicanteligibility;Section21.15 coversapplicationfor typecertificate;Section21.16 coversthe establishmentof specialconditions;and Section21.17 coversdesignationof the applicableversionof Part33 which shouldbe met.forb.ImporteligibilityEnqines.for typeC.Militarybe accomplishedis prescribedinenginesmay alsocertificated,in21.27(c)and (e).Section21.29certificationprescribesof importthe conditionsengines.SurplusEnqines.Enginetype certificationmayfor militarysurplusenginesin the same manner asSection21.21 for otherengines,but thesebe made eligiblefor use withoutbeing typeaccordancewiththe provisionsof Sections(1)Under Sections21.27(c)and (e), militarysurplusenginesmay be approvedfor use on militarysurplusaircraft,ifit is shown on the basisof previousmilitaryqualificationsacceptanceand servicerecord,thatthe engineprovidessubstantiallythe same levelof airworthinessas would be providedif the engine were type certificatedunder Part 33, withappropriatespecialconditionsand laterrequirementsapplied.(2)The ation,and identificationof the enginebe listedon the ata sheet.The followingenginetechnicalhelpfulin identifyingenginelimitsand showingcomplianceFAR Section21.27(c):detailsoffor taryshoulddata arewithservicerecordsummary,includingchanges requiredfor the ications.Chap 2Par33
AC 33-2B06/30/93(iii)informationfor theand are currentlyrequiredto meet the specifictestrequirementsof Section33.49(d),Sections29.923 and 27.927,or Sections29.923 and 29.927,as appropriate.(1)Beforethisspecialendurancetestwas made effectiveon May 15, 1953, in the CivilAir Regulations(CAR) Part13, itbecame evidentfrom serviceexperiencethatsome enginesoperatedin helicopterswere hazardousand unreliable,because of thecharacteristicallyhigh steadyenginespeeds and powers at whichoverspeedswere oftenencounteredin helicopters.(2)To providegood reliabilityin the case ofreciprocatingengineswhich were not qualifiedunder Section33.49(d),or have not been shown to have equivalentcapabilities,it is suggestedthatthey be derated.The followingmethod ofderatingis suggested,as it resultsin engineratingswhich arecomparablyqualified,as if the helicopterenginetesthad beenthe basisfor enginequalification:ratingis notoriginal(i)Limitsea levelenginesto a maximum power(at fullthrottle),correspondingto an enginespeed thatmore than 90 percentof the enginespeed at which themaximum full-throttlepower ratingwas established.(ii)Limitaltitudeenginesto a maximum powerratingof not more than 95 percentof the originalmaximum powerrating,at an enginespeed thatis not more than 90 percentof theenginespeed at which the originalmaximum power ratingwasestablished.6.TYPE CERTIFICATEDATA.(ReferenceFAR Sections21.1921.41).Section21.19 providesthatsome typesof designto enginesrequirea new applicationfor a type certificate.Engine models which areleve?;and designcharacteristics,same type certificate.oftheareandchangessame generalseries,powerusuallyapprovedunder theb.A new type certificateis requiredwhen the proposedchangesin designor limitationsare so extensivethatasubstantiallycompleteinvestigationof compliancewithapplicableregulationsis required,or when the proposedchange is in theprincipleof operation.C.lieu4ofThe use of enginemodelnew model designations,number prefixesis suggestedtoor suffixes,incover many changesChap 2Par 5
--AC 33-2B06/30/93in engineswhich are importantenough to warrantwhich do not involveconsiderationsnecessitatingdesignationbe assigned.d.followingNew model designationsinstances:areaffected(1)When interchangeabilitysignificantlyby changesusuallyofrecognition,butthata new modelassignedinthein a given model aircraftisengine weightor performance.propellervibrationWhen propellermounting,useprovisionsare changed so as to precludepropellerson allenginesof the same model.(2)or controltypesof(3)When, as a resultof designor thrustratingsare changed a significantin excessof theof 20 percentor more),outputmeasurement.model(4)When specialratingsbecause of incorporationofofdamping,certainchanges,the horsepoweramount (on the orderacceptedtoleranceofare grantednew designan existingfeatures.engine(5)When a significantchange is made in the mountingdesignof cowlingor bafflescharacteristicsof an engine,integralwiththe engine,exhaustportlocations,oilsupplysump,or controlcharacteristics.accessories,.-(6)When a designchange resultsinheat rejectionin vibrationcharacteristics,coolant,or oil(7)When specialapplications,for example,resultin uniqueuse, or extendedrange enance(ReferenceFAR Section7.TYPE CERTIFICATEDATA SHEET (TCDS).Itincludesthe21.41)The TCDS is partof the type certificate.type certificateholder,model designation,ratings,limitations,This sheet is preparedby the FAAand certificationbasis.See FAAprojectengineer,withassistancefrom the applicant.fordetailsonpreparationsforOrder 8110.4,Paragraph35,printing.There is no FAA form providedfor TCDSs because of thevariationsin the requireddata associatedwiththe variousproducts.The veto uniformhandlingof the enginedata sheet,withreferenceto the desireddescriptivedata contentand generalarrangementto be consideredin the preparationof thissheet.-General.Applicabledetails,as prescribedin followinga.constitutethe officialstatusof the engine(s)andparagraphs,serve as a guidefor identification,use, and installationofThe formalarrangementof data,explanatoryenginesin aircraft.Chap 2Par65
06/30/93AC 33-2Bnotes,and extentof detailprovidedshouldconform,in general,to thatshown for the most recentlycertificatedcomparabletypesof engines.Extensivedetailsof engineeringinstallationdataare not desirableand thisdata may be merelyreferenced.However,specificdata shouldbe indicated,if feasible.Theassistanceof the applicantis desirablein formulatingandassuringthe accuracyof the data sheets.Standardizationof datasheet formatis desirablewheneverpossible,and specificallyforthe same generictype enginesconsistentwiththe followingrecommendations.The projectengineershouldhave the draftdatasheet completedby the time the type certificateis issued.b.DetailedDescription.(1)Headinq- Numberinq.The data sheet number willappear in the upper right-handcornerof page 1.This number willbe the same as the type certificatenumber.When the data sheetis revised,the revisionnumber willbe shown as a suffix.Thename of the type certificateholder,in the approvedmodelslistedinalphabetical,or numerical,orderfor referenceconvenience.Theissuedate willcompletethisgroup.The above informationwillbe enclosedin a box to set it off.(2)Title.The titleof the document(Type CertificateData Sheet No.) willappear in the centerof the page, afterthe headingbox.The titlewillincludethe exact,unmodified,type certificatenumber,as shown on the type certificate.(3)Sample Preamble.Enginesof models describedherethatconformwiththisdata sheet(which is a part of TypeCertificateNo.) and otherapproveddata on filewiththeFAA, meet the minimum standardsfor use in certificatedaircraft,in accordancewithpertinentaircraftdata sheetsand applicableportionsof the FAR, providedthey are installed,operated,andmaintained;as prescribedby the FAA approvedmanufacturer'smanualsand otherFAA approvedinstructions.(4)Type Certificateaddressof the type lderInsertthe exactname andas shown on the typeSection).(i)Model Desiqnation.Show model designationsone or more columns,as necessaryto exhibitratings,limits,otherparametersfor each of the models.Referenceto recentlyissuedTCDSs willillustraterepresentativeways of groupingenginesin columns,and ways of accomplishingthe followinginstructions.Chap 2Par7inor
AC emodelsFor example:and processes.intermsofmajor(A)Reciprocating- number of cylinders,cylinderarrangementand coolingmethod,reductiongear ratio,and supercharging(e.g.,9RA, 6HOA, IGO, TSIO);fuelinjection,and urbofan- number of compressorsingleor multiplespool,radialor axial(e.g.,12-stageaxialflow Turboprop,turbine,turboshaft- same as inif appropriate.Forreciprocatingengines:- Maximum continuoushorsepower,r.p.m.,-- Rated pressurealtitudeft.----- Sea levelpressurealtitudeft.- Takeoff(5 minutes)horsepower,r.p.m.,-- Rated pressurealtitudeft.----- Sea levelpressurealtitudeft.- Other,impelleralternateif applicable,gear ratios,fuels).(B)turbojet- Maximumr.p.m.atcontinuoussea level.static- Takeoffatr.p.m.(5 minutes)sea level.ifstaticin.Hg at:S.L.--in.Hg at:S.L.---both lowinjection,and highorand plicable,(e.g.,with water-alcoholreheat,reversethrust,or alternate(C)Chap 2Par7(e.g.,withanti-detonatorFor- edmaximum powerat controlsetting,rotationalspeed,pressurealtitude,or otherconditionsas applicablefor thetemperature,generictype engines:(A)NoteitemForturboshaftand turbopropratings).engines(See
06/30/93AC 33-2B- Turboshaft----EngineRatingsMaximum continuous--- Takeoff(5 minutes)--- --30-MinuteOEI (30 minutes)--- Outputshafthorsepower,SHP--- Outputshaftspeed,r.p.m.--2-l/2-Minute--- Output--- Output--ContinuousOEI--- Outputshaft--- Outputshaft- TurbopropEngineminutes)OEI -Maximum continuous--- Outputshafthorsepower,SHP--- Outputshaftspeed,r.p.m.--- Equivalentshafthorsepower,ESHP--Jet r,ESHPJet thrust,lb.-- Other,if speed;and fan(e.g.,Gear Ratio.speed to uelcontrol,power tspeedspeed.and model ofand overspeedFuel.(A)Fuel- octane,grade,ortype,asapplicable.8Chap 2Par7togas
AC tor,or otherapplicable)fuelcontrolrelevant-- manufacturerand model.engineinlet)(D) Fuel- mesh rspecification.dry,oilor wet)- engineinand l)magnetostypeandspecification.(ix)box- models.exciters- s(C)Spark plugs,(If D)TurbosuperchargerLengthignitionand ignitiona note).- Compression.BorePrincipalorBTC).igniters,put into(A)(A)Chap 2Par7only).and stroke(reciprocating).(reciprocating).ratio- model.Dimensions.(in.)(reciprocating).-supply
AC (Dry)Lb.(NoteofGravity.any rcenterShaft.Dampers.lineTypeNumber,ininches.and size.order,location,and type.tomodelgroup,(xvi)Note List.Listingof note numberslistedunder data column for rtificationofsymbols."same"doesapplicableas precedingnotmodel."apply."Basis.(A)FAR (CAR), SpecialConditions,as appropriate,effectivitycoveringtypeof engine.(B)Enginemodeland onbasis.or ificate(6)BasicData.(Notes Section).Variationsare sonumerousin enginetype,and in conditionsrelativeto similarcloseuniformityin the use of notes for allenginestypes r thatappearsimpractical.Uniformityfor uniformity'ssake mightwellimpairthe accuratepresentationof technicalinformation.Thefirstsix notes are assignedto common conditionsor parametersand for uniformityshouldbe used solelyfor these subjects.Theremainingnotes and contentsmay be selectedaccordingto the data10Chap 2Par 7-
AC 33-2B06/30/93to be presented.The followingnotes are presentedaccordingly.(i)examplesCommon NOTE 1.Engineratingsare based on ineperformance,Forexample:type certificateholder.- Staticsea29.92"Hg).levelstandard- No customerbleed,power extraction.no duct- Exhaustconfigurationtype certificateholder).NOTE 2.limits.MaximumpermissibleMaximum CylinderHeadRecip.(Type Thermocouple)Turbineexhaustor turbineinletlosses,(asspecifiedtemperaturesno externalby theengineor temperatureOilCylinderBase5-m.)(59 OF ('C.)'F.('C.)'F.('C.)Maximum transientaccel.( ) F.('C.)'F.('C.)'F.('C.)OtherlimitsChap sbY atTakeoff(5 minutes)Maximumdaytransient( ) sec.temperatureas applicableNOTE 3.Shaft(orFan)NOTE 4.ShafttorqueNOTE 5.Fueland Oilspeedlimitspressurelimits.(orEPR thrustlimits).limits.11
06/30/93AC 33-2BNOTE 6.Accessorydriveor mountingAct.DriveEngineRJ 123ModelsRJC123RotatnFacingDr PadSpeedRatioto tc.-:lcc-:lCetc.etc.etc.- Standard11* * II - Optional"C " - Clockwise"CC " - Counterclockwise11 II means "does not apply"I,provisions.source" # " - Drive" P " - Pneumatic"GP " - Gas Producerrotor"PT " - Power TurbinerotorII--II means "same aspreviousmodel"11NOTE 7.Model descriptionand specialcharacteristics.RJ123- BasicRJC123List- SimilarmajorModelto- similarities,- es.NOTE 8.The followingaccessoriesare providedas partthe engine(or are optional)and comply withthe craft.Compliancefindingsneed to be determined,or delegated,by the appropriateFAA Aircraft(or Engine)CertificationOffice(ACO/ECO).(ii)Uncommon NotesPeculiartoReciorocatinqEngines.NOTE 9.12Thrust- tractororpusher.Chap 2Par 7of
AC 33-2B06/30/93NOTE 10.information.HorizontalorNOTE 11.Centerofbody of data sheet).NOTE 12.NOTE r- cturersbulletinsand instructionsmattersof specialinterest.NOTE 14.SpecialNOTE 15.MilitarymodelsNOTE 16.Specialequipment.NOTE 17.ApprovedNOTE 18.Other(iii)installationratings.note.propellers- models.applicablenotes.Uncommon NotesPeculiartoAllTurbineEnsines.NOTE 9.alternate.-Rotationalratings,velocitiesetc.NOTE 18.BleedairNOTE 11.AlternateNOTE 12.FuelNOTE 13.Anti-icing,NOTE 14.Poweratstandardextraction.fuelor nt,non-standardNOTE 16.Operationalspeciallimits.EngineNOTE tions.NOTE 15.Rotor diskintegrityand rotor(where specialprovisionsapply).NOTE 17.and overspeed,bladesettings,containmentand othersystem.injection.NOTE 19.Other applicablenotes for specialequipment,relatingto specificor uniqueengineinstallationrequirements,such as ERF protection,thrustreversers,Chap 2Par 713or
06/30/93AC 33-2Bcriticalitylevelof softwarefor s,emissionsstandards,extendedrange operations,etc.(iv)NotesPeculiarNOTE 20.ApprovedNOTE 21.EnginePropellersOtherTurboprooEnaines.- Models(whenavailable).- Controls.NOTE 22.Equivalentlb./2.5 SHP.(v)toNotesshafthorsepowerPeculiarto- JetSpecialthrust,ConditionsAssiqned.(vi)TCDS (For 21.31,and 33.5).When an enginemodel hasbecome obsolete;e.g.,if the type certificateholderdoes notintendto manufactureit,or any of itscomponentparts;approvalunder the type certificatemay be canceledupon request.Aftercancellation,it is no longernecessaryfor the [former]typecertificateholderto maintainup-to-datetype designand typecertificatedata.The TCDS of the engine willbe revisedtoreflectthe change in certificationstatusand, when allmodelslistedunder one type certificatehave been canceled,the datasheet willbe transferredto a combinedlistingof obsoleteengines.The operationof obsoleteenginesstillin serviceiseligibleto be continuedunder the statusof the approvalineffectat the time the certificatewas canceled.If reinstatementof the type certificateis desiredby the formertype certificateholderfor the purposeof resumingactiveengineproduction,a newapplicationfor type certificate,to be based on currentFAR, isneeded.8.DATA REOUIRED.(ReferenceFAR Sections21.31,21.41,and FAR Part 33).21.15,21.21,21.29,FAA Form 8110-12."Applicationfor Type Certificate"(OMB :4-R0078)is the form referredto in Section21.15(a).shouldbe submittedto the FAA AircraftCertificationOfficein which the applicantis geographically(AC01 r of the data are needed tomake the initialevaluationof conformitywiththe specificdesignrequirementsand the establishmentof detailedqualificationtestingto be prescribed,in accordancewith FAR Part 33.Thedata most usefulfor these purposesincludea ta,which are requiredunder Sections21.21(b)and mation.To facilitatethisevaluationof14Chap 2Par 7
AC 33-2B06/30/93the preliminaryenginedesignfeatures,along withthe applicationfor a typepreliminarydata are suggested:data may be submittedThe followingcertificate.(1)A preliminarymodel description,specification,containingat leastsufficientinformationtoequivalent,the establishmentof the basisfor ews and cross-sectionsand typicaldetailedofof significantdevelopmenthistory,(3) A reviewemphasizingthe extentof developmentexperiencewiththe engine,withparticularemphasison uniqueor complexfeatures,or theircombinationsnot used up to now in aircraftengines.for substantiatingcompliancewiththe(4) Proposalsrequirementsof FAR Part 33 for U.S. applicants'enginesandby means of technicalanalysesSection21.29 for importengines,or testing.Test proposalsare desiredappreciablybeforetheproposedstartingdate of the test,in sufficientdetailto serveas a guidefor testing,whereuponthey may be incorporatedin theReference[Handbook]FAAType InspectionAuthorization(TIA).Order 8110.4 for more detailedinformationon TIAs,includingtestconformityinspectionand schedulearticlepre- and post-testrequirements.C.FinalType Desiqn and Type CertificateData for U.S.ManufacturedEnqines.Acceptabletype designand typecertificateddata,testreports,and computationsdata,requiredunder Section21.21(b),cover the ntesting.Acceptabledata are describedas qnData.(ReferenceSection(i)Enqine Model Description.shouldprovidedata and informationto replacethe preliminaryverified,Appendixes1 and 2).21.31).The finalmodelthatis allmodel description.(ii)Enqine PartsDrawinqs,Material,and ProcessSpecifications.Acceptabledata willshow the configurationofthe type designthatsuccessfullycompliedwiththe requiredtestsand inspections.A numericallyarrangeddrawinglistthatshowsthe latestdesignchange identificationis ccompanythe drawings.to identifyand completelydescribethe designfeatures;supplyand processesnecessarytoinformationon dimensions,materials,definethe structuralstrengthof the product;partand serialnumber locations;and any otherdata necessaryto allow,byChap 2Par815
AC rminationsame type.(2)Type Certificateand i)Test Reportsand Computations.Test reportsto substantiatecompliancewith the applicableof Part 33.A testreportshouldcover,but notthe following:andbe(A)Test equipment.A completedescriptionwith photographs,or referenceto a previousreportin which thesame equipmentwas used; the manner of enginemountingin the testequipment;and the calibrationstatusof instruments.(B)Test procedure.The name of the test,of the testsequence,or the FAR; the chronologicallog oftesting;delaysin testsand theircauses;stopsfor minorcorrectionsand servicingengine;and time requiredfor starts.part(C)Test data.Graphs showingvariationsinoperatingconditionsduringthe endurancetest;log sheetsandcalibrationcurvesfor calibrationtestdata;method used incorrectingtestdata to 45 and 33.85(a))and substantiationof any correctionfactorsused.NOTE:scalesAll data shouldwhich are easilybe legible,accurate,read and interpolated.and when eof partsbeforeassemblyand afterdisassembly,priorto cleaningfor eand after-testtablesof dimensionsof major partsof the enginethatare likelyto incurwear, or change of dimension.Includephotographsand descriptionsof excessivelyworn parts.Discussany unusualwear,burning,overheating,partfailureor impendingfailure,and occurrenceof heavy depositson parts.Indicatetheconditionof mating,sealing,and frictionsurfaces;e.g.,airoilseals,each ouplings,etc.Indicatethe resultsof visual,X-ray,magnetic,fluorescentparticle,or otherinspectionsof majorparts.(E)Laboratoryanalyses.Analysesand grades of fuel,lubricants,and hydraulicfluidstest.Identifythe specificationto which the fluidsDescribethe conditionof the lubricantand hydraulicthe test.16of theused intypestheconform.fluidsChap 2Par 8after
AC ctionThe manual(s)cover informationfor installing,operating,33.5).Installationandand continuedairworthinessof the engine.operatingmanual data thathave been substantiated,FAA approved,and are specificallyrequiredfor engineapprov
AC 33-2B 06/30/93 Paraqraph Paqe . 56 Section 33.83, Vibration Test 81 Unbalance Tests Unit (APU) Mode 57 Section 33.85, Calibration Tests 83 58 Section 33.87, Endurance Test 84 59 Section 33.88, Engine Overtemperature Test 92 60 Section 33.89, Operation Test 93 61 Section 33.90, Initial Maintenance Inspection 95 62 Section 33.91, Engine Component Tests 96
1.Engine Oil SABA 13 1.Engine Oil 8000 14 1.Engine Oil 6000 15 1.Engine Oil 3000 16 1.Engine Oil Alvand 17 1.Engine Oil Motor Cycle Engine Oil M-150 18 1.Engine Oil M-100 19 1.Engine Oil Gas Engine Oil CNG-BUS 20 1.Engine Oil G.I.C.X.LA 21 1.Engine Oil G.I.C.X. 22 1.Engine Oil Diesel Engine Oil Power 23 1.Engine Oil Top Engine 24
The Aircraft Engine Design Project Fundamentals of Engine Cycles Ken Gould Spring 2009 Phil Weed 1. g GE Aviation Technical History GE Aircraft Engines U.S. jet engine U.S. turboprop engine Vibl tt iVariable stator engine Mach 2 fighter engine Mach 3 bomber engine High bypass engine
- B734 aircraft model added - B735 aircraft model added - E145 aircraft model added - B737 aircraft model added - AT45 aircraft model added - B762 aircraft model added - B743 aircraft model added - Removal of several existing OPF and APF files due to the change of ICAO aircraft designators according to RD3: A330, A340, BA46, DC9, MD80
F/A-18E/F Super Hornet Fighter 1,253.1 million (14 aircraft) 1,996.4 million (24 aircraft) V-22 Osprey Tiltrotor Aircraft 961.8 million (6 aircraft) 1,280.1 million (7 aircraft) C-130J Hercules Military Transport Aircraft 886.1 million (9 aircraft) 1,571.9 millio
A holding pattern is a shift by T This is the set in which we want to schedule aircraft. We seek one arrival time for each aircraft in each of the colored sets. aircraft 1 aircraft 2 aircraft 3 feasible arrival times aircraft aircraft 4 a1 b1 a2 b2 a3 b3 a4 b4 A holding pattern can be expressed as a MILP
Aircraft Type Falcon 50EX Year of Manufacture 2004 Year of Delivery 2004 Airframe Total Time 4376 Hrs Airframe Total Cycles 3209 Manufacturer Honeywell Engine Type TFE731-40-1C Engine Program MSP Engine #1 TSN 4376 Hrs Engine #1 CSN 3209 Engine #2 TSN 4219 Hrs Engine #2 CSN 3150 Engine #3 TSN 4376 Hrs Engine #3 CSN 3209 Manufacturer Honeywell
A forecast of based aircraft was used to assess the demand for facilities used by general aviation aircraft. This includes items such as hangars and aircraft ramp. The TAF estimates that future based aircraft will grow to 430 by 2036. The majority of general aviation aircraft are small, single-engine aircraft with smaller percentages of multi-
Abandoned aircraft: Refers to the aircraft permanently parked without a storage maintenance program. In some cases, the aircraft has been deregistered and it may be impossible to identify the owner. Aircraft owner: In this manual, this term includes the person or organization that has control over whether an aircraft is to be sold or .
