O-360 & IO-360 - Superior Air Parts
Installation & Operation ManualO-360 and IO-360 Series EnginesO-360 & IO-360 SERIES ENGINESINSTALLATION & OPERATION MANUAL621 South Royal Lane, Suite 100 / Coppell, TX 75019 / 800-277-5168www.superiorairparts.comP/N SVIOM01 Revision D, June 2014
Installation & Operation ManualO-360 and IO-360 Series EnginesFAA ApprovedDISCLAIMER OF WARRANTIES AND LIMITATIONS OF LIABILITYSUPERIOR'S EXPRESS WARRANTIES AND THE REMEDIES THEREUNDER ARE EXCLUSIVE ANDGIVEN IN PLACE OF (A) ALL OTHER WARRANTIES, EXPRESS, IMPLIED, OR STATUTORY,WHETHER WRITTEN OR ORAL, INCLUDING, BUT NOT LIMITED TO, ANY WARRANTY OFMERCHANTABILITY, FITNESS OR PARTICULAR PURPOSE, OR IMPLIED WARRANTY ARISINGFROM PERFORMANCE, COURSE OF DEALING OR USAGE OF TRADE AND (B) ALL OTHEROBLIGATIONS, LIABILITIES, RIGHTS, CLAIMS OR REMEDIES, EXPRESS OR IMPLIED, ARISING BYLAW OR OTHERWISE, INCLUDING BUT NOT LIMITED TO ANY RIGHT OR REMEDIES INCONTRACT, TORT, STRICT LIABILITY OR ARISING FROM SUPERIOR'S NEGLIGENCE, ACTUAL ORIMPUTED.SUPERIOR'S OBLIGATIONS AND PURCHASER'S REMEDIES UNDER SUPERIOR'S EXPRESSWARRANTIES ARE LIMITED TO SUPERIOR'S CHOICE OF REFUND, REPAIR OR REPLACEMENTON AN EXCHANGE BASISAND EXCLUDE LIABILITY FOR INCIDENTAL, SPECIAL,CONSEQUENTIAL OR ANY OTHER DAMAGES, INCLUDING WITHOUT LIMITATION, ANY LIABILITYOF CUSTOMER TO A THIRD PARTY OR FOR ECONOMIC LOSS, REPLACEMENT COST, COST OFCAPITAL, LOST REVENUE, LOST PROFITS, OR LOSS OF USE OF OR DAMAGE TO AN AIRCRAFT,ENGINE, COMPONENT OR OTHER PROPERTY AND IN NO EVENT WILL SUPERIOR'S LIABILITYEXCEED THE ORIGINAL COST OF THE ENGINE OR ACCESSORY.Written notice of any warranty claim must be submitted to Superior within thirty (30) days of a suspecteddefect in material or workmanship and the engine, accessory or part must be made available forSuperior's inspection within thirty (30) days after the claim has been made. Superior reserves the right todeny any claim not submitted in accordance with these requirements.These LIMITED WARRANTIES are the only warranties offered by Superior. No agreement varying thesewarranties or Superior's obligations under them will be binding on Superior unless made in writing by aduly authorized representative of Superior.Superior will not process or honor warranty claims on delinquent accounts.
Installation & Operation ManualO-360 and IO-360 Series EnginesTable of ContentsChapter 1Revision HistoryList Of FiguresList Of TablesIntroductionAbout This ManualRelated PublicationsInstallation Approval RequirementsObtaining Service InformationEngine Description1. General Description2. Continued Airworthiness3. Model Designations4. Engine Components General Description5. Features And Operating MechanismsPage Numberiiiiiiivivivivv111313Chapter 2Airworthiness LimitationsChapter 3Aircraft / Engine Integration Considerations1. General2. Induction System3. Fuel System4. Engine Cooling5. Exhaust6. Lubrication System7. Propeller Attachment8. Electrical System9. Engine Controls10. Engine Accessories11. Engine nGeneral InstructionsPreparing Engine For ServiceInstallation of EngineInstrumentation Connections1122Special Procedures1. General Break In Procedures2. Special Tools And Equipment3. Break In Procedures4. General Inspection Check5. Daily Pre Flight Inspection11133Normal Operating Procedures1. General2. Engine Operation And Limits3. Operation Instructions111Chapter 4Chapter 5Chapter 6 June 2014 Superior Air Parts Inc.
Installation & Operation ManualO-360 and IO-360 Series EnginesTable of Contents (continued)Chapter 7Chapter 8Chapter 9Abnormal Operating Procedures1. General2. Engine Will Not Start3. Rough Idling4. Engine Not Able to Develop Full Power5. Rough Engine Operation6. Low Power and Engine Runs Rough7. Low Oil Pressure On Engine Gage8. High Oil Temperature9. Excessive Oil Consumption122333444Servicing Requirements1. General2. Lubricants3. Fuels4. Consumables1122Engine1.2.3.4.1223Preservation And StorageTemporary StorageIndefinite StorageInspection ProceduresReturning An Engine To Service After StorageAppendix A O-360 Model Specification DataAppendix B IO-360 Model Specification DataAppendix C Table of Limits June 2014 Superior Air Parts Inc.
Installation & Operation ManualO-360 and IO-360 Series EnginesManual Number SVIOM01Revision 07C12/14/07D6/18/14DescriptionInitial Release-C, -D and -E modelsAdded Celsius TemperatureAdded Celsius Temp and Models -C, -D and -EAdded front prop governor cases and lowcompression pistonsUpdated TBO to 1500 hrsupdate Fuel Requirements per TCDSPagesRevisedAllChapter 1, AllChapters 3,5,6 & 8 AllAppendices A and BAllChapter 1, pg 1Chapter 8, pg 2WARNINGIt is the users responsibility to ensure that this is the current revision of thismanual. Do not perform any operation, installation, maintenance, or otherprocedure until confirming this manual is current. June 2014 Superior Air Parts Inc.
Installation & Operation ManualO-360 and IO-360 Series EnginesList of FiguresFigureNumberFigure Model Number DesignationO-360 Engine Front ViewO-360 Engine Left Side ViewO-360 Engine Top ViewO-360 Engine Rear ViewO-360 Engine W/Front Prop Gov Front ViewO-360 Engine W/Front Prop Gov Left Side ViewO-360 Engine W/Front Prop Gov Rear ViewIO-360 Engine Front ViewIO-360 Engine Left Side ViewIO-360 Engine Top ViewIO-360 Engine Rear ViewIO-360 Engine W/Front Prop Gov Left Side ViewIO-360 Engine W/Front Prop Gov Top ViewO-360 Engine W/Front Prop Gov Rear ViewOil System SchematicIgnition Wiring DiagramAlternator Mounting Pad#1 Dynafocal Mount Dimensions#2 Dynafocal Mount DimensionsConical Mount DimensionsLimit and Ultimate Engine ForcesEngine Mount Forcing Function for Engine Startup and ShutdownEngine Mount Forcing Function for Steady State 15161718141721232324262727 June 2014 Superior Air Parts Inc.
Installation & Operation ManualO-360 and IO-360 Series EnginesList of TablesTableNumberTable -87-98-18-28-38-4Manufacturer’s General SpecificationsManufacturer’s Physical SpecificationsViews of the EngineAccessory Drive DataLord Engine Mounts for Superior Vantage EnginesLimit and Ultimate Engine Mount LoadsInstrumentation ConnectionsNormal Starting ProceduresStarting A Flooded EngineGround Running / Fixed Wing Warm-UpGround Running / Rotorcraft Warm-UpFixed Wing - Pre-Takeoff Ground CheckRotorcraft - Pre-Takeoff Ground CheckFuel Mixture Leaning General RulesLeaning with Exhaust Gas Temperature GageLeaning with Flow meterLeaning with Manual Mixture ControlShut Down ProcedureAbnormal Operating ProceduresEngine Will Not StartRough IdlingEngine Not Able To Develop Full PowerRough Engine OperationLow Power & Engine Runs RoughLow Oil Pressure On Engine GageHigh Oil TemperatureExcessive Oil ConsumptionOil GradesOil Sump CapacityMinimum Octane 2021252345567899991223334441122 June 2014 Superior Air Parts Inc.
Installation & Operation ManualO-360 and IO-360 Series EnginesIntroductionAbout This ManualThis engine installation and operation manual isprovided as guidance for the installation andinstallation design of a Superior Vantage Engineto an airframe and to describe its’ operationalcharacteristics. Its purpose is to providetechnical information to aid in designing andoperating an effective engine installation so asto achieve maximum performance whileproviding for maximum service life.Superior Air Parts has made clear and accurateinformation available for those who maintain,own and repair the Vantage O-360 and IO-360Series Engines. Superior Air Parts values yourinput regarding revisions and additionalinformation for our manuals. Please forwardyour comments and input to:Superior Air PartsAttn. Engineering Department621 South Royal Lane Suite 100Coppell, Texas 75019Related PublicationsThe following are related engine and accessorypublications.O & IO-360 Maintenance Manual SVMM01O & IO-360 Overhaul Manual SVOHM01O & O-360 Illustrated Parts Cat. SVIPC01Unison Master Service Manual, F-1100Precision RSA-5 Service Manual, 15-338Precision MA-4-5 Manual, MSAHBK-1Champion Aerospace Service Manual,AV-6R June 2014 Superior Air Parts Inc.Installation Approval RequirementsThe engine warranty for a Vantage Engineinstallation is subject to the technical approval ofSuperior. Upon approval of an installationdesign, Superior will provide a letter that statesin part that the installation design is acceptableand does not adversely affect the function of theengine with respect to engine longevity while theengine is operated in accordance withrecommended procedures.Superior requires certain technical dataregarding the installation in order to determineits acceptability for warranty purposes. Thisdata may include, but is not limited to drawings,photographs and test data. Approval of theinstallation for these purposes is limited to theinstallation design furnished by the airframemanufacturer to Superior. Modifications orchanges to the installation design require a newor amended letter of approval prior to thewarranty becoming effective for that design.Approval of the installation by Superior asdescribed above is limited to engine warrantyissues only. It does not in any way indicateapproval of other aspects of the installationdesign such as structural integrity andmanufacturability.Superior Vantage Engines discussed in thisdocument must be installed and operated inaccordance with the limitations, conditions andoperating procedures described in thisdocument, the Model Specification Data and theInstallation and Operation Manual. They mustalso be maintained in accordance with theapplicable Overhaul Manual and otherInstructions for Continued Airworthiness.Superior accepts no responsibility forairworthiness of any aircraft resulting from theinstallation of the engine or associatedequipment.
Installation & Operation ManualO-360 and IO-360 Series EnginesObtaining Service InformationAccessory Information may be obtained at:All Vantage Series Engine manuals and serviceinformation may be downloaded omwww.skytecair.comAll Vantage Series Engine manuals and serviceinformation may also be purchased essories.comSuperior Air Parts621 South Royal Lane, Suite 100Coppell, Texas 75019or call: 972-829-4600 June 2014 Superior Air Parts Inc.
Installation & Operation ManualO-360 and IO-360 Series EnginesCHAPTER 1Engine Description1.GENERAL DESCRIPTIONdefined as viewed from the rear of the enginelooking forward.Superior Vantage Engines are four-cylinder,horizontally opposed, air-cooled, direct drivepowerplants incorporating a wet sump, bottommounted induction, bottom exhaust with eithercarbureted or port injected fuel systems.Provisions exist for both front and rear mountedaccessories.All engine components will bereferenced as they are installed in the airframe.Therefore, the “front” of the engine is thepropeller end and the “rear” of the engine is theaccessory mounting drive area. The oil sump ison the “bottom” of the engine and the cylindershroud tubes are on the “top”. The terms “left”and “right” are defined as being viewed from therear of the engine looking toward the front.Cylinder numbering is from the front to the rearwith odd numbered cylinders on the right side ofthe engine. The direction of crankshaft rotationis clockwise as viewed from the rear of theengine looking forward unless otherwisespecified. Accessory drive rotation direction is2.CONTINUED AIRWORTHINESSVantage Engines discussed in this documentmust be installed and operated in accordancewith the limitations, conditions and operatingprocedures described in this document. Theymust also be maintained in accordance with theapplicableOverhaulManualandotherInstructions for Continued Airworthiness. Theengine’s time between overhaul (TBO) periodsis initially defined as 1500 hours.A TBOextension program is in process.3.MODEL DESIGNATIONSThe model number designation is defined in away that the digits of the model number caneasily identify the basic configuration of theengine as described in Figure 1-1.Figure 1-1 Model Number Designation1 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesFuel System TypeIODenotes Port Fuel Injection System and “opposed cylinder” arrangement.ODenotes a carbureted system and “opposed cylinder” arrangement.Cylinder Type360Parallel valve cylinder, 361 cubic inches.Model SuffixDenotes detail engine configurationst1 DigitCrankshaft & Propeller TypeABCDEnd2Fixed-Pitch, Thin-wall front mainConstant-Speed, Thin-wall front mainFixed-Pitch, Heavy-wall front mainConstant-Speed, Heavy-wall front mainFixed-Pitch, Solid front mainDigitCrankcase & Engine Mount Type123456rd3#1 Dynafocal Mount#2 Dynafocal MountConical Mount#1 Dynafocal Mount, Front Propeller Governor#2 Dynafocal Mount, Front Propeller GovernorConical Mount, Front Propeller GovernorDigitAccessory PackageIgnition SystemAth4 Digit12Unison MagnetosFuel SystemCarburetedPrecision CarburetorFuel InjectedPrecision Fuel InjectionPower Rating: Piston Compression RatioCylinder Type360CRHP7.2:11688.5:11802 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series Engines4. ENGINE COMPONENTS GENERALDESCRIPTION13.14.15.16.17.The O-360 and IO-360 series engines are aircooled, four cylinder, horizontally opposed,direct drive engines.See Table 1-1 forManufacturer’s General Specifications.A. The complete engine includesfollowing components and assemblies:1.2.3.4.5.6.7.8.9.10.11.12.Fuel SystemStarter Support AssemblyOil GageInduction SystemAccessoriesNote: Complete engine does not include outercylinder baffles, propeller governor, and airframeto engine control cables, attaching hardware,hose clamps, vacuum pump, exhaust system,fittings or alternator.theCrankcase AssemblyCrankshaft AssemblyCamshaft AssemblyValve Train AssemblyCylinder AssembliesConnecting Rod AssembliesOil Sump AssemblyInter Cylinder BafflesStarterLubrication System (includes oil filter)Accessory DriveIgnition System (includes spark plugs)B. SpecificationsThe manufacturer’s physical specifications arelisted in Table 1-2 are applicable to the O-360and IO-360 series engines.See ModelSpecificationData(MSD)formorespecific information.Table 1-1 Manufacturer’s General SpecificationsModelRated PowerRated Speed, RPMBore, inchesStroke, inchesDisplacement cubic inchesCompression RatioFiring OrderSpark timingPropeller drive ratioPropeller drive rotation(viewed from rear)HpRPMInIn3In BTDCO-360 and IO-360168 OR 18027005.1254.375361.07.2:1 OR 8.5:11-3-2-4251:1Clockwise3 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesTable 1-2 Manufacturer’s Physical dth(In)33.433.4Length(In)32.832.8WeightSee MSDSee MSDMSD Model Specification DataTable 1-3 Views of the EngineEngine ViewO-360 Engine Front ViewO-360 Engine Left Side ViewO-360 Engine Top ViewO-360 Engine Rear ViewO-360 Engine W/Front Prop Gov Front ViewO-360 Engine W/Front Prop Gov Left Side ViewO-360 Engine W/Front Prop Gov Rear ViewIO-360 Engine Front ViewIO-360 Engine Left Side ViewIO-360 Engine Top ViewIO-360 Engine Rear ViewIO-360 Engine W/Front Prop Gov Left Side ViewIO-360 Engine W/Front Prop Gov Top ViewIO-360 Engine W/Front Prop Gov Rear ViewFigure NumberFigure 1-2Figure 1-3Figure 1-4Figure 1-5Figure 1-6Figure 1-7Figure 1-8Figure 1-9Figure 1-10Figure 1-11Figure 1-12Figure 1-13Figure 1-14Figure 1-15Locationp. 5p. 6p. 7p. 8p. 9p. 10p. 11p. 12p. 13p. 14p. 15p. 16p. 17p. 184 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesSPARK PLUGSPARK PLUGPRIMINGSYSTEMSTARTERCHT PROBE LOCATION(TYPICAL EACH HEAD)ALTERNATOR & BELTALTERNATOR & BELT NOTPROVIDED WITH ENGINETHROTTLE LEVERFUEL LINECARBURETORFigure 1-2 O-360 Engine Front View5 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series OUSINGOILFILTERHARNESSSTARTER SPARKPLUGFUELLINEINDUCTIONSYSTEMOIL SUPMASSEMBLYMIXTURELEVERCARBURETORFigure 1-3 O-360 Engine Left Side View6 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesINNER-CYLINDER BAFFLESPARK PLUGMAGNETOMAGNETOOIL TEMPCONNECTIONOIL FILTERFigure 1-4 O-360 Engine Top View7 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesALTERNATE OIL TO COOLEROIL RETURN FROM COOLERTACHOMETER CONNECTIONEYEBRACKETBREATHERFITTINGVACUUM PUMP/ACCESSORY PADOIL PRESSURE GAGE CONNECTIONOIL LEVEL TUBE & GAGEOIL FILTERMANIFOLDPRESSURECONNECTIONGROUND OR “P LEAD” TERMINALGROUND OR “P-LEAD” TERMINALOIL SUPPLY TO COOLEROIL LINE TOPROPELLERCOMMON PRIMERLINE SOURCEVENT LINECONNECTIONOIL DRAINPLUGDIAPHRAGMFUEL PUMPFUEL LINETHROTTLELEVERFUEL MIXTURELEVEROIL SUCTIONSCREENFUEL PUMP INLETFigure 1-5 O-360 Engine Rear view8 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesSPARK PLUGSPARK PLUGPRIMINGSYSTEMSTARTERCHT PROB LOCATION(TYPICAL EACH HEAD)ALTERNATOR & BELT NOTPROVIDED WITH ENGINEFUEL LINECARBURETORTHROTTLE LEVERFigure 1-6 O-360 W/Front Prop GovernorEngine Front View9 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series OUSINGPROP GOVERNORLOCATIONOILFILTERHARNESSSTARTER SPARKPLUGFUELLINEINDUCTIONSYSTEMOIL SUPMASSEMBLYMIXTURELEVERCARBURETORFigure 1-7 O-360 W/Front Prop Gov. EngineLeft Side View10 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesOIL RETURN FROM COOLERALTERNATE OILTOCOOLEREYEBRACKETBREATHERFITTINGOIL FILTERTACHOMETER CONNECTIONVACUUM PUMP / ACCESSORY PADOIL PRESSURE GAGE CONNECTIONOIL LEVEL TUBE & GAGEMANIFOLDPRESSURECONNECTIONGROUND OR “P-LEAD” TERMINALGROUND OR “P-LEAD”TERMINALOIL SUPPLY TO COOLERCOMMON PRIMERLINE SOURCEOIL DRAINPLUGVENT LINECONNECTIONDIAPHRAGMFUEL PUMPFUEL LINETHROTTLELEVERFUEL MIXTURELEVEROIL SUCTIONSCREENFUEL PUMP INLETFigure 1-8 O-360 W/Front Prop Gov. EngineRear View11 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesFUEL INJECTIONMANIFOLDSPARK PLUGSPARK PLUGFUELINJECTORCHT PROBE LOCATION(TYPICAL EACH HEAD)STARTERALTERNATOR & BELTNOT PROVIDED WITH ENGINEFUEL INJECTIONSERVOFigure 1-9 IO-360 Engine Front View12 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesCYLINDERASSEMBLYCRANKCASEASSEMBLYFUEL INJECTIONMANIFOLDACCESSORYHOUSINGOIL FILTERSTARTER SUPPORTASSEMBLYWIRINGHARNESSMAGNETOSTARTERFUEL PUMPSPARK PLUGFUEL LINEFUEL INJECTIONSERVOOIL SUMPFigure 1-10 IO-360 Engine Left Side View13 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesFUEL INJECTIONMANIFOLDFUEL INJECTOROIL TEMPCONNECTIONFigure 1-11 IO-360 Top View14 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesTACHOMETER CONNECTIONBREATHER FITTINGALTERNATE OILTO COOLERVACCUM PUMP/ACCESSORY PADEYEBRACKETFUEL INJECTION MANIFOLDOIL PRESSURE GAGE CONNECTIONOIL FILEROIL LEVEL TUBE & GAGEGROUND OR “P-LEAD” TERMINALGROUND OR “P-LEAD” TERMINALOIL SUPPLY TO COOLERVENT LINE CONNECTIONDIAPHRAGM FUELPUMPOIL LINE TOPROPELLEROIL DRAIN PLUGMIXTURE CONTROLLEVERFUEL PUMP INLETTHROTTLE CONROLLEVEROIL DRAIN PLUGOIL SUCTIONSCREENFigure 1-12 IO-360Engine Rear View15 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesSTARTER EL INJECTIONMANIFOLDACCESSORYHOUSINGOIL FILTERWIRIN HARNESSMAGNETOFUEL PUMPSTARTERSPARK PLUGOIL SUMPFUEL INJECTIONSERVOFigure 1-13 IO-360 W/Front Prop GovernorEngine Left Side View16 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesFUEL INJECTIONMANIFOLDFUEL INJECTOROIL TEMPCONNECTIONFigure 1-14 IO-360 W/front Prop GovernorEngine Top View17 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesALTERNATE OIL TO COOLEREYEBRACKETBREATHERFITTINGTACHOMETER CONNECTIONOIL RETURN FROM COOLERVACUUM PUMP / ACCESSORY PADOIL PRESSURE GAGE CONNECTIONOIL LEVELTUBE & GAGEOIL FILTERMANIFOLDPRESSURECONNECTIONGROUND OR “P-LEAD”TERMINALGROUND OR “P-LEAD”TERMINALVENT LINECONNECTIONOIL SUPPLY TOCOOLERDIAPHRAGMFUEL PUMPFUEL PUMP INLETOIL DRAIN PLUGFUEL MIXTURELEVEROIL SUCTIONSCREENOIL DRAINPLUGTHROTTLELEVERFigure 1-15 IO-360 W//Front Prop GovernorEngine Rear View18 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series Engines5. FEATURES AND OPERATINGMECHANISMStype with a plug located in each end of the pin.The piston is a 3-ring type with 2 compressionrings and 1 oil control ring.Crankshaft - The crankshaft is made from highstrength steel. All bearing journal surfaces arenitrided.Connecting Rods - The connecting rods aremade from steel.They have replaceablebearing inserts in the crankshaft ends andbronze bushings in the piston ends.Thebearing caps on the crankshaft ends areretained by two bolts with self locking nuts percap.Caps are tongue and groove type forimproved alignment and rigidity.Camshaft - Valve Operating Mechanism - Thecamshaft is located above and parallel to thecrankshaft.The camshaft actuates hydrauliclifters that operate the valves through push rodsand valve rockers.Crankcase - The crankcase is made fromaerospace grade AA C355-T71 stabilized castaluminum alloy. The assembly consists of twocastings fastened together by means of studs,bolts, and nuts. The main bearing bores aremachined for use with precision type mainbearing inserts.Accessory Housing - The accessory housing ismade from an aluminum casting and is fastenedto the rear of the crankcase and the top rear ofthe sump.Oil Sump - The sump incorporates an oil drainplug, oil suction screen, mounting pad forcarburetor or fuel injector, the intake riser, andintake pipe connections.Cylinders - Millennium Cylinders are usedexclusively.These air-cooled cylinders aremanufactured by screwing and shrinking the twomajor parts, head and barrel, together. Theheads are made from heat resistant aluminumalloy casting material. All barrels are made fromaerospace grade forgings. They are internallychoked and honed to allow optimal operatingconditions for the rings and pistons at operatingtemperatures.Pistons - The pistons are made from analuminum alloy. The piston pin is a full floatingCooling System – Superior Vantage Enginesare designed to be air-cooled.Baffles areprovided to build up air pressure and force theair between the cylinder fins.The air isexhausted to the atmosphere through the rear ofthe cowling.Induction System - The distribution of the air toeach cylinder is through the center zone of theinduction system. This is integral with the oilsump.Fuel SystemsCarbureted - Superior Air Parts O-360 enginesare equipped with a float type carburetor TheMA-4-5 carburetors are of the single barrel floattype equipped with a manual mixture control andan idle cut-off.Fuel Injected - IO-360 series engines areequipped with a direct cylinder injected RSA-5fuel injector.The fuel injection systemschedules fuel flow in proportion to airflow. Fuelvaporization takes place at the intake ports. TheRSA fuel injection system is based on theprinciple of measuring airflow and using the airpressure in a stem type regulator, converting theair pressure into a fuel pressure.The fuelpressure (fuel pressure differential), whenapplied across the fuel metering section (jettingsystem), makes fuel flow proportional to airflow.Lubrication System - The full pressure wetsump lubrication system is supplied by a geartype pump. It is contained within the accessoryhousing.Priming System - A manual primer system isprovided on all engines using a carburetor. Fuelinjected engines do not require a manualpriming system, relying instead on the fuelinjectors for priming.Ignition System - Dual ignition is furnished bytwo Unison magnetos with two spark plugs percylinder.Each magneto is equipped withimpulsecouplingforimprovedstarting.19 June 2014 Superior Air Parts Inc.Chapter 1 EngineDescription
Installation & Operation ManualO-360 and IO-360 Series EnginesCHAPTER 2Airworthiness LimitationsThe Airworthiness Limitations Section is F.A.A.approved and specifies maintenance requiredunder sections 43.16 and 91.403 of the FederalAviation Regulations unless an alternateprogram has been FAA approved. This sectionis part of the type design of the O-360 and IO360 engine series pursuant to es to this Airworthiness LimitationsChapter constitute changes to the type design ofthe O-360 and IO-360 engine series and requireF.A.A. approval pursuant to Federal AviationRegulations. Such changes will be published inF.A.A. Approved Mandatory Service Bulletins.Superior Vantage Engine Service Bulletins maybe obtained by writing to:1. MANDATORY REPLACEMENT TIMESubject to additional information contained inF.A.A. Approved Mandatory Service Bulletinsissued after the date of certification, the O-360and IO-360 engine series do not contain anycomponents having mandatory replacementtimes required for type certification.Superior Air Parts621 South Royal Lane, Suite 100Coppell, Texas 75019or call: 972-829-4600or on the web at www.superior-air-parts.com2. MANDATORY INSPECTION INTERVALSSubject to additional information contained inF.A.A. Approved Mandatory Service Bulletinsissued after the date of certification, the O-360and IO-360 engine series do not contain anycomponentshavingmandatoryinspectionintervals.3. OTHER MANDATORYPROCEDURESINTERVALSORSubject to additional information contained inF.A.A. Approved Mandatory Service Bulletinsissued after the date of certification, the O-360and IO-360 engine series do not have anyinspection-related or replacement time-relatedprocedures required for type certification.1 June 2014 Superior Air Parts Inc.Chapter 2 Airworthiness Limitations
Installation & Operation ManualO-360 and IO-360 Series EnginesCHAPTER 3Aircraft / Engine Integration Considerations1.GENERALVantage Series be capable of supplying clean,filtered, cool intake air to the engine at themaximum required flow rate and with maximumattainable pressure.The term “maximumattainable pressure” as used here refers to anair source that provides maximum intake airpressure, (including ram air effects) whileminimizing restrictions and flow losses. Areduction in flow rate or total pressure, orincreased temperature can cause power loss,reduced service ceiling and increased possibilityof detonation during high power requirements.The following sections in this chapter include adiscussion of design practices to be consideredduring the integration of a Superior Vantageengine with an airframe and propeller. Thesediscussions should be used IN ADDITION TOthe applicable requirements of the FARs.Superior requires that proper functioning of thesystem designs outlined in this chapter beproven prior to activation of the warranty.Proper functioning of the installation design shallbe proven by technical data such as test s.Superior Air Parts EngineeringDepartment will provide guidance regarding thespecifics of these requirements as appropriate tothe installation and on a case-by-case basis.Properly engineered intake systems for naturallyaspirated engines should result in total intake airpressures that are greater than ambient airpressure. For example, air pressure in the intakesystemcanberaisedbydirecting the face of the air pickup into therelative wind of the aircraft. Further, by locatingthe air pickup within the propeller diameter, ramair effects can be increased. Care should betaken to position the air pickup as far as possibleaway from the propeller axis (but within the“propeller envelope”) so as to take advantage ofthe increased air velocities at the outer areas ofthe prop. Care should also be given to prevent“blanking” of the intake air pickup by the propblade. Increasing the size of the air pickup,particularly in the direction perpendicular to theblade axis, can help reduce this potential. Careshould also be given to designing an air pickupthat maintains maximum frontal area duringperiods of high aircraft angle of attack.Typically, maximum power is required duringflight conditions having high angle of attack andreductions in airflow will restrict maximum powercapability.Throughout this chapter reference is made todata contained in the Model Specification Data.These documents are engine series specific andare contained in Appendices of this manual.Refer to the appropriate Model SpecificationData for your engine model when consulting thisdata.2.INDUCTION SYSTEMThe induction system design can significantlyaffect both performance and longevity of anaircraft
Installation & Operation Manual O-360 and IO-360 Series Engines O-360 & IO-360 SERIES ENGINES INSTALLATION & OPERATION MANUAL 621 South Royal Lane, Suite 100 / Coppell, TX 75019 /
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