Garmin G3000 Owner's manual

CESSNAAIRCRAFTCOMPANY
AIRCRAFTDIVISION
WICHITA,KANSAS67277
GarminG3000IntegratedAvionicsSystem-
Adjustment/Test
ICASupplement
MODELNO:525B
SUPPLEMENTNO:ICA-525B-34-00002A
SUPPLEMENTDATE:12/05/2016
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Form2261Rev1

CESSNAAIRCRAFTCOMPANY
AIRCRAFTDIVISION
WICHITA,KANSAS67277
REVISIONS
ICA-525B-34-00002Rev:-Date:Dec17/2015
ICASummaryPages1-6
ManualsAffectedDescriptionTitle
MaintenanceManual34-65-00pages
501-540
GarminG3000IntegratedAvionicsSystem-Adjustment/
Test
•Changesthesoftwareloadingprocedures.
AppendixA:IllustratedParts
Catalog
NOTUSED
AppendixB:WiringDiagram
Manual
NOTUSED
ICA-525B-34-00002Rev:ADate:Dec05/2016
ICASummaryPages1-6
ManualsAffectedDescriptionTitle
MaintenanceManual34-65-00Pages
101-103
GarminG3000IntegratedAvionicsSystem-
Troubleshooting
•Changesthetroubleshootinginstructions.
MaintenanceManual34-65-00Pages
501-542
GarminG3000IntegratedAvionicsSystem-Adjustment/
Test
•Changesthesoftwareloadingprocedures.
MaintenanceManual45-40-15Pages
201-205
UpdateCMCConguration/CDMSVersion-
MaintenancePractices
•Changesthesoftwareloadingprocedures.
AppendixA:IllustratedParts
Catalog
NOTUSED
AppendixB:WiringDiagram
Manual
NOTUSED
1.ExportCompliance
A.ThispublicationcontainstechnicaldataandissubjecttoU.S.exportregulations.Thisinformationhas
beenexportedfromtheUnitedStatesinaccordancewithexportadministrationregulations.Diversion
contrarytoU.S.lawisprohibited.
ECCN:9E991
2.RevisionBars
A.RevisionbarsinthisICAsupplementidentifynewICAsand/orchangestothecurrentICAsinthe
releasedmaintenancemanual.
•NewICAsthatarenotinthecurrentmaintenancemanualwillhavearevisionbarfromtopto
bottomalongtheleftmargin.
•ICAsthatareinthecurrentmaintenancemanualandhaveinformationadded,deletedorrevised
willhavearevisionbar(s)intheleftmarginadjacenttotheadded,deletedorrevisedinformation.
•Neworchangedillustrationswillhaveachangebarfortheentirelengthofthepage.
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3.PageNumbering
A.ThepagenumbersystemforICAincludedinthissupplementhavethree-elementnumbersthatare
separatedbydashes.Thethree-elementnumberisfoundatthebottomrightcornerofthepage,left
ofthepagenumber.Thedateisfoundbelowthepagenumber.
B.Whenthechapter/systemelementnumberisfollowedwithzerosinthesection/subsystemand
subject/unitelementnumber(28-00-00),theinformationisapplicabletotheentiresystem.
C.Whenthesection/subsystemelementnumberisfollowedwithzerosinthesubject/unitelement
number(28-21-00),theinformationisapplicabletothesubsystemsinthesystem.
D.Thesubject/unitelementnumberisusedtoidentifyinformationapplicabletounitsinthesubsystems.
Thesubject/unitelementnumbercontinuesinsequencefromthenumber-01-withthenumberof
subsystemunitsinwhichmaintenanceinformationisnecessary.
E.Allsystem/subsystem/unit(chapter/section/subject)maintenancedataisseparatedintospecied
typesofinformation:DescriptionandOperation,Troubleshooting,MaintenancePractices,etc.
Blocksofpagenumbersthatareinsequenceareusedtoidentifythetypeofinformation:
(1)DescriptionandOperationorTroubleshootinginformationmaynotbeincludediftheprocedure
iseasy.Whensubtopicsareshort,theymaybeputtogetherintotheMaintenancePractices
section.MaintenancePracticescanhaveamixofsubtopicsthatincludesinformationtoservice,
remove,install,adjust,test,clean,paintordoapprovedrepairs.
(2)Longerproceduresthatarenotaseasytodomaybeincludedinaspeciedsection.
Page1through99-DescriptionandOperation
Page101through199-Troubleshooting
Page201through299-MaintenancePractices
Page301through399-Servicing
Page401through499-Removal/Installation
Page501through599-Adjustment/T est
Page601through699-Inspection/Check
Page701through799-Cleaning/Painting
Page801through899-ApprovedRepairs
F.Atypicalpagenumber:
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G.Illustrationsusethesamegurenumbersasthepageblockinwhichtheyappear.Forexample,Figure
202wouldbethesecondgureinaMaintenancePracticessection.
4.SupplementRevisions
A.Revisionstothissupplementmaybeaccomplishedifchangestothissupplementarerequiredafter
releaseoftheoriginalissueandpriortoincorporationintothemanualslistedintheREVISIONStable.
B.Allrevisionstothissupplementwillhavechangesidentiedindetailintherevisionblock(s)above.
C.AllpagesinthisICAsupplementwillhavethesamedateandarevalidasofthedateshown.
5.ICAIncorporationintoApplicableManuals
NOTE:MostICAsupplementswillbeincorporatedinthenextavailablerevisiontothemanualslisted
aboveandshouldbeusedinconjunctionwiththosemanualsuntilthenextavailablerevisionis
released.
A.TheICASupplementListlocatedintheIntroductionsectionofeachmanuallistedintheREVISIONS
tablewillindicatetheincorporationstatusasofthereleasedateofthepublishedrevision.
B.Themanualrevisionlevelofthesupplementincorporationwillbelistedinthe"ManualIncorporation
Status"columnintheICASupplementList,whenthoseICAsassociatedwiththatmanualhavebeen
incorporated.AfterICAsareincorporated,themanualthattheyareincorporatedinmustnowbeused
forthoseICAsinsteadofthesupplement.
•Basedonrevisioncycletimesfortheaffectedmanuals,MMICAs,WDMICAs,etc.inthis
supplementmaybeincorporatedinthemanualsatdifferenttimes.
•Therewillnotbearevisiontothissupplementtoindicateincorporationinthemanuals.Usersare
requiredtochecktheICASupplementListforeachmanualaffectedtodetermineincorporation
status.
C.ThissupplementwillbecompletelysupersededbythemanualslistedintheREVISIONStablewhen
ithasbeenincorporatedinallofthemanuals.
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INTRODUCTION
1.Purpose
A.ThepurposeofthisSupplementistoprovidethemaintenancetechnicianwiththeinformation
necessarytoensurethecorrectfunctionalityandperformanceoftheGarminG3000Integrated
AvionicsSystem-Adjustment/TestontheCessnaModel525Buntilthisinformationgetsincorporated
intothenextrevisiontothemanualslistedinthe"REVISIONS"sectionofthissupplement.
B.ThisICAsupplementisdesignedtosatisfytherequirementsof14CFR23.1529"Instructionsfor
ContinuedAirworthiness"associatedwiththisinstallation.Thisdocumentisasupplementtothe
Model525BMaintenanceManualandwillbeincorporatedinthenextrevisiontothemanual.
C.Whenthisinformationisincorporatedinthenextrevisiontothemanualslistedinthe"REVISIONS"
section,thosemanualsshalltakeprecedenceoverthissupplementaldocument.Refertothe"ICA
SupplementList"inthe"Introduction"sectionoftherespectivemanualforthestatusofallapplicable
ICASupplements.
D.RevisionstothissupplementmayoccurifthereisachangetoanyoftheICAsinthissupplement
priortoincorporationintoalloftheaffectedmanuals.
NOTE:Thisdocumentmustbeplacedwiththeaircraftoperator'sTechnicalLibraryCD-ROM
orModel525BMaintenanceManualandincorporatedintotheoperator'sscheduled
maintenanceprogram.
2.Effectivity
A.TheseInstructionsforContinuedAirworthiness(ICA)areeffectiveforthefollowingaircraftmodeland
serialization.
ModelBeginningEffectivityEndingEffectivity
525B000057000057
525B000451andOn
3.CompleteICADocuments
A.Thefollowingdocument(s),inconjunctionwiththissupplement,constitutetheInstructionsfor
ContinuedAirworthinessfortheGarminG3000IntegratedAvionicsSystem-Adjustment/Testonthe
CessnaModel525B.Allitemsmustbeavailabletotheoperatoratinitialdelivery.
(1)Model525BMaintenanceManual
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LISTOFINSTRUCTIONSFORCONTINUEDAIRWORTHINESS
1.Model525BMaintenanceManual
A.Chapter34Navigation
(1)ATA34-65-00GarminG3000IntegratedAvionicsSystem-Troubleshooting
(a)General
(b)G3000SystemTroubleshooting
(c)SoftwareUploadTroubleshooting
(2)ATA34-65-00GarminG3000IntegratedAvionicsSystem-Adjustment/Test
(a)General
(b)AirplaneSetup
(c)CompleteSoftwareLoadingOverview
(d)CongurationLoadingOverview
(e)OptionsActivationOverview
(f)OptionsRemovalOverview
(g)LRUReplacementOverview
(h)DiagnosticDataWirelessTransmitSettings
(i)SoftwareLoadingCongurationMode
(j)StandardCongurationMode
(k)UpdateSystemFiles
(l)BaseSoftware/CongurationLoadProcedures
(m)UpdateCustomGraphics
(n)DiagnosticConguration
(o)AirplaneOptionsInstallation
(p)CongurationModuleProgramming
(q)CongurationManagement
(r)AirplaneConguration
(s)DefaultPilotProleLoadingProcedures
(t)Verication
(u)DatabaseCardLoadingProcedures
(v)TOLDDatabase
(w)ReloadConguration(OptionsRemoval)Procedures
(x)LRUReplacementSoftwareUploadProcedures
B.Chapter45CentralMaintenanceSystem
(1)ATA45-40-15UpdateCMCConguration/CDMSVersion-MaintenancePractices
(a)General
(b)ToolsandEquipment
(c)VerifytheCMC/CDMSDiagnosticsConguration
(d)UpdatetheCMCDiagnosticCongurationand/ortheCDMSSoftwareVersion
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INSPECTIONPROGRAMANDAIRWORTHINESSLIMITATIONS
1.ContinuousInspectionProgram
A.ThisICASupplementdoesnotaffectthecurrentinspectionprogram.
2.AirworthinessLimitations
A.CessnaAircraftCompanyModel525BMaintenanceManual,Chapter4,AirworthinessLimitations,
containsthesystemandairframelimitationsfortheModel525B.
NOTE:TheAirworthinessLimitationssectionisFAA-approvedandspeciesmaintenance
requiredunderSection43.16and91.403ofTitle14CodeofFederalRegulations,unless
analternativeprogramhasbeenFAAapproved.
(1)Therearenonew(oradditional)airworthinesslimitationsassociatedwiththisequipmentand/or
installation.
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CESSNAAIRCRAFTCOMPANY
MODEL525B
MAINTENANCEMANUAL
GARMING3000INTEGRATEDAVIONICSSYSTEM-TROUBLESHOOTING
1.General
A.ThissectiongivestheGarminG3000IntegratedAvionicsSystemstandardinstallationtroubleshooting
procedures.ForageneraldescriptionoftheG3000systemrefertoGarminG3000IntegratedAvionics
System-DescriptionandOperation.FormoreadetailedoverviewoftheCrewAlertSystem(CAS)
data,refertotheGarminG3000IntegratedAvionicsSystemLineMaintenanceManual,P/N190-
01579-00,Section4.0,foundintheSupplierPublicationList.
B.TheGarminGTC570T ouchscreenControlUnitspilotGTC1(left),andcopilotGTC2,(right)arethe
primarycontrollersoftheGarminG3000IntegratedAvionicsSystem.Forageneraldescriptionofthe
GTC570refertoGarminG3000IntegratedAvionicsSystem-DescriptionandOperation.
C.Thissectioncontainslinereplaceableunit(LRU)troubleshootingmethodsandprocedurestoisolate
LRUandotherpossiblesystemcircuitfaults.Theseproceduresareintendedasageneralguidefor
G3000systemtroubleshootingandsystemreturntoservice.Thissectioncanassistwithgeneral
troubleshootingproceduresforoptionalGarminandothersupplierssystemsthatintegratewiththe
G3000system.Formoretroubleshootingprocedurestondthecauseofasystemfault,refertothe
specicGarminsystemLRUsectioninthismanual.
D.TotroubleshootrelatedCentralMaintenanceComputer(CMC)eventdrivenfaultmessagedothe
stepsthatfollow:
(1)ToshowthespecicCMCAlertIDonthemultifunctiondisplay(MFD),getaccesstotheCitation
DiagnosticMaintenanceSystem(CDMS)FaultDetailscreen.RefertoChapter45,Citation
DiagnosticMaintenanceSystem(CDMS)-MaintenancePractices.
(2)FortroubleshootingdatarelatedtothespecicCMCAlertID,refertoRefertoChapter45,Event
Drivenfaultmessages-DescriptionandOperation.
2.G3000SystemTroubleshooting
A.Dothepreliminarystepsthatfollowtoprepareforthefaultisolationprocedures.
(1)Ontheprimaryightdisplay(PFD)lookforaCrewAlertingSystem(CAS)WARNING,CAUTION
orADVISORYalert.
NOTE:DuringthetimetheG3000ispoweringup,certainwindowsremaininvalidasthe
equipmentbeginstoinitialize.Allwindowsshouldbeoperationalwithinoneminute
ofpower-up.Ifanywindowcontinuestobeagged,begintroubleshooting.
(2)IfthereisaCASalertmessagedothestepsthatfollow:
(a)ForadetaileddescriptionofthepossiblecauseoftheCASmessageinitiationreferto
Navigation(GarminG3000Airplanes)-Troubleshooting.
(b)Makesurethatthesystemlinereplaceableunit(LRU)circuitbreakerisengaged.
(c)Ifasubscriptionserviceisnecessaryforthesystemfunctionthathasthefault,makesure
thatthesubscriptioniscurrent.
1Ifthesubscriptionisnotcurrentcontactsubscribercompanytogetthenecessary
service.
(d)Ifthefaultisnotcorrected,onGTC1orGTC2,pushtheMSGbuttontoacknowledgethe
messageandtoshowtheMessagespage.
(e)Recordtheactivemessages(whitetext).
(3)OntheGTC1orGTC2Homepage,pushthebuttonsinthesequencethatfollows:
(a)SetuptoshowtheSetuppage.
(b)AvionicsStatustoshowtheAvionicsStatuspage.
(c)Ifnecessary,touchtheLRUInfotab.
(4)ScrolltotheapplicableLRUInfotabandmonitorthedatathatfollows:
(a)TheLRUstatus.
•Activeshowscheck(green)
•CautionshowsX(amber)
•FailedshowsX(red).
(b)TheLRUserialnumber.
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CESSNAAIRCRAFTCOMPANY
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MAINTENANCEMANUAL
(c)TheLRUversion.
(5)RefertotheGarminG3000IntegratedAvionicsSystemLineMaintenanceManualCessna
CitationCJ3+,P/Ndocument190-01785-00,Section4.0forthepossiblecausesforthesystem
fault.
B.TroubleshootaCaution(amber)orFailedX(red)thatshowsonthedisplay.
(1)Usethesystemfaultsymptoms,advisorymessages,G3000initiatedmanualtestresults,and
theG3000LineMaintenanceManualrecommendedprocedurestoanalyzethesystemfaultand
makeadecisionastothebestprocedurestofollowtocorrectthesystemproblem.
(2)Whenaproblemiscorrected,checkthesystemoperationagain.
(3)Dothestepsthatfollowthatareapplicabletothefaultanalysiscompletedforthesystemfault.
(a)IftheGTCAvionicsStatuspageshowsacongurationorsoftwareproblemloadthecorrect
version.RefertoGarminG3000IntegratedAvionicsSystem-Adjustment/Test.
(b)Ifthesoftware/congurationdoesnotuploadforaspecicLRUrefertoSoftwareUpload
Troubleshooting.
(c)Ifthereisstillacongurationand/orsoftwareproblemafteryouuploadtheLRUspecic
les,uploadtheentireG3000systemcongurationandsoftwareles.RefertoGarmin
G3000IntegratedAvionicsSystem-Adjustment/T est.
(4)Ifasatelliteisusedforthesystemtotransmit/receive,makesurethattheantennalocationon
theairplanehasanunobstructedviewofthesatellite.
C.WiringTroubleshooting
(1)DoaVisualcheckoftheapplicableLRUelectricalconnector(s)andairplaneelectrical
connectorsfortheunserviceableconditionsthatfollow:
•Bentpins
•Pushedbackpins
(a)Repairfounddamage.
(2)AtthesuspectLRUconnectormakesurethatelectricalpowerandgroundsignalsarepresent.
(3)Makesurethatdatabuslinesareproperlyterminatedandsecure.Useanohmmetertodoa
continuitycheckofthebuswires.Checkeachwireendtoend.
NOTE:Donotbuswiringtoeachotherorshieldgrounds.ChecktheHSDBandARINC429
buswiring.
(4)Ifapplicable,refertotheModel525BWiringDiagramManualanddoavisualcheckofthewiring
componentsthatfollowandmakesurethat:
•TheLRU'slocationstrappingiscorrect
•OthernecessaryG3000systemstrappingiscorrect.
(5)DoaVisualcheckofthewiringbundlesfordamage.
(a)Ifnecessary,repairorreplacethewiringbundles.
(6)Doacheckoftheapplicablesystemwiringforcontinuity,groundfaultsorotherunserviceable
conditions.RefertotheModel525BWiringDiagramManual.
(a)Ifnecessary,repairorreplacethewiringbundles.
(7)FortheVHF ,DataLinkandGPSsystems,doavisualcheckofthecoaxialcableconnectionsto
theapplicableLRUandantenna(s)andifnecessary:
(a)Tightenloosecoaxialcableconnectors.
(b)Repairorreplaceunserviceablecoaxialcable.
(8)IftherearetwoidenticalLRUsinstalled,interchangetheLRUpositionsandchecksystem
operationagain.
NOTE:WhenredundantLRUsareinterchangedintheairplaneandarekeptinthenew
position,theymustbeconguredagain.RefertoGarminG3000IntegratedAvionics
System-Adjustment/T est.
(a)IftheproblemfollowstheLRU,replacetheLRUandchecksystemoperationagain.
(b)IftheproblemdoesnotfollowtheLRU,thereisawiringbundle,coaxial,antennaor
conguration/softwarefault.Continuetroubleshootingthesystemfault.Ifnecessary,
contactCessnaCustomerService.Forcontactinformation,refertotheIntroduction.
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MODEL525B
MAINTENANCEMANUAL
3.SoftwareUploadTroubleshooting
NOTE:Forsoftware/congurationuploadproceduresinthestepsthatfollowrefertoGarminG3000
IntegratedAvionicsSystem-Adjustment/Test.
A.Softwaredoesnotupload(DualLRUinstallation).
(1)LRU1doesnotloadsoftware.
(a)DisengagethenengagetheLRU1circuitbreaker.
(b)RepeatsoftwareloadingforLRU1.
(c)Ifsoftwarestillfailstoloadcontinuetroubleshooting.
(d)DisengagetheLRU2circuitbreaker.
(e)Continueloadingsoftwarefromthepointoffailure.
(f)AllowtheLRU1softwaretoloadandtheLRU2softwareloadtofail.
(g)EngagetheLRU2circuitbreaker.
(h)DisengagetheLRU1circuitbreaker.
(i)WhenLRU2hasloadedengagetheLRU1circuitbreaker.
(j)Ifsoftwarestillfailstoloadcontinuewiththenextstep.
(2)SwaptheLRUpositions.
(3)LoadsoftwaretoLRU1.
(a)Ifthesoftwaredoesn'tuploadtheLRUisnotserviceable.
(b)IfthesoftwareuploadstroubleshoottheLRU'soriginalpositionsystemwiring.
B.Softwaredoesnotupload(singleLRUinstallation).
(1)CyclepowertotheLRUwhichisnottakingthesoftwareload.
(2)RepeatsoftwareloadingattheaffectedLRU.
(3)Ifsoftwarestillfailstoloadcontinuetroubleshooting.
(4)ForasingleinstalledLRUdoacheckofthewiring.RefertoWiringTroubleshooting.
(5)IfthewiringisserviceablereplacetheLRUandtrythesoftwareloadagain.
C.SoftwaredoesnotloadtotheGIA63WorGSD41units.
(1)CyclepowertotheLRUwhichisnottakingthesoftwareload.
(2)RepeatsoftwareloadingattheaffectedLRU.
(3)Ifsoftwarestillfailstoloadcontinuetroubleshooting.
(4)Navigatetothecongpage.RefertoGarminG3000IntegratedAvionicsSystem-Adjustment/
Test.
(5)UsethePFDsoftkeytoremovethecheckmarksfromallsoftwareandcongurationboxes.
(6)UsethePFDsoftkeytochecktheGIAandGSD.
(7)PushtheLoadsoftkeytoloadsoftwaredirectlytotheGIAandGSD.
(8)Exitthesoftwareloadingscreenandnavigatetoanyothercongpage.
NOTE:ThisforcesthePFDtorecheckSWversionsloadedtotheLRUs.)
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CESSNAAIRCRAFTCOMPANY
MODEL525B
MAINTENANCEMANUAL
GARMING3000INTEGRATEDAVIONICSSYSTEM-ADJUSTMENT/TEST
1.General
A.ThissectiongivestheprocedurestouploadtheGarminG3000softwareandcongurationles.For
moredataapplicabletotheModel525BG3000softwareandcongurationuploadingprocedures,
refertoSection6andSection8ofthemostcurrentrevisionoftheGarminG3000IntegratedAvionics
SystemLineMaintenanceManualP/N190-01785-00,foundintheIntroduction,SupplierPublication
List.
B.GarminG3000IntegratedAvionicsSystemlinereplaceableunits(LRUs)donotneedsoftwareor
congurationlesuploadedthatareremovedandinstalledagaininthesameairframeposition(same
location).GarminLRUsmusthavesoftwareandcongurationlesuploadedwhentheconditionsthat
followoccur:
•GarminLRUsthatarereplaced
•GarminLRUsthatareswappedinairframepositionorinadifferentlocation
•Fortroubleshootingandtorestorecorrectoperationoftheaffectedsystem.
C.ThesoftwareuploadandtheG3000congurationlesystemuploadproceduresaregiveninthis
sectionfortheGarmindisplayunits(GDUs)andtheGarminT ouchscreenControlUnits(GTCs).The
GDUsincludethepilot'sandcopilot'sPrimaryFlightDisplays,LPFDandRPFD(PFD1andPFD2),
respectively,theMultifunctionDisplay(MFD),andthepilot'sandcopilot'sTouchscreenControlUnits
LGTCandRGTC(GTC1andrightGTC2),respectively.ThissectionalsogivestheG3000system
LRUandoptionalsystemLRUsoftwareandcongurationlesuploadprocedures.
D.TheGTC570ControllerUnits(GTCs)andthePFDsandMFDareusedinthesoftwareand
congurationuploadprocedures.Eachdisplayunithassecuredigital(SD)cardslotsinthetop
rightportionofthedisplaybezel.TheSDcardsareinsertedforthesoftware/congurationuploads.
RefertoFigure502.FormoredataapplicabletotheGTCs,PFDs,andMFDrefertoGarminG3000
IntegratedAvionicsSystem-DescriptionandOperation.
E.Eachsystemsoftwareloadorcongurationuploadprocedurecanberepeateduptovetimesdue
toafailedorcancelleduploadpromptmessage.Donotcancelasoftwareuploadthatisinprogress,
letthesystemeithersuccessfullyloadorfail.Ifveattemptshavebeencompletedpleasecontact
CessnaCustomerCareforfurtherassistance.Forcontactinformation,refertotheIntroduction.
F.TheG3000receiveselectricalpowerdirectlyfromtheelectricalbusses.TheG3000PFDs,MFD,
GTCs,andsupportingsub-systemsincludebothpower-onandcontinuousbuilt-intestfeaturesthat
checktheprocessor,RAM,ROM,externalinputs,andoutputstoprovidesafeoperation.During
systeminitializationtestannunciationsareshownoneachofthetwoPFDsandtheMFD.Allsystem
annunciationsshouldtypicallydisappearwithintherstminuteofpower-up.WhentheG3000system
isenergizedtheannunciatorlightsontheAFCSControllermomentarilycomeonandthePFDandthe
AHRSinitializeanddisplayAHRSALIGN:KeepWingsLevel.TheAHRSshoulddisplayvalidattitude
andheadingeldstypicallywithinseveralminutesafterpower-up.TheAHRScanalignitselfwhile
taxiingandduringlevelight.Uponpower-up,eachofthetwoGTCsshowtheinitializationpageon
thedisplay.WheninitiallyenergizedtheMFDSplashScreenshowsthedatathatfollows:(Referto
Figure501)
•SystemVersion
•Copyright
•LandDatabaseNameandVersion
•SafeTaxiDatabaseInformation
•TerrainDatabaseNameandVersion
•ObstacleDatabaseNameandVersion
•NavigationDatabaseName,Version,andEffectiveDates
•AirportDirectoryName,VersionandEffectiveDates
•Flitecharts/ChartviewDatabaseInformation.
G.ToolsandEquipment
(1)ToolsandEquipment
•GarminG3000,Cessna525Bsoftwareloadercard
•CessnaG3000DefaultPilotProlesoftwareloadercardNOTE
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CESSNAAIRCRAFTCOMPANY
MODEL525B
MAINTENANCEMANUAL
A94875
6310T1168
A6314P1879
B6314P1879
C6314P1879
AA6318T1848
DETAIL B
MFD POWER UP SCREEN
DETAIL A
PFD INITIALIZATION SCREEN
A
A
A
B
A
C
VIEW A-A
DETAIL C
PFDandMFDPowerOnScreens
Figure501(Sheet1)
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MODEL525B
MAINTENANCEMANUAL
A94876
6310T1168
A6314T1881
B6314T1881
RIGHT OUTER
KNOB
A
DETAIL A
RIGHT INNER
KNOB
SECURE
DIGITAL
CARD SLOTS
PFD (NOTE)
SOFTKE
PFD SHOWN, MFD IDENTICAL
DETAIL B
NOTE:
B
GDUandGTCSoftwareUploadFunctionsandControls
Figure502(Sheet1)
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MODEL525B
MAINTENANCEMANUAL
•CMCsoftwareloadercardNOTE
•PurchasedOptionUnlocksoftwareloadercard(s)ifapplicable
•CessnaCDMSMaintenancecardNOTE
•TOLDDatbasecard(ifsoftwareversionis3.2(006-B1814-10)orlater.)
NOTE:Softwareversionpriorto3.2(006-B1814-10)thesoftwareisavailablefordownloadat
www.txtavsupport.com.Softwareversion3.2(006-B1814-10)andlaterthesoftwaremustbe
orderedfromTextronAviation.
H.Hereisalistingoftheproceduresinthissectionintheordertheyappearinthissection:
(1)General
(2)AirplaneSetup
(3)CompleteSoftwareLoadingOverview
(4)CongurationLoadingOverview
(5)OptionsActivationOverview
(6)OptionsRemovalOverview
(7)LRUReplacementOverview
(8)DiagnosticDataWirelessTransmitSettings
(9)SoftwareLoadingCongurationMode
(10)StandardCongurationMode
(11)UpdateSystemFiles
(12)BaseSoftware/CongurationLoadProcedures
(13)UpdateCustomGraphics
(14)DiagnosticConguration
(15)AirplaneOptionsInstallation
(16)CongurationModulePrograming
(17)CongurationManagement
(18)AirplaneConguration
(19)DefaultPilotProleLoadingProcedures
(20)Verication
(21)DatabaseCardLoadingProcedures
(22)TOLDDatabase
(23)ReloadConguration(OptionsRemoval)Procedures
(24)LRUReplacementSoftwareUploadProcedures
2.AirplaneSetup
A.Theairplanesetupmustbecompetedpriortoloadingorverifyinganysoftwareloads.
(1)Makesureexternalelectricalpowerisconnectedtotheairplaneandadjustedtosupply28VDC
+0.5or-0.5VDC.
(2)SettheBATTERYswitchtotheONposition.
(3)Makesurethatthecircuitbreakersthatfollowareengaged.
LRUCBNameModel525Requirement
NAVIAU1CoreComponent
GIA-63W#1COM1CoreComponent
NAVIAU2CoreComponent
GIA-63W#2COM2CoreComponent
GSD-41#1DCU1CoreComponent
GSD-41#2DCU2CoreComponent
GEA-71H#1ENGINEINTER1CoreComponent
GEA-71H#2ENGINEINTER2CoreComponent
GMA-36#1AUDIO/MKR1CoreComponent
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LRUCBNameModel525Requirement
GMA-36#2AUDIO/MKR2CoreComponent
GTX3000#1XPDR1CoreComponent
GTX3000#2XPDR2CoreComponent
GDC7400#1ADC1CoreComponent
GDC7400#2ADC2CoreComponent
GCU-275#1LDISPLAYCONTROLCoreComponent
GCU-275#2RDISPLAYCONTROLCoreComponent
GMC-710AFCSCONTCoreComponent
ServosAFCSCoreComponent
GTS8000TCASCoreComponent
GWX-70RADARCoreComponent
GRS77#1AHRS1CoreComponent
GRS77#2AHRS2CoreComponent
GSR-56#1TELEPHONE1OptionalSystem
GSR-56#2TELEPHONE2OptionalSystem
GDL-59CABINPHONEHANDSETOptionalSystem
GDR-66VHFDATALINKOptionalSystem
GDL-69AXMDATALINKOptionalSystem
NOTE:Thecircuitbreakersfortheoptionalsystemsmustbeengagedifthesystemisinstalled.
3.CompleteSoftwareLoadingOverview
A.General
(1)ThissectiongivesthesequentialorderStepsnecessarytocompletetheGarminG3000
CompleteSoftwareLoadingprocedureandisnecessarytobecompletedwhentheinstalled
aircraftsystemsoftwareisnotthecorrectsoftwareload.
(2)TheGarminG3000BaseSoftwareCompleteSoftwareLoadingiscomposedofthestepsas
giveninT able501.
Table501.CompleteSoftwareLoadingProceduresOverview
St-
ep
CompleteSoftwareLoadingRequiredor
Conditional
2AirplaneSetupRequired
8DiagnosticDataWirelessTransmitSettingsRequired
11UpdateSystemFilesRequired
12BaseSoftware/CongurationLoadProceduresRequired
13UpdateCustomGraphicsRequired
14DiagnosticCongurationRequired
15AirplaneOptionsInstallationRequired
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CESSNAAIRCRAFTCOMPANY
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MAINTENANCEMANUAL
Table501.CompleteSoftwareLoadingProceduresOverview(continued)
St-
ep
CompleteSoftwareLoadingRequiredor
Conditional
18AirplaneCongurationRequired
16CongurationModuleProgramingRequired
17CongurationManagementRequired
19DefaultPilotProleLoadingProceduresRequired
20VericationRequired
21DatabaseCardLoadingProcedures(Fornewsoftwareloadsonly)Required
22TOLDDatabaseRequired
4.CongurationLoadingOverview
A.General
(1)ThissectiongivesthesequentialorderStepsnecessarytocompletetheGarminG3000
CongurationLoadingprocedureandisnecessarytobecompletedwhenthebaseconguration
mustbereachedfortroubleshootingorotherreasonsasgiveninTable502.
Table502.CongurationLoadingProcedures
St-
ep
CongurationLoadingRequiredor
Conditional
2AirplaneSetupRequired
8DiagnosticDataWirelessTransmitSettingsRequired
23ReloadConguration(OptionsRemoval)ProceduresRequired
14DiagnosticCongurationRequired
15AirplaneOptionsInstallationRequired
18AirplaneCongurationRequired
16CongurationModuleProgramingRequired
17CongurationManagementRequired
19DefaultPilotProleLoadingProceduresRequired
20VericationRequired
21DatabaseCardLoadingProceduresRequired
22TOLDDatabaseRequired
5.OptionsActivationOverview
A.General
(1)ThissectiongivesthesequentialorderStepsnecessarytocompletetheGarminG3000Options
ActivationprocedureasgiveninT able503.
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Table503.OptionsActivationProcedures
St-
ep
OptionsActiviationRequiredor
Conditional
2AirplaneSetupRequired
15AirplaneOptionsInstallationAdded
optionsonly
16CongurationModuleProgramingRequired
17CongurationManagementRequired
20VericationRequired
6.OptionsRemovalOverview
A.General
(1)ThissectiongivesthesequentialorderStepsnecessarytocompletetheGarminG3000Options
Removalprocedure.
(2)ThissectiongivesthesequentialorderofadjustmentsandtestsnecessaryfortheAircraftOption
Removal/DisableSoftwareCongurationProcedure.
(3)Completionofthissectionisnecessarywhenanoptionisremovedorneedstobedisabledfrom
theairplane.
(4)TheAircraftOptionRemoval/DisableSoftwareCongurationProcedureiscomposedofthe
stepsasgiveninT able504.
Table504.OptionsRemovalProcedures
St-
ep
OptionsRemovalRequiredor
Conditional
2AirplaneSetupRequired
8DiagnosticDataWirelessTransmitSettingsRequired
23ReloadConguration(OptionsRemoval)ProceduresRequired
14DiagnosticCongurationRequired
15AirplaneOptionsInstallationRequired
16CongurationModuleProgramingRequired
17CongurationManagementRequired
19DefaultPilotProleLoadingProceduresRequired
20VericationRequired
21DatabaseCardLoadingProceduresRequired
22TOLDDatabaseRequired
7.LRUReplacementOverview
A.General
(1)ThissectiongivesthesequentialorderStepsnecessarytocompletetheGarminG3000LRU
ReplacementprocedureasgiveninTable505.
(2)CompletionofthissectionisnecessarywhenaGarminLRUcomponentisreplacedoris
swappedfromonepositiontoanotherposition.
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Table505.LRUReplacementProcedures
St-
ep
LRUReplacementRequiredor
Conditional
2AirplaneSetupRequired
8DiagnosticDataWirelessTransmitSettingsRequired
11UpdateSystemFilesRequiredif
GDUwas
replaced
24LRUReplacementSoftwareUploadProceduresRequired
13UpdateCustomGraphicsRequiredif
GDUwas
replaced
14DiagnosticCongurationRequired
16CongurationModuleProgramingRequired
17CongurationManagementRequired
18AirplaneCongurationRequired
19DefaultPilotProleLoadingProceduresRequiredif
MFDwas
replaced
20VericationRequired
21DatabaseCardLoadingProceduresRequired
22TOLDDatabaseRequiredif
GTCwas
replaced
8.DiagnosticDataWirelessTransmitSettings
A.FromtheGTCHomepage,selectasfollows:Home>AircraftSystems>Maintenance>Start
Maintenance.
B.EntertheMaintenancepassword:CACCDMSandpressENTER.
C.FromtheMaintenancepage,selectasfollows:Maintenancepage>CMCLOGS>FAULTS.
D.OntheFaultspage,selecttheFOLDERoptionsandllinTable506withthedatafromFAULTS-
OPTIONSGTC.
Table506.OperatorTransmitPreferences
CMCFolderTxTypeTxMode1TxMode2TxMode3TxMode4
Faults
LHService
Messages
RHService
Messages
LHEngine
Exceedances
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