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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CESSNAAIRCRAFTCOMPANY
AIRCRAFTDIVISION
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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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CESSNAAIRCRAFTCOMPANY
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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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