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[BLUEMAXINSTALLATIONINSTRUCTIONS] i
BlueMAXBluetoothAdapter
InstallationInstructions
Documentno.2456-05
Date:2017-06-07
Revision5
Approved:
Control-JPty.Ltd.100HursleyRd.RedbankNSW2446Australia
ii [BLUEMAXINSTALLATIONINSTRUCTIONS]
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Copyright©2017Control-JPty.Ltd.
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RevisionHistory
Date Revision Document Changes
2017-02-17 1 InitialDraft
2017-02-22 2 Reviseddocumentlist
2017-02-22 3 PlacardCB;Flightmanualsupplement
2017-04-13 4 Minorcorrectionstowiringinstructions
2017-06-07 5 Additionalinformationonwiringandconnectoridentification.
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TableofContents
1 Introduction.........................................................................................................................................................................61.1 TheBlueMAXmodule.....................................................................................................................................................61.2 Applicability.......................................................................................................................................................................6
2 Definitions.............................................................................................................................................................................63 Specifications.......................................................................................................................................................................74 ReferencedDocuments....................................................................................................................................................75 Powerrequirements.........................................................................................................................................................76 Preparationforinstallation...........................................................................................................................................76.1 Aircraftidentification....................................................................................................................................................76.2 Connectoridentification...............................................................................................................................................76.3 VerifyingpresenceofSIU..............................................................................................................................................9a) MissingconnectorsinSIUaircraft...................................................................................................................................10
6.4 VerifyprimaryenginedataonPFDforDAUaircraft...................................................................................107 InstallationwithMFDpermanentlyremoved....................................................................................................118 Partsrequired...................................................................................................................................................................129 Toolsrequired..................................................................................................................................................................129.1 ProbingconnectorP1426B......................................................................................................................................12
10 Installationprocedure................................................................................................................................................1310.1..SIUaircraft-iftheMFDhasbeenpermanentlyremoved...........................................................................1310.2..SIUaircraft–withMFDfitted.................................................................................................................................1310.3..DAUG2Aircraft.............................................................................................................................................................1410.4..G3Aircraft........................................................................................................................................................................14
11 Postinstallchecks........................................................................................................................................................1412 Weightandbalance.....................................................................................................................................................1513 FlightManualSupplement.......................................................................................................................................1514 Logbookentry................................................................................................................................................................1515 Instructionsforcontinuedairworthiness.........................................................................................................1516 RemovaloftheBlueMAXinstallation..................................................................................................................1517 Technicalsupport.........................................................................................................................................................15
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ListofTables
Table1:BlueMAXTechnicalspecifications............................................................................................................7
Table2:ReferencedDocuments..................................................................................................................................9
Table3:Enginemonitortypes..................................................................................................................................11
Table4:BlueMAXpartnumbers..............................................................................................................................12
ListofFigures
Figure1Connectorlocations........................................................................................................................................8
Figure2:Analogengineinstruments.....................................................................................................................10
Figure3:PrimaryenginedataonPFD...................................................................................................................11
Figure4:ProbingP1426B...........................................................................................................................................13
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1 Introduction1.1 TheBlueMAXmoduleTheBlueMAXmodulecapturesserialdatafromanAvidyneenginemonitoringsystemandstreamsitviaBluetoothLowEnergytoportabledevices.Thisenablessupplementaryenginedatatobedisplayedandloggedonaportabledevice.
TheBlueMAXinstallationisnotintendedtoreplaceprimaryengineinstruments.
Optionally,themodulemayalsobeconnectedtotheserialGPSdatatransmittedbythe#1GPSnavigatortotheMFD,providingnavigationdatatotheportabledeviceviaBluetoothtoenablecalculationssuchasfuelatdestination.
1.2 ApplicabilityTheBlueMAXmoduleisintendedforinstallationintoaircraftalreadyfittedwithanAvidyneenginemonitoringsystem,utilizingeitheraDataAcquisitionUnit(DAU)oraSerialInterfaceUnit(SIU.)ThemajorityofsuchinstallationsareinCirrusSR22andSR20aircraft,andtheseinstructionsrelatespecificallytothosemodels.
2 DefinitionsThefollowingabbreviationsandacronymsareusedinthisdocument:
BLE BluetoothLowEnergy–theradioprotocolusedbytheBlueMAXmodule,operatingat2.4GHz.
DAU DataAcquisitionUnit–oneofthetwointerfacemodulesusedbyAvidynetocollectanalogenginedataandconverttoRS-232serialdata.
SIU TheotherAvidyneinterfacemodule,usedonolderaircraft.
DTU DataTransferUnit–amoduleinstalledinG3aircraftwhichcollectsaircraftdataandtransmitsittoaloggingmodule.
EMAX Avidyne’sproductnamefortheenginemonitoringsystem.
MFD MultiFunctionDisplay–apanel-mounteddisplayusedtodisplaynon-flight-criticaldata,includingsupplementaryenginedata.
EX5000 TheAvidyneMFDinstalledinCirrusSR22andSR20aircraft.
PFD PrimaryFlightDisplay–apanelmounteddisplayforflight-criticalinformation.
RS-232 Aserialdataformatusedforlow-speedcommunicationbetweenelectronicdevices.
AMM TheCirrusAircraftMaintenanceManual(seeTable2:ReferencedDocuments.)
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3 SpecificationsSize(moduleonly) 55.2x52x19mm
Weight(installed,includingharness) Lessthan100g
Voltage 5-35VDC
Current Maximum:10mA;Average:2mA
Transmissionprotocol BluetoothLowEnergy(2.4GHz)
Transmissionpower(peak) 4dBM(2.5mW)
Table1:BlueMAXTechnicalspecifications
4 ReferencedDocumentsThedocumentsreferredtointheseinstructionsarelistedinTable2:ReferencedDocuments.
5 PowerrequirementsTheBlueMAXmoduledrawsamaximumofonly10mAandmaybesuppliedfromanexistingbreaker.ItisrecommendedthatitbesuppliedfromtheconveniencepowerbreakerCB638(5Aor3Adependingonaircraftconfiguration)onthenon-essentialbus.AllpowerwiringtotheBlueMAXadaptershouldbe22AWG,whichisratedto5AperAC43.13-1B,orheavier.
6 Preparationforinstallation6.1 AircraftidentificationCirrusaircraftfittedwithPerspectiveavionicsarenoteligibleforBlueMAXinstallation.
CirrusaircraftfittedwithAvidyneEMAXenginemonitoringfallintotwogeneralcategories–thosefittedwithanSIUorthosefittedwithaDAU.SIUsarefittedonlytoearlyserialnumbersandcanbeidentifiedbythepresenceofanalogengineinstrumentsontherighthandsideoftheinstrumentpanel.NotethatthattheSIUwasanoption,andmaynotbefittedtoallapplicableaircraft.LaterAvidyne-equippedaircraftdonothavetheanaloginstrumentsonthepanel(thereisagloveboxinthelocationwheretheengineinstrumentswere)andalltheseaircraftarefittedwithaDAU.TheDAUprovidestwoRS-232outputs,onefeedstheMFDandisusedforconnectiontotheBlueMAXmodule,andtheotherfeedsthePFDwhichdisplaystheprimaryengineinstrumentation.
6.2 ConnectoridentificationConnectorsinstalledbyCirrusaregenerallywelllabeled,butnotethatthereisapeculiaritywiththenomenclatureused–connectorswithmalepins(whichwouldnormallybecalled“plugs”)arecalledjacksandlabeledasJnnnandconnectorswith
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femalepins(whichwouldnormallybecalled“sockets”or“jacks”)arecalledplugsandlabeledasPnnn.
IfconnectionistobemadetoGPSdatafromthe#1GPSonwireANGP543-22,thisislocatedinJ518(mostaircraft)orJ517(serialnumbers22-0434andearlier,and20-1336andearlier.)RefertotheCirruswiringmanualforfurtherinformation.
J518carriesRS-232GPS#1(wireANGP543-22)dataonpin9.J518isaD-Subplug(i.e.malepins)whichconnectstoP518,whichismountedonthetoprightoftheradiorack,belowtheMFDopening.J518issecuredbyaslide-locksoisrelativelyeasytoremove,buttheremaybeothercablesinthewaythatwillhavetobedisconnectedtoaccessit.
P1047andJ1047arepresentinG3aircraftonly,andarelocatedforwardoftheMFD.Theyusemetalbackshellswithslide-lockcoupling.
P1426andJ1426arelocatedinthesamearea,andarefoundinallDAUaircraft.Theyhaveplasticbackshellsandjackscrewcoupling.SeeFigure1Connectorlocations.Bothpairsofconnectorsareunpluggedfromeachotherinthisimage.Theremaybevariationsinthehardwareindifferentaircraft,butallshouldbelabeled–verifyidentificationbycheckingthelabels.
Figure1Connectorlocations
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Title Documentnumber
Rev Date
Internaldocuments
SIUharness 2350-07 3 2017-02-22
P528harness 2350-06 2 2017-02-20
DAUharness 2350-08 3 2017-06-06
G3harness 2350-11 3 2017-06-06
J719-P719Wiring 2530-17 1 2017-06-07
BlueMAXinstallation–SIU 2350-09 1 2017-02-15
BlueMAXinstallation–DAUG2 2350-10 1 2017-02-15
BlueMAXinstallation–DAUG3 2350-12 1 2017-02-16
BlueMAXinstallation-MFDremoved 2530-13 1 2017-02-17
BlueMAXmodule–circuit 2530-16 3 2017-02-22
BlueMAXmodule-mechanical 2350-01 2 2017-02-22
Externaldocuments
AIRPLANEWIRINGMANUALFORTHECIRRUSSR22ANDSR22T
13775-001 D4 2016-01-01
AIRPLANEWIRINGMANUALFORTHECIRRUSSR20
12129-001 C5 2016-01-01
AIRPLANEMAINTENANCEMANUALFORTHECIRRUSSR20
12137-001 B7 2016-01-01
AIRPLANEMAINTENANCEMANUALFORTHECIRRUSSR22ANDSR22T
13773-001 B6 2016-01-01
ACCEPTABLEMETHODSTECHNIQUES,ANDPRACTICES⎯AIRCRAFTINSPECTIONANDREPAIR
AC 43.13-1B
1 1998-09-08
Table2:ReferencedDocuments
6.3 VerifyingpresenceofSIUIftheaircraftisfittedwithanalogengineinstrumentsasshowninFigure2:Analogengineinstruments,confirmthepresenceofanSIUeitherbyverifyingthattheMFDdisplaysenginedataontheEnginepage,orvisuallyconfirmthepresenceofanSIUmountedontheco-pilotsidekickpanel(belowtheanalogengineinstruments.)Referto
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theCirrusAMMchapter77-40.IftheaircrafthasanalogengineinstrumentsandnoSIUtheBlueMAXmodulecannotbeinstalled.
a) MissingconnectorsinSIUaircraftTheSIUserialdataisconnectedfromtheSIUtotheMFDbycableANMD977-22(refertoCirrusWiringManualchapter77-00-01)andinSR22swithserialnumbers1087andabove,andSR20swithserialnumbers1456andabove,thiscableincorporatesapairofconnectorslabelledJ719/P719whichprovidesaconvenientplacetoinserttheadapterharnessp/n4370-03.AircraftwithserialnumbersbelowthoserangesmaynothaveJ719/P719fittedandinstallationofBlueMAXwillbefacilitatedifthoseconnectorsareinstalledinaccordancewiththeCirrusWiringManualchapter77-00-01.ThenecessaryconnectorscanbeorderedfromControl-Jaspartnumber4370-9869anddrawing2530-17providesadditionalguidance.
Figure2:Analogengineinstruments
6.4 VerifyprimaryenginedataonPFDforDAUaircraftDAUequippedaircraftdisplayprimaryenginedataonthePFD,butthisrequiresthatthesoftwareversioninstalledonthePFDsupportsthisdisplay.Toverifythis,poweruptheaircraftandinspectthelowerrightareaofthePFD.ThereshouldbeadatablockwithprimaryenginedataasshowninFigure3:PrimaryenginedataonPFD.Ifthisdataisabsent,thePFDsoftwaremustbeupgradedbeforeinstallingBlueMAX.
Theapplicableaircraftmodels,serialnumbersandconfigurationsaresummarisedinTable3:Enginemonitortypes.
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Figure3:PrimaryenginedataonPFD
Model Serialnumbers Interfacetype Notes
G1/G2SR22 0002-1601,1603-1643and1645-1662
SIU SIUmustbefitted.
G2SR22 1602,1644,1663-2437
DAUG2 VerifyprimaryenginedatadisplayedonPFD
G3SR22(withAvidyneAvionics)
2438andsubsequent
DAUG3 VerifyprimaryenginedatadisplayedonPFD
G1/G2SR20 1005-1581 SIU SIUmustbefitted.
G2SR20 1582-1877,1879-1885
DAUG2 VerifyprimaryenginedatadisplayedonPFD
G3SR20(withAvidyneAvionics)
1878,1886&subsequent
DAUG3 VerifyprimaryenginedatadisplayedonPFD
Table3:Enginemonitortypes
7 InstallationwithMFDpermanentlyremovedIftheMFDhasbeenpermanentlyremovedfromtheaircraft,analternativeinstallationmethodistoconnecttheBlueMAXmoduletothenowunusedMFDconnector.ThisconnectorisshownintheCirrusWiringManualasP528.Thisprovidesserialengine
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data,serialGPSdata(SIUaircraftonly)andpowerinasingleconnector.Anadapterharnessp/n4370-9630isavailabletoplugdirectlyintoP528.
InstallationinDAUequippedaircraftwillbethesameregardlessofwhethertheMFDisfittedornot,astheMFDconnectorP528inDAUequippedaircraftdoesnotreceiveGPSdataoverRS232,soconnectionviaP528isnotrecommended.
8 PartsrequiredInstallationofBlueMAXrequirestheBlueMAXmoduleandanadapterharnesswhichconnectsittotheaircraftwiring.TheharnessforSIUandDAUaircraftaredifferent–orderthecorrectpartsaslistedinTable4:BlueMAXpartnumbers.ThekitpartnumbersincludetheBlueMAXmoduleandtheappropriateharnessandconnectors(wherenecessary.)Inaddition,theremaybecableties,wire,splicesandothercommonelectricalpartsrequired–thesearenotincludedinthekit.
Installationtype BlueMAXmodule
AdapterHarness
Connectors Kit
SIU 4370-2730 4370-5146 N/A 4370-8012
SIU(J719/P719notpresent)
4370-2730 4370-5146 4370-9869 4370-1477
DAUG2 4370-2730 4370-2720 N/A 4370-4451
DAUG3 4370-2730 4370-8434 N/A 4370-4734
SIUwithMFDpermanentlyremoved
4370-2730 4370-9630 N/A 4370-5604
Table4:BlueMAXpartnumbers
9 ToolsrequiredForpostinstallationcheckoutaBLEscannerwillberequired.BLEscannersareavailableasappsforinstallationonAndroidoriOSportabledevices.
Standardtoolswillberequired.
9.1 ProbingconnectorP1426BIfitisrequiredtoprobetheconnectorP1426B(thisistheonethatplugsintotheBlueMAXmodule)toconfirmcontinuityormeasurepowersupplyvoltage,doNOTinsertaprobeintothepinopeningasthiswilldamagetheterminal.Useafineprobe(0.66mmorsmaller)intheprobeopeningbelowthepinopening–seeFigure4:ProbingP1426B.
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Figure4:ProbingP1426B
10 InstallationprocedureInstalltheBlueMAXsysteminaccordancewithoneofthefollowingprocedures.AllwiringshouldbeperformedinaccordancewithAC43.13-1B.
10.1 SIUaircraft-iftheMFDhasbeenpermanentlyremoveda) GainaccessbehindtheinstrumentpanelthroughtheopeningwheretheMFD
waspreviouslyfitted.b) PlugP528adapterharnessp/n4370-9630intotheMFDconnectorP528.c) PlugtheBlueMAXmoduleintotheotherendoftheadapterharness.d) Securethemoduleandcablingtoexistingstructureorwirebundlesusingcable
ties.
10.2 SIUaircraft–withMFDfitted.a) RemoveMFDtogainaccessbehindtheinstrumentpanel.b) LocateP719andJ719.IfthesearenotfittedlocatewireANMD977-22running
fromtheSIUtotheMFD,andinstallP719andJ719inaccordancewiththeCirrusWiringManual.Control-Jdrawing2530-17isavailableforguidanceontheconnectorwiring.
c) DisconnectP719andJ719fromeachotherandre-connecttotheSIUharnessp/n4370-5146.
d) IfGPSdataistobeconnectedtotheBlueMAXmodule,locatewireANGP543-22whichrunsfromGPS1totheMFDandsplicethesignalwiretotheinneroftheshieldedwireprovidedintheadapterharness.Toavoidanearthloopdonotconnecttheshieldstogether(theshieldisearthedattheBlueMAXmoduleend.)
e) IfGPSdataisnottobeconnected,capandstowtheshieldedcable,orremovefromtheBlueMAXconnector.
f) RunthepowerwireintheSIUharnesstothecircuitbreakerpanelandterminatetotheconveniencepowerbreakercurrentlylabeled“12VDCOUTLET”.Relabelthebreaker“12VDCOUTLET/BLUETOOTH”.
g) PlugtheBlueMAXmoduleintotheotherendoftheadapterharness.h) Securethemoduleandcablingtoexistingstructureorwirebundlesusingcable
ties.
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i) ReplaceMFDIAWtheCirrusAMM.
10.3 DAUG2Aircrafta) RemoveMFDtogainaccessbehindtheinstrumentpanel.b) LocateP1426andJ1426.ThesewillbedirectlybehindtheMFD.Disconnect
P1426andJ4126fromeachotherandre-connecttotheDAUharnessp/n4370-2720.
c) IfGPSdataistobeconnectedtotheBlueMAXmodule,locateconnectorpairP518/J518(atthetoprightoftheradiorack)disconnect,andremovethebackshellfromJ518.Pin9inJ518shouldbeempty.
d) Theadapterharnesshasashieldedwireattachedterminatedwithapre-crimpedmalepin.InsertthispinintoJ518inthepin9position.
e) ReplacethebackshellonJ518,securingallcables.ReconnectJ518toP518.f) IfGPSdataisnottobeconnected,capandstowtheshieldedcable,orremove
fromtheBlueMAXconnector.g) RunthepowerwireintheDAUharnesstothecircuitbreakerpaneland
terminatetotheconveniencepowerbreakercurrentlylabeled“12VDCOUTLET”.Relabelthebreaker“12VDCOUTLET/BLUETOOTH”.
h) PlugtheBlueMAXmoduleintotheotherendoftheadapterharness.i) Securethemoduleandcablingtoexistingstructureorwirebundlesusingcable
ties.j) ReplaceMFDIAWtheCirrusAMM.
10.4 G3Aircrafta) RemoveMFDtogainaccessbehindtheinstrumentpanel.b) LocateP1047andJ1047.ThesewillbedirectlybehindtheMFD.Disconnect
P1047andJ1047fromeachotherandre-connecttotheG3harnessp/n4370-8434.
c) RunthepowerwireintheDAUharnesstothecircuitbreakerpanelandterminatetotheconveniencepowerbreakercurrentlylabeled“12VDCOUTLET”.Relabelthebreaker“12VDCOUTLET/BLUETOOTH”.
d) PlugtheBlueMAXmoduleintotheotherendoftheadapterharness.e) Securethemoduleandcablingtoexistingstructureorwirebundlesusingcable
ties.f) ReplaceMFDIAWtheCirrusAMM.
11 Postinstallchecks• Poweruptheaircraftandverifythattheanaloginstruments(iffitted)orthePFD
displayprimaryenginedata.• VerifythattheMFD(iffitted)displayssupplementaryenginedata.• UsingaBLEscannerverifythattheBlueMAXmoduleisadvertising(thedefault
devicenameisEMAX.)Thisconfirmsthatthemoduleispoweredup.Pullthebreakersupplyingthemoduleandconfirmthatitstopsadvertising.
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12 WeightandbalanceTheinstalledweightoftheBlueMAXadapterandharnessisapproximately80g(lessthan3ounces)andresultsinachangeintheCGpositionofapproximately0.008%MAC.ThisisconsideredanegligiblechangeperAC43.13-1Bandnoweightandbalanceupdateisrequired.
13 FlightManualSupplementCompletetherequiredinformationontheprovidedFlightManualSupplementandinsertitintotheaircraftFlightManualorPOH.
14 LogbookentryMakeasuitablelogbookentrydocumentingtheinstallation.
15 InstructionsforcontinuedairworthinessNoroutinemaintenanceorinspectionoftheBlueMAXmoduleisrequired.Correctdisplayofprimaryandsupplementaryenginedatashouldbemonitoredduringnormaloperation.
16 RemovaloftheBlueMAXinstallationFortemporaryremoval,disconnectthemodulefromP1426Bandremoveit.Forpermanentremoval,removetheadapterharness,andreconnectP719/J719,P1407/J1407orP1426/P1426asappropriate,inaccordancewiththeCirrusWiringManual.
17 TechnicalsupportForassistancewithinstallationissuesorforserviceorreplacementparts,contactControl-Jviaemailadmin@control-j.com.
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