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Redmond, WA 060-4314-082 Rev -
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This document and all information and expression contained herein are the property of Honeywell International Inc., and is provided to the recipient in confidence on a “need to know” basis. Your use of this document is strictly limited to a legitimate business purpose requiring the information contained therein. Your use of this document constitutes acceptance of these terms.
RCD Selection Guide for the
EGPWS Runway Advisory and Awareness System (RAAS)
Drawing Number: 060-4314-082 Revision: -
Prepared by: Honeywell International, Inc.
Redmond, WA 98073-9701
This document is an unpublished work. Copyright 2013 Honeywell International Inc.
All rights reserved
Description: Released per ECO- 0202701
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TABLE OF CONTENTS
1 SCOPE ........................................................................................................................................................ 3
1.1 IDENTIFICATION ............................................................................................................................................. 3 1.2 RAAS PARAMETER SELECTION PROCESS ............................................................................................................. 3
2 APPLICABLE HONEYWELL STC DOCUMENTS ................................................................................................ 4
2.1 REFERENCE DOCUMENTS ................................................................................................................................. 5
3 HOW TO USE THIS RCD SELECTION GUIDANCE ............................................................................................ 5
3.1 COMPLIANCE WITH THE EASA RAAS CERTIFICATION REVIEW ITEM .......................................................................... 7
4 FUNCTION SELECTIONS AND DESCRIPTIONS SUMMARY ............................................................................. 8
5 RCD WORKSHEET GUIDANCE ..................................................................................................................... 10
5.1 OPERATOR INFORMATION AND SYSTEM PREFERENCES ......................................................................................... 11 5.2 RAAS ROUTINE ADVISORIES .......................................................................................................................... 16
5.2.1 Approaching Runway – In Air advisory (Product Description 4.2.1) ..................................................... 16 5.2.2 Approaching Runway – On Ground advisory (Product Description 4.2.2) ............................................ 16 5.2.3 On Runway – On Ground advisory (Product Description 4.2.3) ............................................................ 17 5.2.4 Distance Remaining – Landing and Rollout advisory (Product Description 4.2.4) ................................ 17 5.2.5 Runway End advisory (Product Description 4.2.5) ............................................................................... 19
5.3 RAAS NON ‐ ROUTINE ADVISORIES AND CAUTIONS ............................................................................................ 19 5.3.1 Approaching Short Runway – In Air advisory (Product Description 4.3.1) ............................................ 19 5.3.2 Approaching Short Runway – In Air Caution (Product Description 4.3.2) ............................................. 21 5.3.3 Insufficient Runway Length – On Ground advisory (Product Description 4.3.3) ................................... 23 5.3.4 Insufficient Runway Length – On Ground caution (Product Description 4.3.4) ..................................... 24 5.3.5 Extended Holding On Runway advisory (Product Description 4.3.5) .................................................... 26 5.3.6 Taxiway Takeoff (Product Description 4.3.6) ....................................................................................... 27 5.3.7 Distance Remaining – Rejected Takeoff advisory (Product Description 4.3.7) ..................................... 28 5.3.8 Taxiway Landing caution (Product Description 4.3.8) .......................................................................... 30
5.4 STABILIZED APPROACH MONITOR (PRODUCT DESCRIPTION 5) ............................................................................... 31 5.4.1 Landing Flap Monitor (Product Description 5.2.1) ............................................................................... 31 5.4.2 Excessive Approach Angle Monitor (Product Description 5.2.2) .......................................................... 33 5.4.3 Excessive Approach Speed Monitor – (Product Description 5.2.3) ....................................................... 34
5.5 CORRECTED ALTIMETER MONITOR (PRODUCT DESCRIPTION 6) .............................................................................. 36 5.6 TAKEOFF FLAP CONFIGURATION MONITOR (PRODUCT DESCRIPTION 7) ................................................................... 38 5.7 LONG LANDING MONITOR (PRODUCT DESCRIPTION 8) ........................................................................................ 40 5.8 VOLUME REQUIREMENTS .............................................................................................................................. 45 5.9 ADDING ADDITIONAL COMMENTS ................................................................................................................... 46 5.10 ADDITIONAL CONSIDERATIONS ........................................................................................................................ 47
6 NOTES ...................................................................................................................................................... 48
6.1 ACRONYMS AND ABBREVIATIONS .................................................................................................................... 48
APPENDIX – RCD WORKSHEET ........................................................................................................................... 49
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1 Scope
1.1 Identification
This document identifies the set of functions available in the Honeywell Enhanced Ground Proximity Warning System (EGPWS) Runway Awareness and Advisory System (RAAS). For each function, guidance is provided for selecting configuration settings stored in the Reloadable Customer Definitions (RCD) database.
The original RAAS consisted of a set of functions first introduced in software version MK V / MK VII (-218-218/-051/-002) and are referred to as “basic” functions in this document.
Additional functions were introduced in software version MK V / MK VII (-230-230/-054/-004) and are referred to as “extended” functions in this document. Extended functions include, SAM (Stabilized Approach Monitor), LL Mon (Long Landing Monitor), CAM (Corrected Altimeter Monitor), and Takeoff Flaps Monitor.
Software versions MK V / MK VII (-236-236/-057/-006) and MKV-A (-x01/-x51) were introduced to provide compliance with EASA CRI. The software update included support for RAAS Not Available/INOP, changes to Self Test level 1, and the option to inhibit CAM.
The extended version of RAAS is also known by its marketing name, SmartRunway® and SmartLanding® (SR/SL). However, it should be noted that the term “RAAS” will continue to be used on the flight deck, in the AFMS, and in the Pilot’s Guide regardless of the function set available in the installed system.
RAAS support is provided in MKV and MKVII hardware platforms and the new MKV-A platform. MKV-A software version (-x01/-x51) contains the same functionality as MK V software version (-236-236/-057/-006).
1.2 RAAS Parameter Selection Process
Honeywell, as the STC Applicant, utilizes a STC methodology that tests and certifies a wide range of possible RCD values during a First-of-Type (FOT) certification. For example, instead of certifying a single volume for an alert, a maximum volume and a minimum volume are certified. In addition, all possible functions for a specific aircraft type are certified in the ON and OFF states. This approach allows the Operator to select a new volume within the certified range or turn ON/OFF a RAAS function with minimal risk of additional certification testing.
Conducting an STC using this methodology involves the following steps:
1. Honeywell(astheApplicant)obtainsaircraftdatafromtheOperatorinordertoassessthemaximumpossiblenumberofRAASfeaturesforthespecificaircrafttype.HoneywellthenbuildsaTestRCDandconductsengineeringgroundandflighttestingwiththeOperatortodeterminemaximumandminimumvolumelevelswhiletestingotherparametervaluesasnecessary.
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2. Fromtheengineeringflighttestresults,Honeywellbuilds,andconforms,aCertificationRCDandconductsCertificationgroundandflighttestingtovalidateallRAASfunctionsmeettheirintendedfunction.FollowingthecompletionofCertificationtesting,HoneywellreceivesSTCapprovalandprovidestheSTCdatapackagetotheOperatorforinstallationaccordingtotheSTCEngineeringOrder.
3. ShouldtheOperatordecidetomodifyoneofthecertifiedRCDparameters(e.g.adjustavolumeorturnON/OFFaRAASfunction),they(withtheassistanceoftheApplicantasnecessary)wouldcompleteanewRCDWorksheetusingthisRCDSelectionGuide.NotethatthisRCDSelectionGuidemustbeusedinconjunctionwiththeApprovedRCDSettingsdocumenttoensurethenewparametervalueconformstothecertifiedparameterset.Seethefollowingsectionforadescriptionofnecessarydocumentsforthisactivity.
When Applicants other than Honeywell are utilizing this methodology, they should follow the same steps as described above with the exception that they must provide the completed RCD Worksheet to Honeywell for processing. Honeywell as the Manufacturer remains responsible for building the RCD and returning the RCD media, either PCMCIA card for MK V / MK VII or Universal Serial Bus (USB) flash drive for MKV-A, to the Applicant.
When Applicants other than Honeywell choose not to certify volume ranges or the maximum number of available functions and choose instead to certify a static set of volumes or a subset of possible functions, the Applicant is still encouraged to utilize this document as guidance in selecting specific RCD values. However some of the documents described in the following section will not apply.
2 Applicable Honeywell STC Documents
When utilizing the methodology described in the section above, the Honeywell STC data package will contain three specific documents intended to assist the Operator/Applicant in defining and loading a valid set of RCD parameters:
1. ApprovedRCDSettings–Itsfulltitleis“ApprovedRCDSettingsfortheInstallationoftheHoneywellEGPWCandActivationofRAASinthe<insertaircrafttype>”andisidentifiedbyits10‐digitpartnumberendingin“‐003”.ThisdocumentwascreatedduringtheFOTcertificationandcontainsthefullsetofcertifiedRCDparametersfromwhichtheOperator/Applicantwillselecttheirspecificsetofparameters(e.g.avolumelevelfromwithinavolumerange,aspecificrunwayholdtimefromasetofavailableholdtimes,orturningaspecificRAASfunctionONorOFF).
2. RCDDefinitionInstructions–Itsfulltitleis“RCDDefinitionInstructionsfortheInstallationoftheHoneywellEGPWCandActivationofRAASinthe<insertinstallationaircraft>”andisidentifiedbyits10‐digitpartnumberendingin“‐010”.Thisdocumentprovidesstep‐by‐stepinstructionsforcompletingeachsectionofanRCDWorksheetbyreferencingthisRCDSelectionGuide.ItthendirectstheOperator/ApplicanttoinstructionsforloadingtheRCDintotheinstalledEGPWSoncetheRCDmediahasbeenreceivedfromHoneywell.
3. RCDSelectionGuide‐ProvidesguidanceforselectingtheparametervalueforeachRAASfunctionandcontainstheRCDWorksheet(seeAppendixA).
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2.1 Reference Documents
Document Number, use latest revision
Document Title
060-4199-180 Enhanced Ground Proximity Warning System Line Maintenance Manual
060-4314-080 Test Procedure for Adjustable Volume Settings of RAAS Functions in the EGPWS
060-4564-001 Product Description SmartRunway® / SmartLanding® Functions of the Enhanced Ground Proximity Warning System.
993-0976-401 Interface Control Document for the Mark V Enhanced Ground Proximity Warning System (MKV EGPWS)
993-1076-401 Interface Control Document (ICD) for the Mark VII Enhanced Ground Proximity Warning System (MK VII EGPWS)
PDS69000940-201 Line Maintenance Manual for the MKV-A Enhanced Ground Proximity Warning System (EGPWS)
SYS69000940-700 Interface Control Document for the MKV-A EGPWS
CRI / <Aircraft Type Specific Identifier>
EASA Certification Review Item - Honeywell Runway Awareness and Advisory System (including extended functionality in software 230-230 and later)
3 How to Use This RCD Selection Guidance
DocumentLayout:
Section4ofthisdocumentcontainsatableofRAASfunctionsandotherrequiredRCDparameters. Each function and parameter listed in the table references a corresponding paragraph in section 5 that provides guidance for completing the corresponding entry in the RCD Worksheet.
From the paragraph in Section 5, the Operator/Applicant will choose a value from theoptionslistedbasedon:
1. GuidanceprovidedintheSection5paragraph2. ConformancetotheApprovedRCDSettingsdocument(‐003)3. OperatorspecificoperatingproceduresapplicabletotheOperator’saircrafttype
fortheroutenetworkthetypeoperateson.
RCDParameterTypes:
RCDparameteroptionsareoneofthreetypes:
a. Ranges:Volumerangeswherebyamaximumandminimumvolumeiscertifiedallowinganyvolumewithintherangetobeselectedwithaminimumriskofsubsequentretest.AvolumesettingcanbespecifiedforeachRAASalert.
b. DiscreteValues:Asetofdiscretevalueswherebyeachvalueiscertifiedallowinganyvaluewithinthesettobeselectedwithaminimumriskofsubsequentretest.Forexample,sixrunwayholdtimesmaybecertifiedfromwhichtheOperatorwillselectthemostappropriateholdtime.
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c. Distances:AvaluethatisselectedandcertifiedtomeettheintendedfunctionallowingtheOperatortoselectanoptimalvaluefortheiroperatingprocedureswithaminimumriskofsubsequentretest.Forexample,theOperatormaychooseanalerttriggervaluefortheShortRunwayfunctionthatmostcloselymatchestherunwaysusedintheOperator’sroutestructure.
CompletingtheRCDWorksheet:
Onceaspecificparametervalueisdetermined,theApplicantwillcompletethecorrespondingsectionoftheRCDWorksheetlocatedinAppendixAofthisdocument.Notethatformanyoftheparameterselections,thereisspaceprovidedfortheApplicanttostatetheselectionmethodology.
Notes:AlthoughHoneywellreviewsRCDWorksheetselectionspriortobuildingtheRCD,responsibilityforthecorrectnessoftheparameterselectionsremainswiththeapplicant.ProvidingselectionmethodologyassistsHoneywellwiththisreviewandmaycontributetofindingerrorsearlyintheprocess.
EachfunctionlistedinSection5isannotatedwithareferencetoasectioninHoneywelldocument060‐4564‐001,“ProductDescriptionSmartRunway®andSmartLanding®FunctionsoftheEnhancedGroundProximityWarningSystem”.ThesereferencesallowtheOperatortoeasilylocateamoredetaileddescriptionofthefunction.
SubmittingtheRCDWorksheet:
OncetheApplicanthasspecifiedthedesiredRCDparameterselectionsintheRCDWorksheet,theywillsubmittheworksheettoHoneywellforprocessing.HoneywellisresponsibleforcreatingtheRCDasspecifiedintheRCDWorksheet,loadingitonthephysicalmedia(PCMCIAcardorUSBflashdrive),andreturningittotheApplicant.
TheApplicantcansubmitthecompletedworksheettoHoneywellOrderAdministration,viafaxinUSA(913‐712‐1335)orINTL(+420234625777).
EGPWSPartNumberStandards
Throughoutthisdocument,MKVandMKVIIsoftwareversionnumbersareoftheform,‐XXX‐YYY;where–XXXrepresentstheApplicationSWversionnumberand–YYYrepresentstheConfigurationSWversionnumber.Notethatinnearlyallinstances,thesetwoversionnumberswillbeidentical.
ThestandardEGPWSMKVP/N965‐0976‐0XXappendstheSWversionnumbertotheend.Forexample,anEGPWSMKVP/Nmaybe965‐0976‐040‐236‐236.Similarly,thestandardEGPWSMKVIIP/N965‐1076‐0XXmaybe965‐1076‐040‐236‐236.
InordertosimplifytheEGPWSP/NforAirbusandBoeingaircraft,eachEGPWSMKVP/Nmapstoaunique10‐digitAirbusorBoeingP/N(seeTable3‐1,below).ForadetaileddiscussionofEGPWSP/Ns,seeSection1.0oftheEGPWSMKVorMKVIIICDnotedinSection2.1ReferenceDocuments.
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Table3‐1‐EGPWSPartNumberStandard
StandardP/N AirbusP/N BoeingP/N
965‐0976‐0XX‐218‐218 965‐1676‐002 965‐1690‐051
965‐0976‐0XX‐230‐230 965‐1676‐004 965‐1690‐054
965‐0976‐0XX‐236‐236 965‐1676‐006 965‐1690‐057
TheMKV‐Awillhavepartnumbersintheformof69000940‐XYY,whereXistheHWversionandYYistheSWversion.Forexample,69000941‐101isa28VDCMKV‐AEGPWCwithhardwareversion1andsoftwareversion01.SeeTable3‐2below.
Table3‐2–MKV‐AEGPWSPartNumberStandard
MKV‐AStandardP/N Characteristics
69000940‐XYY 115VAC
69000941‐XYY 28VDC
69000942‐XYY Airbus115VAC
3.1 Compliance with the EASA RAAS Certification Review Item
EASApublishedaCertificationReviewItem(CRI)containingspecificrequirementsforRAAS.ApplicantsintendingtoapplyforanEASATypeCertification(ETC),EASASupplementalTypeCertification(ESTC),orEASAValidationofanapprovedTCorSTCfromanEASA‐recognizedCertificationAuthority,mustshowcompliancetotheEASARAASCRI.
Note:TheEASARAASCRIappliestoallinstallationsofRAASwhetherconsistingofbasicRAASonly(softwareversions‐218‐218to‐228‐228)orRAASwithextendedfunctionsSAM,LLMonitor,CAM,andTakeoffFlapsMonitor(softwareversion‐230‐230andlater).
TheCRIcontainsspecificrequirementswhen,1)theinstallationactivatesanyoftheextendedfunctionsor,2)activatesextendedfunctionswithcautionlevelalerts.Therefore,itisimperativethattheapplicantunderstandwhichRAASfunctionsarebeingactivatedandtheassociatedCRIrequirements.SeeTable4‐1–RAASFunctionSelectionsandDescriptions,below.
MKV‐AprovidescompliancetotheEASARAASCRIbeginningwiththefirstsoftwarerelease‐x01/‐x51.
EASARAASCRIrequirementspertainingtoRCDparameterselectionhavebeenembeddedinSection5ofthisRCDConfigurationSelectionGuidancedocument.
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4 Function Selections and Descriptions Summary
Table4‐1–RAASFunctionSelectionsandDescriptionsprovidesalistofRCDselectionsanddescriptionsforRAAS.
Table4‐1–RAASFunctionSelectionsandDescriptions
Function(ProductDescriptionReferenceparagraph)
Monitor
Routine/
Non‐Routine
Advisory/
Caution
Section
Reference
EnableVisualMessages(All,Cautions‐only,Non‐Routine‐only,None)
‐ ‐ ‐ 5.1
RAASEnableMethod
(RCDMasterKey/EnableKeyCard)‐ ‐ ‐ 5.1
RAASProgramPinEnable
(No/Yes)‐ ‐ ‐ 5.1
EASACRISettings
(No/Yes)‐ ‐ ‐ 5.1
RAASInhibit/EnableSwitch(No/Yes)
‐ ‐ ‐ 5.1
RAASINOPIndicator
(No/Yes)‐ ‐ ‐ 5.1
SelectVoiceGender(Male/Female)
‐ ‐ ‐ 5.1
SelectAnnunciationofUnitofMeasure
(Off/First)‐ ‐ ‐ 5.1
DistanceUnitofMeasure(Feet/Meters)
‐ ‐ ‐ 5.1
SelectAdvisorySuppressWindow
(450‐550ft/350‐450ft)‐ ‐ ‐ 5.1
GPSAntennaLocation
(Tonearest5feet)‐ ‐ ‐ 5.1
ApproachingRunwayInAir(4.2.1)
(Off/On)RAAS Routine Advisory 5.2.1
ApproachingRunwayOnGround(4.2.2)(Off/On)
RAAS Routine Advisory 5.2.2
OnRunwayOnGround(4.2.3)
(Off/On)RAAS Routine Advisory 5.2.3
DistanceRemaining,LandingandRoll‐out(4.2.4)(Off/50%ofRunway)
(1000,2000,3000,4000,5000feet)
RAAS Routine Advisory 5.2.4
RunwayEnd(4.2.5)
(Off/On)RAAS Routine Advisory 5.2.5
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Function(ProductDescriptionReferenceparagraph)
Monitor
Routine/
Non‐Routine
Advisory/
Caution
Section
Reference
ApproachingShortRunwayInAir(4.3.1)
(Off,On,Always*)‐IfOn,thenenternominalrunwaylength
‐IfAlways,thenentermaximumlengthof9,.999feet*SelectingAlwaysmakesthisaRoutineadvisory
RAAS Non‐Routine Advisory 5.3.1
CautionApproachingShortRunwayInAir(4.3.2)
(Off,On‐IfOnthenenternominalrunwaylength)RAAS Non‐
Routine Caution 5.3.2
InsufficientRunwayOnGround(4.3.3)(Off,On,Always*)
‐IfOn,thenenternominalrunwaylength
‐IfAlways,thenentermaximumlengthof99,999feet*SelectingAlwaysmakesthisaRoutineadvisory
RAAS Non‐Routine Advisory 5.3.3
CautionInsufficientRunwayOnGround(4.3.4)
(Off,On‐IfOnthenenternominalrunwaylength)RAAS Non‐
Routine Caution 5.3.4
ExtendedHoldingOnRunway(Initial&Repeat)(4.3.5)
(TimeinsecondsforInitial&forRepeat)RAAS
Non‐Routine Advisory 5.3.5
TaxiwayTakeoff(Advisory)(4.3.6.1)or,
TaxiwayTakeoff(Caution)(4.3.6.2)(Off,On)
(SelectAdvisoryorCautionbutnotboth)
RAASNon‐
Routine Advisory 5.3.6.1
RAAS Non‐Routine
Caution 5.3.6.2
DistanceRemaining,RejectedTakeoff(4.3.7)
(Off,50%ofRunway)
(1000,2000,3000,4000,5000feet)
RAAS Non‐Routine Advisory 5.3.7
TaxiwayLanding(4.3.8)(Off,On)
RAAS Non‐Routine Caution 5.3.8
VolumeSettings
(ReconfigureRCDVolumeNo,Yes–IfYes,entervolumes)‐ ‐ ‐ 5.8
StabilizedApproachMonitor–Unstable(5.2.4)(EnableSAMOff,On)
SAM Non‐Routine Caution 5.4
StabilizedApproachMonitor–LandingFlaps(5.2.1)
(UpperFlapGateAlertOff,On–IfOn,setGateAltinfeet)
(LowerFlapGateAlertOff,On–IfOn,setGateAltinfeet)
SAM Non‐Routine Advisory 5.4.1
StabilizedApproachMonitor–ExcessiveApproachAngle(5.2.2)(Off,On)
SAM Non‐Routine Advisory 5.4.2
StabilizedApproachMonitor–ExcessiveApproachSpeed(5.2.3)
(Off,On)SAM Non‐
Routine Advisory 5.4.3
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Function(ProductDescriptionReferenceparagraph)
Monitor
Routine/
Non‐Routine
Advisory/
Caution
Section
Reference
AltimeterMonitor–BelowTransitionAltitude(6.2.1)
AltimeterMonitor–AboveTransitionAltitude(6.2.2)(EnableAltimeterMonitorOff,On)
(EnableAltimeterMonitorBelowTAOff,On)(EnableAltimeterMonitorAboveTAOff,On)
Alt Non‐Routine Advisory 5.5
TakeoffFlapConfigurationMonitor(7.2)
(EnableTakeoffFlapsMonitorOff,On)(Enable/InhibitNone,Gnd,28v)
(TakeoffFlapHandleMinimumSetting)
(TakeoffFlapHandleMaximumSetting)
T/OFlaps
Non‐Routine Caution 5.6
LongLandingMonitor(8.2)(EnableLLMonitorOff,On)
(ConfigureCallout“LongLanding”,“DeepLanding”)(LLDistancefromThresholdinfeetormeters)
(LLPercentagefromStopEndOff,On,%)(LLDistanceRemainingOff,On,feetormeters)
(LLDistanceRemainingPercentagefromStopEndOff,On,%)
LLNon‐
Routine Caution 5.7
5 RCD Worksheet Guidance
Alloptionsintheworksheetmustspecifyavalue,evenifselectedOFF.Worksheetswithblankentriescannotbeprocesseduntilallquestionableselectionsareclarified.
RefertotheProductDescriptionSmartRunway®andSmartLanding®FunctionsoftheEnhancedGroundProximityWarningSystem,Honeywelldocument060‐4564‐001,formoreinformationabouteachfunction.Therelevantproductdescriptionsectionnumbersarelistedinparenthesesfortheitemsbelow.
TheOperator/ApplicantmayusetheCOMMENTSblockonthefinalpageoftheworksheetorwritefreehandnotesanywherepracticalintheworksheettocommunicateanyinstructionsnotspecificallycoveredbycurrentavailableselections.TheOperator/Applicantmayappendmorethanoneworksheetifthenumberofseparateaircrafttypesisgreaterthannine.
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5.1 Operator Information and System Preferences
Completethefollowingtablesasspecified.
General Information
Aircraft Operator
Date (MM/DD/YYYY)
Customer name/Company
Customer Phone/Fax/email
Ordering Information
Customer: P.O. #: Requested Ship Date:
EGPWS P/N:
EGPWS S/N:
Model and Part Number Selection
Ex:
Columns are provided for up to nine separate aircraft types
AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
OEM Aircraft Model 737-500
OEM Aircraft TN or SN
(leave blank for fleet)
EGPWS Aircraft Type number
(See Notes 1 & 2 below) 194
MK V, MK VII, or MKV‐A EGPWS MK V
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Model and Part Number Selection
Notes
Note1:A/Ctypenumberisa1to3‐digitnumberusedbytheEGPWSmodeltodefinetheinstallation.Thisnumbercanbefoundusingoneofthefollowingmethods:
ConductingaLevel3Self‐TestontheaircraftperLineMaintenanceManual–MKV,MKVII,EnhancedGroundProximityWarningSystems,andHoneywelldocument060‐4199‐180.ForMKV‐AusedocumentnumberPDS69000940‐201,LineMaintenanceManualfortheMKV‐AEnhancedGroundProximityWarningSystem(EGPWS).
ExaminingEGPWSaircraftprogrampinwiringagainsttheInterfaceControlDocumentfortheMarkVEnhancedGroundProximityWarningSystem(MKVEGPWS),Honeywelldocument993‐0976‐401.FortheMKV‐AuseDocumentNumberSYS69000940‐700,InterfaceControlDocumentfortheMKV‐AEGPWS.
ExaminingEGPWSaircraftprogrampinwiringagainsttheInterfaceControlDocumentfortheMarkVIIEnhancedGroundProximityWarningSystem(MKVIIEGPWS),Honeywelldocument993‐1076‐401.
Note2:MKVIIaircrafttypes3,4,5,7aregeneric,nowindshearaircrafttypesthatcanbeusedwithmultipleairframes.Forexample,MKVIIEGPWSA/Ctype5isagenericAirTransport,nowindshearconfigurationthatmaybeusedonDC‐9‐32,B747‐200andA300B4‐200aircraft.TheRCDwillnotdistinguishbetweenaircraftmodels,onlyaircrafttypenumbers.IfmorethanoneaircraftmodelhasEGPWSinstalledandisusingaMKVIIgenericaircrafttype,thenmultipleRCDswillberequired.Completetheworksheetlistingallaircraftusingthegenericaircrafttypes,andsendtoHoneywellforevaluation.
VisualMessagesonTerrainDisplayforNon‐TSOFunctions
EnableVisualMessages
(See Note, below)
AllMessages Non‐routineMessagesOnly
CautionsOnly None
Notes
Note:Table4‐1–RAASFunctionSelectionsandDescriptionsintheprevioussectionindicatesforeachfunctionthetypeofmessageandwhetherthealertlevelisconsideredacautionoradvisorymessage.VisualmessagesontheTerraindisplaycanbeselectedforeachauralannunciationexceptfortheLongLandingDistanceRemaining(8.0),RAASDistanceRemaining(4.2.4and4.3.7)andtheRAASRunwayEnd(4.2.5)callouts.
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General RCD InformationSelect RCD Enable Method
(SeeNote1,below) RCD Master Key Enable Key Card
Add RAAS Program Pin Enable
(SeeNote2) NO YES
EASA CRI Settings (SeeNote3) NO YES
Runway Awareness and Advisory System (RAAS) Common Selections
Select RAAS Enable On Off
Select RAAS Enable / Inhibit Discrete
None Ground or 28V = Inhibit
Ground or 28V = Enable
BOTH 1st : Ground or 28V = Enable2nd: Ground or 28V = InhibitNOTE: Only valid for MKV‐A
RAAS Discrete Connector Pin (ex: TP1A) 1ST 2ND
RAAS Enable / Inhibit Switch Configuration
If installing a RAAS Enable / Inhibit Discrete, select one Option
Option 1: RAAS Discrete(s) applies to: Rwy + LL + T/O Flaps
Option 2:RAAS Discrete(s) applies to: Rwy + LL + T/O Flaps + SAM
Option 3: RAAS Discrete(s) applies to: Rwy + LL + T/O Flaps + CAM*
Option 4: RAAS Discrete(s) applies to: Rwy + LL + T/O Flaps + SAM +CAM*
*NOTE: Options including CAM can only be selected for an “Inhibit” Discrete
Add RAAS INOP Indicator NO YES
Select voice gender (seeNote4) Female Voice
Male Voice
Select Annunciation of Unit of Measure (UOM) – (seeNote5) OFF FIRST
Select Distance Unit of Measure (UOM) – (seeNote6) Feet Meters
AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
Select Advisory Suppress Window (seeNote7)
450‐550 (feet)
350‐450 (feet)
GPS Antenna Location (seeNote8)
35 feet
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General RCD InformationNote 1: TheEGPWShastwomethodstounlockRAAScapabilityontheEGPWS.
OnemethodutilizesaRCDMasterKey.TheMasterKeyisloadedonthesamePCMCIAcardorUSBflashdrive(MKV‐A)astheRCD.RAASactivationisaccomplishedwhenthissinglePCMCIAcard/USBflashdriveisusedtoinstalltheRCDacrossafleetofaircraft.
AnothermethodutilizesanEnableKeyCard.AnEnableKeyuniquetoanEGPWSserialnumberisgeneratedthenloadedonaPCMCIAcard/USBflashdrive.TheRCDisloadedonaseparatePCMCIAcard/USBflashdrive.RAASactivationisaccomplishedwhenthePCMCIAcard/USBflashdrivecontainingtheEnableKeyisloadedfollowedbythePCMCIAcard/USBflashdrivecontainingtheRCD.BecauseauniqueEnableKeyCardisrequiredforeachaircraft,thismethodistypicallyusedbybusinessaviationoperatorsandairlineoperatorswithfleetsizesoffiveorless.
Note2:Onceunlocked(seeNote1,above),anoptionalRAASProgramPinEnablecanbeusedtoensureRAASisnotactivateduponinstallationunlesstheprogrampinsarewiredcorrectly.Thismethodwasintroducedinsoftwareversion‐230‐230(forMVKseeAppendixD‐15ofICD993‐0976‐401,forMKV‐AseeappendixD‐15ofICDPDS69000940‐201).ThisapproachishelpfulwhenmultipleoperatorsutilizeasharedpoolofspareunitswherebyanunlockedRAASEGPWScomputercouldbeinstalledonanaircraftnotcertifiedforRAAS.Inthiscase,theabsenceofcorrectlywiredprogrampinswouldpreventtheactivationofRAAS.
Note3:EASACRI
TheEASARAASCRIappliestoallinstallationsofRAASwhetherconsistingofbasicRAASonlyMKV/MKVII(softwareversions‐218‐218to‐228‐228)orRAASwithextendedfunctionsSAM,LLMonitor,CAM,andTakeoffFlapsMonitor(softwareversion‐230‐230andlater).
ForbasicRAAS,anInhibitSwitchandINOPIndicatorarenotrequired.However,whentheinstallationactivatesanyoftheextendedfunctions:
AnInhibitSwitchmustbeinstalledthatiscapableofinhibitingallRAASfunctionsandenabledextendedfunctionsSAM,LLMonitor,CAM,andTakeoffFlapsMonitor.
ARAASINOPIndicatormustbeinstalledthatiscapableofannunciating"allRAASfunctionsandenabledextendedfunctionsSAM,LLMonitor,CAM,andTakeoffFlapsMonitorfailuresifanalternatefailindicationmechanismisnotavailablesuchasanEICASdisplay(seeICDfortheappropriateaircraftwiring).
Note:RAASautomaticallyinhibitsanyauralalertforwhicharequiredinputhasfailedandilluminatestheRAASINOPIndicatortoadvisethecrewoflossoffunction.However,RAAScontinuestoenunciateauralalertswhereallrequiredinputsremainvalid.TheEASACRIclassifiescontinuedauralalertinginthepresenceofaRAASINOPindicationas,“…inappropriate
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General RCD Informationalertsduringsystemmalfunctions”.Thereforewhenextendedfunctionsareactivated,theCRIrequiresthesilencingofallalertsusinganinhibitswitchwhentheRAASINOPIndicatorisilluminated.
OptionSelection:
TocomplywiththeEASACRI,aRAASInhibitSwitchmustbeinstalledandconfiguredtosilenceallRAASfunctions(basicRAAS,LL,T/OFlaps,SAM,andCAM)byselectingOption4,above.
IfanoperatordoesnotintendtoseekanEASASTCorEASAvalidationofaFAASTC,theoperatorcanchooseto:
NotinstallaRAASInhibitSwitch(oraRAASINOPIndicator)
InstallaRAASInhibitSwitchandselectoneofthealternateOptions,above
Note4:EASACRI
TheEASACRIrequiresthattheGenderSelectionbeconsistentwiththeflightdeckphilosophy.
Note 5: SelectionofFIRSTaddstheUOM(e.g.feetormeters)tothefirstcalloutforDistanceRemainingadvisories(5.2.4,5.3.7,5.7)butnotsubsequentcallouts.Forexample,“Four‐ThousandFeetRemaining”,“Three‐ThousandRemaining”,“Two‐ThousandRemaining”,…
ForRunwayEnd(6.2.5)andShort/InsufficientRunwayAdvisories(6.3.1,6.3.3),FIRSTaddstheUOMtoeveryinstanceofthecallout.
Note6:EASACRI
TheEASACRIrequiresthattheUnitofMeasurefunctionbeactivated.AselectionofFIRSTmustbemadeifintendingtoapplyforanEASATC/STC
Note7:Whenselected450‐550,theRAASInAiradvisoryissuppressedbetween550feetand450feetaboverunwayelevationtoallownormal500‐footaltitudecalloutsand/orcrewprocedureswithoutconflict.Theoption,350‐450,willsuppresstheRAASInAiradvisorytoallowthe400‐footaltitudecalloutsinAirbusaircraft.Mostaircraftshouldselect450‐550.
Note8:EnterthedistancetheGPSantennaislocated,fromthenoseoftheaircrafttothecenteroftheantenna,roundeduptothenearest5foot.(i.e.ifdistancemeasuredis11feet,thenroundupto15feet).
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5.2 RAAS Routine Advisories
5.2.1 Approaching Runway – In Air advisory (Product Description 4.2.1)
ThepurposeoftheApproachingRunway–InAiradvisoryistoprovidethecrewwithawarenessofwhichrunwaytheaircraftislined‐upwithonapproach.
Annunciationcriteria
RAASequippedaircraftprovidetheflightcrewwithanauraladvisorywhentheaircraftisairborneandapproachingarunway.Thisadvisoryisenabledwhen:
Aircraftisbetween750feetand300feetabovetheairportelevation(AFE)and
Aircraft iswithin3nauticalmiles (<3NM)of the thresholdendof the runway:and
Aircrafttrackisalignedwiththerunway(aircrafttrackiswithin±20degreesoftherunwayheading)and
Aircraft position is within 200 feet laterally of the runway centerline plusrunwaywidth.
MessageContent
Thisadvisoryconsistsoftheword“Approaching”followedbytherunwayidentifier,forexample,“ApproachingTwo‐Five‐Right”.
AdvicetoOperator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofeachfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperation.
EnableApproachingRunway‐ inair(4.2.1) OFF ON
5.2.2 Approaching Runway – On Ground advisory (Product Description 4.2.2)
ThepurposeoftheApproachingRunway–On‐Groundadvisoryistoprovidetheflightcrewwithawarenessofaproximaterunwayedgebeingapproachedbytheaircraftduringtaxioperations.
AnnunciationCriteria
RAASdeterminestherunwayidentifierfortheendoftherunwaythatisclosesttothepositionoftheaircraft.Thisadvisoryisenabledwhen:
Aircraftisontheground,and
Aircraftgroundspeedislessthan40knots,and
Aircraftiswithinaspecifieddistancefromtherunway.
MessageContent
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Theauralmessageconsistsoftheword“Approaching”followedbytherunwayidentifier.Forexample,“ApproachingThree‐Four‐Left”.Thisadvisoryisissuedonceeachtimetheaircraftapproachesarunway.
AdvicetoOperator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofeachfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperation.
EnableApproachingRunway– onground(4.2.2) OFF ON
5.2.3 On Runway – On Ground advisory (Product Description 4.2.3)
ThepurposeoftheOnRunwayadvisoryistoprovidethecrewwithawarenessofwhichrunwaytheaircraftislinedupwithduringgroundoperations.
AnnunciationCriteria
TheOnRunwayadvisoryisgeneratedwhenthefollowingconditionsaremet:
Aircraftentersontorunway,and
Aircraftheadingiswithin±20degreesoftherunwayheading.
MessageContent
Theauralmessageconsistsofthewords“OnRunway”followedbytherunwayidentifier,forexample,“OnRunwayTwo‐Four”.Thisadvisoryisannunciatedonceeachtimetheaircraftentersarunway.
AdvicetoOperator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofeachfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperation.
EnableOnRunway–onground(4.2.3) OFF ON
5.2.4 Distance Remaining – Landing and Rollout advisory (Product Description 4.2.4)
ThepurposeoftheDistanceRemainingadvisoriesistoenhancecrewawarenessofaircraftalong‐trackpositionrelativetothestopendoftherunway.
AnnunciationCriteria
Aircraft iswithin100 feetof the ground, over the lasthalf of the runwayoraspecifieddistancefromtherunwayend;or
Aircraftisontheground,onthelasthalfoftherunway(default)oraspecifieddistancefromtherunwayend,and
Aircraftgroundspeedisabove40knots.
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MessageContent
Forsystemsusingfeetastheunitoflength,theseadvisoriesaregeneratedatwholethousand‐footintervals,exceptthatthelastpossibleadvisoryoccursat500feet.Forexample,aRAASequippedaircraftlandingona9000footrunway,configuredwiththeDistanceRemainingadvisorystartingatthelasthalfoftherunway,couldgeneratethefollowingadvisories:“Four–ThousandFeetRemaining”,“Three‐ThousandRemaining”,“Two‐ThousandRemaining”,“One‐ThousandRemaining”,and“Five‐HundredRemaining”.AsecondexampleofaRAASequippedaircraftlandingona9000footrunway,configuredwiththeDistanceRemainingadvisorystartingat2000feetfromthestopendoftherunway,couldgeneratethefollowingadvisories:”Two‐ThousandfeetRemaining”,“OneThousandRemaining”and“Five‐HundredRemaining”.
Advice to Operator
Thelandingdistancecanbeascertainedfromseveralalternativestodeterminewhetheryouwanttoselectthe50%ofrunwaycriteriaornot.
a) PerformanceLandingdistancerequiredatmaximumallowablelandingweightinISAsealevelconditionswithzerowindcomponent.
b) Alternatively,theOperatorcouldselectalandingdistancerequiredrepresentingtheaverageweightandtheaverageweatherconditionstheaircrafttypeoperatesatandinwithanaverageAutobrakesetting.Thedata,includingAutobrakesettingsused,canbereadilyavailableiftheOperatorhasaFOQAprograminplaceforallflights.
Oncealandingdistancehasbeenascertained,theOperatorwillbeinapositiontojudgehowoftenanaircraftwouldbeusingmostofagivenrunwayontheroutenetwork,andtherelevancyofchoosingeitherthelatterhalfoftherunwayorafixeddistancefromthestopend.
Formanyaircraft,choosingthelasthalfoftherunwaymaycauseunwantedadvisoriestobegeneratedonwhatisaslightlyabnormallandingandrollout.Considerationshouldbegivenregardingtheconsequencesofthisselectionovertheselectionofafixeddistancefromthestopendoftherunway.
Thecrewwillneedtobefamiliarwiththerelevant/criticalspeedsforrelevantweight(s)atgivendistancesfromtheendoftherunway;thiswillenablecrewstoassesswhetherthespeedtheyareat,ataparticulardistancefromthestopendiscriticalornot,intheeventthatcalloutsareannunciated.
Foragivenapproachspeed,landingdistances(distanceoftouchdownpastthresholdplusdistancefromtouchdowntostop)forvariousconditionsand“AutobrakeSettings”maybecalculatedbythecrew,providedtheyarefurnishedwithrelevantdata(whichtheyneedtobe).Fromthisdatathecrewcananticipateifanadvisorycanbeexpected,giventheyknowtherelevantdistanceselectedforthesystem.
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SelectDistanceremaining,landingandRollout(4.2.4)
(SeeNote1,below)
OFF 50%ofrunway
1000feet
(300m)
2000feet
(600m)
3000feet
(900m)
4000feet
(1200m)
5000feet
(1500m)
Notes
Note1:IfactivatingboththeDistanceRemainingLanding&Rollout(DREML&R)functionandtheLongLandingDREMfunction,theselectedtriggervaluesmustbeconsideredtogether.Seesection6.8LongLandingMonitorforthisdiscussion.
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
5.2.5 Runway End advisory (Product Description 4.2.5)
ThepurposeoftheRunwayEndadvisoryistoimproveflightcrewawarenessofthepositionoftheaircraftrelativetotherunwaystopendduringlowvisibilityoperations.
AnnunciationCriteria
Theadvisoryisprovidedtotheflightcrewwhen:
Aircraftisontherunwayandalignedwithin20degreesofrunwayheading,and
Aircraftapproacheswithin100feetofrunwaystopend:and
Aircraftgroundspeedisbelow40knots.
MessageContent
Theauralmessageis“One‐HundredfeetRemaining”forunitsoffeet,or“ThirtyMetersRemaining”forunitsofmeters.
AdvicetoOperator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofthisfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperationandotheradvisories.
Enablerunwayendadvisory(4.2.5) OFF ON
5.3 RAAS Non - Routine Advisories and Cautions
5.3.1 Approaching Short Runway – In Air advisory (Product Description 4.3.1)
ThepurposeoftheApproachingShortRunway–In‐AirAdvisoryistoprovidethecrewwithawarenessofwhichrunwaytheaircraftislined‐upwith,andthattheavailablerunwaylengthforlandingislessthanthedefinednominallandingrunwaylength.Theavailablerunwaylengthisdeterminedbycomparingrunwaylengthasdefinedinthe
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EGPWSRunwayDatabasewiththenominalrunwaylengthrequiredfortheaircraftasdefinedintheRCD.
AnnunciationCriteria
Theadvisoryisgeneratedwhenthefollowingconditionsaremet:
Allconditions foraRoutineApproachingRunwayIn‐AirAdvisoryaresatisfied,and
Alignedrunwayisshorterthananominalrunwaylength.
MessageContent
TheRoutineApproachingRunwayAdvisoryisappendedwithavailablerunwaylengthinformation,forexample”ApproachingTwo‐Five‐Left,Three‐Thousand‐Eight‐HundredFeetAvailable”.TheavailableelementofthemessagereferstotherunwaydistanceavailablefromtheEGPWSrunwaydatabasetothenearest100feetor30metersdependingonunitsselected.
Advice to Operator
Thenominalrunwaylengthchosenmaybebasedononeofthefollowingcriterion.
Approachingrunwayxxandshortrunwayadvisoriesaretiedtogether,however,thedistanceavailableisonlyvoicediftherunwaylengthavailableisshorterthannominallengthstipulatedbelow.
TheshortestrunwayontheOperator’sroutenetwork.
Alternatively,theOperatorcouldselectanominalrunwaylengthbasedonthelandingdistancerequired(landingrun[distancefromtouchdowntostop]plusdistanceoftouchdownpastthreshold)usingthemeanweightandtheaverageweatherconditionstheaircrafttypeoperatesatandin,withanaverageAutobrakesetting.Thedata,includingAutobrakesettingsused,canbereadilyavailableiftheOperatorhasaFOQAprograminplaceforallflights.
Thenominaldistanceselectedshouldbemadeavailabletocrews,sothatanadvisorycallcanbeanticipated,ifplanningtolandonanexceptionallyshortrunway.
Selectapproachingshortrunwaylength–inairadvisory(4.3.1)
(SeeNote1,below)
OFF ON
(Enternominalrunwaylength
below)
ALWAYS
(Enterarunwaylengthof99,999feetmakingthisa
RoutineAlert)
ShortRunwayLength‐inair
(feetorm)
Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
4500ft
Notes
Note1:RAASShortandInsufficientRunwayfunctionsdonottakeintoaccountaircraft
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performancefactorssuchasaircraftweight,wind,runwayconditions,slope,airtemperatureandaltitudeofairport.Thisinformationisintendedtoenhancetheflightcrewawarenessbyidentifyingthattherunwaylengthavailablemaybemarginalfortheaircrafttype.NominalRunwayLengths:Entervalueroundeduptothenearest100feet(30m).IfadvisoryisturnedOFF,thenleaveblank.Ifavailablerunwaylengthistoalwaysbeannunciated,thenenterALWAYS.TheRAASalgorithmprocessesdistancesinfeet.IftheOperatorselectstheMetersoption,andthenominalrunwaylengthslistedareinmeters,Honeywellwillconvertthemetersvalueintofeetusingtheformula(Feet=Metersx3.280839895).Whentheadvisoriesaretriggered,thealgorithmrecalculatesandprovidesdistanceadvisoriesinmeters.
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
5.3.2 Approaching Short Runway – In Air Caution (Product Description 4.3.2)
Thepurposeofthisannunciationistoprovidethecrewwithanimmediateawarenessthattheavailablerunwaylengthforlandingislessthantherunwaylengthdefinedforthecautionmessage(ProductDescription4.3.1).
TheavailablerunwaylengthisdeterminedbytheEGPWSRunwayDatabase.
TheselectionofaCaution,inadditiontotheexistingadvisory,isconfigurableviatheRCD.
Ifthecautionisdesired,itisrecommendedthatboththeadvisoryandcautionareenabled.
AnnunciationCriteria
TheApproachingShortRunway–InAirCautionisgeneratedwhenthefollowingconditionsaremet:
AllconditionsforanApproachingShortIn‐Air‐Advisoryaresatisfied(6.3.1)and
Alignedrunwayisshorterthananominalrunwaylength,and
AircraftisbelowRAASAdvisorySuppressWindow(either450feetor350feet)andmorethan300feetaboveairportelevation(AFE).
ThenominalrunwaylengthvaluemustbespecifiedbytheOperatororisdefaultedtoOFF.Thisnominalrunwaylengthisusedtoprovideadvisorymessagestoenhancecrewawarenesstothefactthattherunwaylengthavailablemaybemarginalfortheaircrafttype.TheApproachingShortRunway–InAirCautiondoesnottakeintoaccountaircraftperformancefactorssuchasaircraftweight,wind,runwayconditions,slope,airtemperatureandaltitudeofairport.
TheApproachingShortRunway–InAirCautionauralmessageis“CautionShortRunway,ShortRunway”
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Advice to Operator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofthisfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperationandotherselections.
Crewproceduresshouldenablethecrewtoknowtherunwaylengthrequiredfortherelevantconditions.Also,thenominaldistanceselectedshouldbemadeavailabletocrews,so,whenplanningtolandonanexceptionallyshortrunway,thecrewwillbeinapositiontoanticipateifa“CautionShortRunway,ShortRunway”messagewillbepromulgatedornot.
Crewprocedureswillneedtoreflecttheneedtoexecuteago‐aroundintheeventthemessageisactivatedandtosubsequentlyassessthesituation.
SelectCautionshortrunwayinair(4.3.2)
(SeeNotes1&2,below)
OFF ON
(ifON,enternominalrunwaylengthbelow)
CautionShortRunwayLength‐inair
(feetorm)
Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
4500ft
Notes
Note1:RAASShortandInsufficientRunwayfunctionsdonottakeintoaccountaircraftperformancefactorssuchasaircraftweight,wind,runwayconditions,slope,airtemperatureandaltitudeofairport.Thisinformationisintendedtoenhancetheflightcrewawarenessbyidentifyingthattherunwaylengthavailablemaybemarginalfortheaircrafttype.NominalRunwayLengths:Entervalueroundeduptothenearest100feet(30m).IfadvisoryisturnedOFF,thenleaveblank.TheRAASalgorithmprocessesdistancesinfeet.IftheOperatorselectstheMetersoption,andthenominalrunwaylengthslistedareinmeters,Honeywellwillconvertthemetersvalueintofeetusingtheformula(Feet=Metersx3.280839895).Whentheadvisoriesaretriggered,thealgorithmrecalculatesandprovidesdistanceadvisoriesinmeters.
Note2:EASACRI
TheEASACRIstatesthatanAbnormal/Non‐normaloperatingprocedureshouldbeestablishedanddocumentedintheAirplaneFlightManualSupplement(AFMS)tosilence(inhibit)theShortRunwayLengthalertwhenanticipatinglandingonarunwayshorterthantheselectedRCDvalue.TheCRIemphasizesthisprocedureisusedforexceptionalcasessuchasdiversionsinflight.
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
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5.3.3 Insufficient Runway Length – On Ground advisory (Product Description 4.3.3)
ThepurposeoftheInsufficientRunwayLength–On‐Groundadvisoryistoprovidecrewwithawarenessofwhichrunwaytheaircraftislined–upwith,andthattherunwaylengthavailablefortakeoffislessthanthedefinednominaltakeoffrunwaylength.Therunwaylengthisdeterminedbycomparingtheaircraft’spositionintherunway,withthedistanceavailableasdefinedintheEGPWSRunwayDatabase.
AnnunciationCriteria
Theadvisoryisgeneratedwhenthefollowingconditionsaremet:
AllconditionsforaroutineOn‐Runwayadvisoryaresatisfied(6.2.3).
Availabledistancefortake‐offislessthanthedefinednominalrunwaylength.
Operatorwillneedtodefinenominalrunwaylengthrequiredfornormaloperations,sothatifrunwaydistanceremainingislessthanthefiguredesignated,theadvisorymessagewillbegiven.Notethatthisadvisorydoesnottakeintoaccountaircraftperformancefactorssuchasaircraftweight,wind,runwaycondition,andslope,aswellasairtemperatureandaltitudeofairport.
Note:Operatorsmaywishtobealertedoftheavailabledistancefortake‐offateverytake‐off.Inthiscase,therunwaylengthissettoitsmaximumallowablevalueof99,999feet.ExercisingthisoptioneffectivelyredefinestheInsufficientRunwayonGroundasaRoutineadvisory.
MessageContent
Runwaylengthremaininginformationisappendedtotheroutine“OnRunway”advisory.Forexample:“OnRunwayThree‐Four‐Left,Two‐ThousandFeetRemaining”.The”remaining”elementofthemessagereferstorunwaydistanceavailablefromtheEGPWSrunwaydatabasetothenearest100feet(30meters).
AdvicetoOperator
Runwaylengthsrequiredcanvaryconsiderably,dependingupon,takeoffweight,thrustused(full,derated,assumedtemperature),airfieldaltitude,outsideairtemperatureandrunwaydirectionwindcomponent.
Tooptimizetheapplicabilityandenhancedsafetylevelavailablewiththeimplementationofthisfunction,crew/dispatchproceduresthatenablethecrewtoidentifytherunwaylengthrequiredforaparticulartakeoffshouldbeimplemented.Thecrewwillthenbeinapositiontoknowifany“InsufficientRunaway”advicewillbepromulgatedornot.Iftheadviceisgiven,thecrewshouldnottakeoffpriortoevaluatingiftherunwaylengthadvisedisequaltoorgreaterthantherunwaylengthrequiredfortakeoffandtakeappropriateaction.
ThenominalRunwaylengthchosenshouldbebasedononeofthefollowingcriterion.
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a) Selectarunwaylengthrepresentingthemeanweightandthrustusedaswellastheaverageweatherconditionstheaircrafttypeoperatesin.ThedatacanbereadilyavailableiftheOperatorhasaFOQAprograminplaceforallflights.
b) SelecttheshortestrunwayintheOperator’sroutestructureandsubtractanominalvaluefromthelengthsufficienttoeliminatenuisancealerts.
Selectinsufficientrunwaylengthongroundadvisory(4.3.3)
(SeeNotes1&2,below)
OFF
ON
(ifON,enternominalrunwaylength
below)
ALWAYS
(Enterarunwaylengthof99,999feetmakingthisaRoutineAlert)
(SeeNotes1and2,below)
InsufficientRunwayLength–onground
(feetorm)
Ex:AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
4500ft
Notes
Note1:Operatorsmaywishtobealertedoftheavailabledistancefortake‐offateverytake‐off.Inthiscase,therunwaylengthissettoitsmaximumallowablevalueof99,999feet.ExercisingthisoptioneffectivelyredefinestheInsufficientRunwayonGroundasaRoutineadvisory.
Note2:IfALWAYSisselectedconsiderationshouldbegiventothecoloroftheassociatedvisualmessage.Bydefaultitisamber,butgreenisrecommendedfor“routineadvisories”.
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
5.3.4 Insufficient Runway Length – On Ground caution (Product Description 4.3.4)
Thepurposeofthisannunciationistoprovidethecrewwithimmediateawarenessthattherunwaylengthavailablefortakeoffislessthanthedefinednominaltakeoffrunwaylengthwhenthetakeoffiscontinuedasnotedbelowaftertheremaininglengthfortakeoffhasbeenprovided.
Theavailablerunwaylengthisdeterminedbycomparingtheaircraft’spositionontherunwaywiththedistanceavailabledefinedintheEGPWSRunwayDatabase.
AnnunciationCriteria
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TheInsufficientRunway–OnGroundCautionisgeneratedwhenthefollowingconditionsaremet:
AllconditionsforaroutineOn‐Runwayadvisoryaresatisfied,and
AvailableDistance for take‐off is less than thedefinednominal runway length,and
Aircraftgroundspeedtransitionstoabove40knots.
MessageContent
TheInsufficientRunwayLength–OnGroundCautionauralmessageis“CautionShortRunwayShortRunway”.
AdvicetoOperator
Forthis“Caution”messagethenominalrunwaylengthselectedcanbedifferenttothatchosenfor6.3.1above.Itisrecommendedthattherunwaylengthnominatedbelessthanthatchosenfor6.3.1,thiswillminimizethepotentialfornuisancemessages.Asstatedabove,tooptimizetheapplicabilityandenhancedsafetylevelavailablewiththeimplementationofthisfunction,crew/dispatchproceduresthatenablethecrewtoidentifytherunwaylengthrequiredforaparticulartakeoffshouldbeimplemented.Thecrewwillthenbeinapositiontoknow,priortotakeoff,ifany“CautionShortRunwayShortRunway”messagewillbepromulgatedornot.
ThecrewproceduresneedtoreflecttherequirementtoactionaRTOintheeventofamessagebeingpromulgatedduringthetakeoffrun.
SelectCautionshortrunwayonground(Product4.3.4)
(SeeNotes1,2&3,below)
OFF ON
(ifON,enternominalrunwaylength
below)
CautionShortRunwayLength–onground
(feetorm)
Ex:AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
4500ft
Notes
Note1:A/Ctypenumberisa1to3‐digitnumberusedbytheEGPWSmodeltodefinetheinstallation.Thisnumbercanbefoundusingoneofthefollowingmethods:
ConductingaLevel3Self‐TestontheaircraftperLineMaintenanceManual–MKV,MKVI,MKVII,MKVIIIEnhancedGroundProximityWarningSystems,andHoneywelldocument060‐4199‐180.
ExaminingEGPWSaircraftprogrampinwiringagainsttheInterfaceControlDocumentfortheMarkVEnhancedGroundProximityWarningSystem(MKVEGPWS),Honeywelldocument993‐0976‐401.
ExaminingEGPWSaircraftprogrampinwiringagainsttheInterfaceControl
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DocumentfortheMarkVIIEnhancedGroundProximityWarningSystem(MKVIIEGPWS),Honeywelldocument993‐1076‐401.
Note2:RAASShortandInsufficientRunwayfunctionsdonottakeintoaccountaircraftperformancefactorssuchasaircraftweight,wind,runwayconditions,slope,airtemperatureandaltitudeofairport.Thisinformationisintendedtoenhancetheflightcrewawarenessbyidentifyingthattherunwaylengthavailablemaybemarginalfortheaircrafttype.NominalRunwayLengths:Entervalueroundeduptothenearest100feet(30m).IfadvisoryisturnedOFF,thenleaveblank.Ifavailablerunwaylengthistoalwaysbeannunciated,thenenterALWAYS.TheRAASalgorithmprocessesdistancesinfeet.IftheOperatorselectstheMetersoption,andthenominalrunwaylengthslistedareinmeters,Honeywellwillconvertthemetersvalueintofeetusingtheformula(Feet=Metersx3.280839895).Whentheadvisoriesaretriggered,thealgorithmrecalculatesandprovidesdistanceadvisoriesinmeters.
Note3:EASACRI
TheEASACRIstatesthatanAbnormal/Non‐normaloperatingprocedureshouldbeestablishedanddocumentedintheAirplaneFlightManualSupplement(AFMS)tosilence(inhibit)theInsufficientRunwayonGroundalertwhenanticipatingtakingofffromarunwayshorterthantheselectedRCDvalue.
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
5.3.5 Extended Holding On Runway advisory (Product Description 4.3.5)
ThepurposeoftheExtendedHoldingOnRunwayadvisoryistoprovidecrewawarenessofanextendedholdingperiodontherunway.
AnnunciationCriteria
RAASgeneratestheadvisorywhenthefollowingconditionsaremet:
Aircraftmustbeontherunway,and
Aircraftheadingiswithin20degreesofrunwayheading,and
Aircraftalongtrackdistancedoesnotchangemorethan100feetinaperiodoftime considered to be an extended holding period (the time period can beconfigured60,90,120,180,240,or300seconds).Theadvisorymayberepeatedagainafter30,60,90,120,180,240,or300seconds.
ExtendedHoldingOnRunwayadvisoriesaresuppressedafteraRejectedTakeoffisdetected.Theadvisoryisresetwhentheaircraftleavestherunway.
MessageContent
Afterthespecifiedtimeperiodhaselapsed,RAASgeneratesanadvisorythatconsistsoftheauralmessage“OnRunway”followedbytherunwayidentifier.Thisadvisoryis
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annunciatedtwiceforeachtimeinterval.Forexample,ifanaircraftisclearedtolineupandwaitonrunway22,and,afterwaitinginpositionforanextendedperiod,say90seconds,thesystemwillannunciate“OnRunwayTwoTwo,OnRunwayTwoTwo”.
Iftheaircraftcontinuestoholdforanotherperiodoftime,whichmaybesetforthesametimeintervaloradifferentone,theabovemessagewouldrepeat.TherepeatmessagecanalsobeconfiguredtobeOFF.
AdvicetoOperator
TheOperatorneedstotakeintoaccountnormalwaitingtimesATCmayimposeonaircraftfortheroutenetworkoperated.
Selectextendedholdingtimeonrunway,initial(inseconds)
(4.3.5)
OFF 60 90 120 180 240 300
Selectextendedholdingtimeonrunway,repeats(inseconds)
(4.3.5)
OFF 30 60 90 120 180 240 300
5.3.6 Taxiway Takeoff (Product Description 4.3.6)
5.3.6.1 Taxiway Takeoff advisory
ThepurposeoftheTaxiwayTakeoffadvisoryistoenhancecrewawarenessofexcessivetaxispeedsoraninadvertenttakeoffonataxiway.
AnnunciationCriteria
Theadvisoryisgeneratedif:
Groundspeedoftheaircraftexceeds40knots,and
Aircraftisnotalignedwiththerunway.
Note: RAASfunctionsarebasedonadatabaseofrunwaylocations.Thesystemdoesnothaveknowledgeofthelocationsoftaxiways.
MessageContent
Theauralmessagestring“OnTaxiwayOnTaxiway”isannunciatedeachtimetheadvisoryisgenerated.
5.3.6.2 Taxiway Takeoff caution
ItmaybedesiredtoclassifytaxiwaytakeoffasaCautionconditionratherthanadvisory.
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AnnunciationCriteria
Sameasfortheadvisoryconditionabove.
MessageContent
Theauralstring“CautionOnTaxiwayOnTaxiway”isannunciatedonceeachtimethecautionisgenerated.
AdvicetoOperator
Someairfieldsuseataxiwayasasubstituterunwayonatemporarybasis.Whenusingsuchtaxiwaysasarunway,thecrewproceduresshouldindicateabriefingtoexpectamessageduringthesubsequenttakeoffcanbeexpectedandthatitmaybeignored.
TheOperatorneedstoevaluatetherelevanceanddesirabilityofeachfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperation.
EnableTaxiwaytakeoff(4.3.6) OFF ON
SelectAlertStatus(4.3.6)
(SeeNotes1&2,below)Advisory Caution
Notes
Note1:Table4‐1–RAASFunctionSelectionsandDescriptionsintheprevioussectionindicatesforeachfunctionthetypeofmessageandwhetherthealertlevelisconsideredacautionoradvisorymessage.VisualmessagesontheTerraindisplaycanbeselectedforeachauralannunciationexceptfortheLongLandingDistanceRemaining(8.0),RAASDistanceRemaining(4.2.4and4.3.7)andtheRAASRunwayEnd(4.2.5)callouts.
Note2:EASACRI
Forthecautionlevelalert,theEASACRIstatesthatanAbnormal/Non‐normaloperatingprocedureshouldbeestablishedanddocumentedintheAirplaneFlightManualSupplement(AFMS)tosilence(inhibit)theTaxiwayTakeoffalertwhenanticipatingtakingofffromataxiway.TheCRIemphasizesthisprocedureisusedforexceptionalcasessuchastemporaryrunwayclosures.
5.3.7 Distance Remaining – Rejected Takeoff advisory (Product Description 4.3.7)
RAASactivatesdistanceremainingadvisoriestoprovidetheflightcrewwithpositionawarenessduringaRejectedTakeoff(RTO).
AnnunciationCriteria
Theadvisoryisgeneratedif:
Aircraftisonarunway,and
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Groundspeedisgreaterthan40knots,and
Aircraft ground speed during the takeoff roll decreases by 7 knots from itsachievedmaximum,and
Aircraftisonthelasthalfoftherunway(default)orspecifieddistancefromtherunwaystopend.
RAASwillprovidedistanceremainingadvisoriesuntilthegroundspeeddecreasesbelow40knots,whentheadvisorieswillterminate.
ExtendedHoldingOnRunwayadvisoriesaresuppressedafteraRejectedTakeoffisdetected.Theadvisoryisresetwhentheaircraftleavestherunway.
MessageContent
Forsystemsusingfeetastheunitoflength,theseadvisoriesaregeneratedatwholethousand‐footintervals,withlastpossibleadvisoryoccurringat500feet.Forexample,aRAASequippedaircraftabortingatakeoffona9000footrunway,withtheDistanceRemainingadvisoryissuedatthelasthalfoftherunway,wouldgeneratethefollowingadvisories:“Four‐ThousandfeetRemaining”,“Three‐ThousandRemaining”,“Two‐ThousandRemaining”,“One‐ThousandRemaining”,and“Five‐HundredRemaining”.Asecondexample,aRAASequippedaircraftabortingatakeoffona9000footrunway,withtheDistanceRemainingadvisoryissuedstartingat2000feetwouldgeneratethefollowingadvisories:“Two‐ThousandfeetRemaining”,“One‐ThousandRemaining”,and“Five‐HundredRemaining”.
Forsystemsusingmetersastheunitoflength,theseadvisoriesaregeneratedatmultiplesof300meterintervals,withlastpossibleadvisoryoccurringat100meters.Forexample,aRAASequippedaircraftabortingatakeoffona3000meterrunway,withtheDistanceRemainingadvisoryissuedatthelasthalfoftherunway,wouldgeneratethefollowingadvisories:“One‐Thousand‐Two‐HundredMetersRemaining”,“Nine‐HundredRemaining”,“Six‐HundredRemaining”,“Three‐HundredRemaining”,and“One‐HundredRemaining”.Asecondexample,aRAASequippedaircraftabortingatakeoffona3000meterrunway,withtheDistanceRemainingadvisoryissuedstartingat600meterswouldgeneratethefollowingadvisories:“Six‐HundredMetersRemaining”,“Three‐HundredRemaining”,and“One‐HundredRemaining”.
AdvicetoOperator
Forlargeheavyaircraft,whichgenerallyuseabalancedfieldlength,thedefaultoption(lasthalfofrunway)willbetheappropriateonetochoose.However,forsmallerrelativelylightaircraftadistancefromtherunwayendcouldbemoreappropriatetoavoidunnecessarycalloutsforarelativelyrareoccurrence,particularlyiftheaircraftconsistentlyoperatesfromrelativelylongrunways.
TheOperatorshoulddeterminethemeanweightandthrustusedaswellastheaverageweatherconditionstheaircrafttypeoperatesin.ThedatacanbereadilyavailableiftheOperatorhasaFOQAprograminplaceforallflights.IntheseconditionsdeterminethedistancerequiredtoacceleratetoV1andthedistancerequiredtostopfromV1.Fromthesefiguresdeterminewhethertheaircraftwillnormally(fortheroutenetworkoperated)achieveV1withinthefirsthalfoftherunway,inwhichcasethecalloutswill
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generallynotbenecessary.However,itisrecommendedcalloutsbegivenfortheremaining2000feetregardless,giventhataRTOisararelyperformedmaneuver.ForanRTO,Crewshouldbeawareofarealisticspeedfortheaircrafttobeat,at2000ftand1000ftonarunwaytoensureastopwithinthatdistance.
SelectdistanceremainingRejectedtakeoff(4.3.7)
OFF 50%ofrunway
1000feet
(300m)
2000feet
(600m)
3000feet
(900m)
4000feet
(1200m)
5000feet
(1500m)
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
5.3.8 Taxiway Landing caution (Product Description 4.3.8)
Thepurposeofthetaxiwaylandingcautionistoprovidecrewawarenessthattheaircraftisnotlinedupwitharunwayatlowaltitudes.
AnnunciationCriteria
Thecautionisgeneratedif:
Aircraftisairbornebetween150and250feetAGL,and
Aircraftclimbrateislessthan450FPM,and
Aircraftiswithin5NMofarunwayandisnotlinedupwitharunway.
Note: RAASfunctionsarebasedonadatabaseofrunwaylocations.Thesystemdoesnothaveknowledgeofthelocationoftaxiways.
MessageContent
Theauralmessagestring“CautionTaxiwayCautionTaxiway”isannunciatedonceeachtimethecautionisgenerated.
AdvicetoOperator
Someairfieldsuseataxiwayasasubstituterunwayonatemporarybasis.Whenusingsuchtaxiwaysasarunway,thecrewproceduresshouldindicateabriefingtoexpectamessageduringthesubsequentapproachandthatitmaybeignored.
Considerationshouldbegiveniffrequentlyoperatingintorunwayswithlargeoffsetapproaches(LDA,circling,etc)wheretheaircraftisnotalignedwithin20degreesofrunwayheadinguntilwellbelow250feetAGL,asnuisancealarmsmayresult.
EnableTaxiwayLanding(4.3.8)
(SeeNote1,below)OFF ON
Notes
Note1:TheEASACRIstatesthatanAbnormal/Non‐normaloperatingprocedureshouldbe
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establishedanddocumentedintheAirplaneFlightManualSupplement(AFMS)tosilence(inhibit)theTaxiwayLandingalertwhenanticipatinglandingonataxiway.TheCRIemphasizesthisprocedureisusedforexceptionalcasessuchastemporaryrunwayclosures.
5.4 Stabilized Approach Monitor (Product Description 5)
TheStabilizedApproachMonitorisintendedtoinformtheflightcrewofawarenessofunstableapproachesandthusreducelandingrisksandpotentialrunwayexcursions.
Stabilized Approach Monitor
Enable stabilized approach monitor (SAM)
(See Note 1, below)
OFF (if OFF, skip Landing Flap, Excessive Approach Angle, and Excessive Approach
Speed Monitors)
ON
Select SAM Enable / Inhibit Discrete
None*
Ground or 28V = Inhibit
Ground or 28V = Enable
BOTH1ST : Ground or 28V = Enable2nd : Ground or 28V = InhibitNOTE: Only valid for MKV‐A
*Select “None” if SAM was already selected as part of the RAAS Enable / Inhibit Switch Configuration
SAM Discrete Connector Pin (ex: TP1A) 1st 2nd
SAM Enable / Inhibit Switch Configuration
If installing a SAM Enable / Inhibit Discrete, select one Option
Option 1: SAM
Option 2: SAM +CAM*
*NOTE: Options including CAM can only be selected for an “Inhibit” Discrete
Select Voice Gender Female Voice Male Voice
Notes
Note1:TheStabilizedApproachMonitor(SAM)canbeinhibitedusingtheRAASInhibitSwitchifinstalledandproperlyconfigured.SeetheRAASCommonSelectionsTableinSection5.1forinformationregardingtheselectionandconfigurationofRAASInhibitSwitch.
5.4.1 Landing Flap Monitor (Product Description 5.2.1)
AnnunciationCriteria
Thisfunctionprovidesa“FlapspauseFlaps”auralannunciationifthelandingflapsarenotsetatanOperatorchosenheight(500ft–1400ft)AFE.
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Thisfirst(Upper)LandingFlapMonitorannunciationisgeneratedwhenthefollowingconditionsaremet:
TheUpperFlapalertisenabledviatheRCD,and
FlapsarenotinLandingConfiguration,and
HeightAFEislessthanorequaltoanOperatorchosenheight(500ft–1400ft).
A“Flaps–Flaps”(nopauseinbetween)auralannunciationisprovidediftheaircraftisalignedwiththerunwayandthelandingflapsarestillnotsetatanOperatorchosenheight(500ft–1000ft)AFE.
Thesecond(Lower)LandingFlapMonitorannunciationisgeneratedwhenthefollowingconditionsaremet:
TheLowerFlapalertisenabledviatheRCD,and
FlapsarenotintheLandingConfiguration,and
HeightAFEis lessthanorequaltoanOperatorchosenheight(500ft–1000ft),and
Aircraft is linedupwith a runway (aircraft iswithin approximately 3 nauticalmilesof the runwayandaircraft track is alignedwith the runwaywithin±20degrees).
MessageContent
Theauralmessageconsistsofthephrase“Flaps(pause)Flaps”andisissuedoncefortheinitialentryintotheenvelopewhenflapsarenotinlandingconfigurationandtheaircraftisnotnecessarilyalignedwiththerunway.Thephrase“FlapsFlaps”isissuedoncewhenflapsarenotinlandingconfigurationandtheaircraftisalignedwiththerunway.
AdvicetoOperator
First/UpperLandingFlapMonitorheightAFE
Ascrewsareexpectedtohavetheaircraftfullystabilizedwithlandingflapsetby1000feetAFE,thisuppergateissetbydefaultto950feetAFE.Forlargeraircraftthatperformonlystraight‐inapproachesorforoperatorswithSOPsdemandinganearlierstabilizationpoint,considerationcanbegiventoahigherfigure(i.e.1200feetAFE).However,foraircraftlikelytoperformcirclingapproacheswherelandingflapwillbesetbelow1000feetAFE(businessjets),considerationshouldbegiventosettingtheuppergateOFF(andraisingthelowergate).
Second/LowerLandingFlapMonitorheightAFE
Afterthefirst/uppergatecalloutthecrewneedstimetosetflapstothelandingpositionandcompletethechecklist.Thereforethislowergateissetbydefaultto600feetAFE(uppergateminus350feet).Asmentionedabove,ifaflapalertONLYWHENALIGNEDWITHTHERUNWAYisdesired,thentheuppergatecanbedisabled,andthislowergatecanbesetto600to800feetdependingonpreference.
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EnableLandingFlapMonitor(5.2.1)
UpperFlapGateAlert OFF ON
LowerFlapGateAlert OFF ON
FlapGateMaximumAltitude
(SeeNote1,below)
AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
UpperFlapGate(feet)
950feet
LowerFlapGate(feet)
600feet
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
5.4.2 Excessive Approach Angle Monitor (Product Description 5.2.2)
ThepurposeoftheExcessiveApproachAngleMonitorannunciationistoprovidetheflightcrewwithawarenessofapossibleunstabilizedapproachiftheapproachangletothedestinationbecomestoosteep.
AnnunciationCriteria
Thefunctionprovidesa“TooHigh‐TooHigh”annunciationiftheapproachangletotherunwaybecomestoosteep.
Theaircraftmustbelinedupwithdestinationrunwayonfinalapproachtoenablethisfunction.Whenacirclingapproachisflown,theaircraftcanflyovertherunwayonadownwindleg,whichmakesthecomputedangletotherunwayverylarge.Therefore,theExcessiveApproachAngleMonitorisnotenableduntil600feetAFE(minimumcirclingminima)unlesstheaircraftisfullyconfiguredtoland.
Note:thereisaneffective450feetlowerlimitwheretheunstablevoicewouldtakeprecedence.
MessageContent
Theauralmessageconsistsofthephrase“TooHigh‐TooHigh”andisissuedoncewhentheaircraftmeetstheconditionsdescribedin5.2.2.1oftheProductDescription.
AdvicetoOperator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofthisfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperationandotherselections.
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EnableExcessiveApproachAngleMonitorAdvisory(5.2.2)
OFF ON
5.4.3 Excessive Approach Speed Monitor – (Product Description 5.2.3)
ThepurposeoftheExcessiveApproachSpeedMonitorannunciationistoprovidetheflightcrewwithawarenessofapossibleunstableapproachduetoexcessiveapproachspeeds.
AnnunciationCriteria
Thefunctionprovidesa“TooFast‐TooFast”annunciationiftheaircraftapproachspeedbecomestoofastcomparedtothetargetapproachspeed(VreforVapp).
TheExcessiveApproachSpeedMonitorannunciationisgeneratedwhenallofthefollowingconditionsaremet.
HeightaboveFieldElevationislessthanorequalto950feet(default)withgearandflapsinlandingconfigurationOR
HeightaboveFieldelevationislessthanorequalto600feet(default)regardlessof gear and flap configuration if Aircraft is linedupwith a runway (aircraft iswithinapproximately3NMoftherunwayandaircrafttrackisalignedwiththerunwaywithin±20degreesAND
HeightaboveAirfieldElevationandExcessiveSpeed(ComputedAirspeedminusApproach Speed (Vref orVapp) violate the excessive speed curve (ref ProductDescription5.2.3.1).
MessageContent
Theauralmessageconsistsofthephrase“TooFast‐TooFast”andisissuedoncewhentheaircraftmeetstheconditionsdescribedinsection5.2.3.1oftheProductDescription.
AdvicetoOperator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofthisfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperationandotherselections.
EnableExcessiveApproachSpeedMonitorAdvisory(5.2.3)
(SeeNote1,below)
OFF ON
Checklist:
Thismonitoriscurrentlyonlyavailableonsomeairframes.RefertoAppendixHoftheProductDescriptionSmartRunway®/SmartLanding®FunctionsoftheEnhancedGroundProximityWarningSystem(060‐4564‐001).
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ThefollowingconsiderationsarevaluablefortheTC/STCApplicantandremaininthisdocumentforthatreason.TheyarenotnecessaryfortheOperatorwhenmakingdecisionsregardingRCDselections.
ForAirbusaircraftthismonitorrequiresanewconnectiontotheFMGCtosupplythethreesignalsdefinedinICDsection4.1.1.142.AlsoconfirmboththattheFMGCsuppliesthisdatainthespecifiedformat,andthattheMKVaircrafttypeinterfacebeinguseddefinestheinputbusasillustratedinthefollowingexample:
Example1:A319/320/321MKVAircraftType113,inputfromFMGCtoEGPWSchannel14wasaddedtosupportthisfunction.
ForBoeingaircraftthismonitorrequiresasourceofApproach/ReferenceSpeed(perICDsections4.1.1.141or4.1.1.61.1).Confirmboththattheaircraftsuppliesthisdatainthespecifiedformat,andontheexistingbusconnectedtotheEGPWS,andthattheMKVaircrafttypeinterfacedefinestheinputasillustratedinthefollowingexamples:
Example2:B737‐600MKVAircraftType195,Label070/072wasaddedtoFMCBus1(channel2)&FMCBus2(channel18).
Example3:B777‐200LR/300ERMKVAircraftType208,ReferencespeedbroughtinonbothAIMSIRSbuses(channels1&2).
DotheAircraftandEGPWSsupportExcessiveApproachSpeedMonitor?
EGPWSICDAircraftTypesupportsApproach/ReferenceSpeed? YES NO
AircraftFMS/FMGC,AIMS,orEFISmatchestheEGPWSinterface
Forexample,anFMSmaynotprovidetheneededdataunlesstheSpeedTapeoptionisactivated.
YES NO
AircraftFMS/FMGC,AIMSorEFISpartnumber:
AircraftFMS/FMGC,AIMSorEFISSoftwarelevel:
UsethisareaifmorethanoneFMStypeused:
Note1:Ifafunctionisenabledandthesignalsrequiredforthatfunctionarefailedornotavailableontheaircraft,thenthefunctionwillbeinoperative.ForaTableofaircraftwhichsupporttheExcessiveSpeedMonitorseetheProductDescription060‐4564‐001AppendixH.
SAM Speed Curve – Select one of the three options below IF “Enable Excessive Approach Speed Monitor Advisory” is ON
Curve A YES NO
300 feet – 15 knots
500 feet – 15 knots
950 feet – 40 knots
950 feet – 40 knots
950 feet – 40 knots
Curve B YES NO
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300 feet – 30 knots
500 feet – 30 knots
950 feet –40 knots
950 feet –40 knots
950 feet –40 knots
Custom‐ If selecting this option, fill‐in the points below [Altitude (feet) ‐ Excessive Speed (knots)]
YES NO
5.5 Corrected Altimeter Monitor (Product Description 6)
Note: The Above Transition Altitude feature is recommended for North American airspace operations ONLY, see Service Information Letter D201009000033.
AnnunciationCriteria(BelowTransitionAltitude)
TheBelowTransitionAltitudeMonitorannunciationisgeneratedwhenthefollowingconditionsaremet:
GPSAltitudeandVerticalFigureofMerit(VFOM)arevalidandhavepassedtheinternalreasonablenesschecks.
GPS is not in altitude aiding mode, the number of satellites tracked is 5 orgreater, a non‐isolatable satellite failure (NISF) does not exist, and GPSHorizontalIntegrityLimit(HIL)isvalid.
CorrectedBarometricAltitudeandStaticAirTemperaturearevalid.
EGPWSRunwaydatabaseisvalid.
AircraftAltitudeislessthantheTransitionAltitudeformorethan30secondsORheightaboveairfield is less than1500 feet. The transitionaltitude isobtainedfromtheEGPWSrunwaydatabaseforthedestinationrunway.
Aircraftiswithin20NMoftheEGPWSselecteddestinationrunway.
Heightaboveairfieldislessthan5000feet.
Airport isnot indicatedasQFE,altimetersetting isnotQFE,andQFEprogrampinisnotselected.
RadioHeightisgreaterthan600feet.
The filtereddifferencebetweenCorrectedAltitudeandGPSAltitude exceeds athresholdcomputedbasedonthecurrentestimatedaltimetrysystemerrors.
MessageContent
Theauralmessageconsistsofthephrase“AltimeterSetting”.Thisadvisoryisissuedoncewhenthealtimetererrorisfirstdetectedandwillrepeatonce,8secondslateriftheerrorpersists.Aftertwovoicemessages,noadditionalmessageswillbegenerated.
AnnunciationCriteria(AboveTransitionAltitude)
The Corrected Barometric Altitude, Uncorrected Barometric Altitude, and
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RunwayDatabasearevalid.
Theaircrafthasbeenabovethetransitionaltitudeformorethan30secondsandnotmorethan5minutes.
ThedifferencebetweenCorrectedAltitudeandUncorrectedAltitudeislessthanthe fixed threshold or the Barometric Altitude does not equal standard,dependingontheselectedaircrafttype.
MessageContent
Theauralmessageconsistsofthephrase“AltimeterSetting”.Thisadvisoryisissuedoncewhenthealtimetererrorisfirstdetectedandwillrepeatonce,8secondslateriftheerrorpersists.Aftertwovoicemessages,noadditionalmessageswillbegenerated.
AdvicetoOperator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofeachfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperationandotherselections.
Corrected Altimeter Monitor
Enable Altimeter Monitor (6.)
(See Note 1, below)
OFF ON
Select Voice Gender Female Voice Male Voice
Select CAM Inhibit Discrete (Note 1) None
Inhibit*
*CAM Inhibit is available for any MKV‐A, or MK V if using software ‐236‐236 or later.
CAM Discrete Connector 2 Pin (ex: TP1A) – If installing a CAM Inhibit Discrete
Enable Altimeter Monitor Below Transition Altitude (6.2.1)
OFF ON By RCD Program Pin
Enable
By Discrete Enable
NOTE: Only valid for MKV‐A
Enable Altimeter Monitor Above Transition Altitude (6.2.2)
OFF ON By RCD Program Pin
Enable
By Discrete Enable
NOTE: Only valid for MKV‐A
CAM Discrete Connector Pin (ex: TP1A) –If transition altitude controlled by Discrete Enable
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Corrected Altimeter Monitor
Note1:TheCorrectedAltimeterMonitor(CAM)canbeinhibitedusingtheRAASInhibitSwitchifinstalledandproperlyconfigured.SeetheRAASCommonSelectionsTableinSection5.1forinformationregardingtheselectionandconfigurationofRAASInhibitSwitch.
5.6 Takeoff Flap Configuration Monitor (Product Description 7)
ThepurposeoftheTakeoffFlapConfigurationMonitoristoprovidetheflightcrewwithawarenessofimproperflapsettingwhentheaircraftislined‐uponarunwayinadvanceoftakeoff.
AnnunciationCriteria
TheTakeoffFlapConfigurationMonitorannunciationisgeneratedwhenthefollowingconditionsaremet:
FlapHandlenotsettoavalidtakeoffflapsetting,and
Aircraftentersarunway,and
Aircraftheadingiswithin±20degreesoftherunwayheading.
MessageContent
Theauralmessageconsistsofthephrase“FlapsFlaps”.Thisauralmessageisannunciatedonceeachtimetheaircraftenters,andisalignedwiththerunway.Nofurtherauralmessagesoccurunlesstheflaphandleisadjustedand,after5secondsofsettlingtime,theflapsarestillnotsetwithinthevalidtakeoffsettingrange.ShouldthePilotadjusttheflapsafterthefirstauralmessagebutfailtosettakeoffflaps,anadditional“FlapsFlaps”messageisprovided.Eachtimeanewflapsettingismade,theauralwillbeprovidedifflapsarenotwithinthetakeoffflaprange.
IftheRAASOnRunwayadvisoryisenabled,“FlapsFlaps”isappendedattheendoftheOnRunwayauralmessage.Forexample,“OnRunwayTwo‐Four,FlapsFlaps”.
AdvicetoOperator
TheOperatorneedstoevaluatetherelevanceanddesirabilityofeachfunctioninrelationtoroutenetwork,crewexperienceandtypeofoperation.
Notes
TheTakeoffFlapselectionbelowmustreflecttheAFM.
On some aircraft, the flap handle to flap angle conversion has an associatedtolerance.Thesettingenteredbelowshouldaccountforthesetolerances.
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TakeoffFlapConfigurationMonitor
EnableTakeoffFlapConfigurationMonitor(7.)(SeeNotes1&4,below)
OFF ON
SelectVoiceGender FemaleVoice MaleVoice
Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
TakeoffFlapHandleMinimumSetting
(SeeNote2,below)
50
TakeoffHandleMaximumSetting
(SeeNote3,below)
100
FlapAngleChecklist
NoteveryaircraftwillsupportFlapAngleMonitorfunctionality.
Foracompletelistofsupportedaircrafttypes,seeAppendixGoftheProductDescriptionSmartRunway®/SmartLanding®FunctionsoftheEnhancedGroundProximityWarningSystem(document060‐4564‐001).
DoAircraftandEGPWSsupportTakeoffFlapConfigurationMonitor?
EGPWSICDAircraftTypesupportsFlapAngle? YES NO
AircraftinterfacematchestheEGPWSinterface? YES NO
Notes
Note1:RAAS,TakeoffFlapsMonitor,andLongLandingMonitorsharethesameRAASProgramPinEnableDiscrete.SeetheRAASCommonSelectionsTableinsection5.1regardingtheRAASProgramPinEnableDiscrete.
Note2:Minimumflaphandlesetting,indegrees(0‐50),requiredforsafetakeoff.FlapselectionmustreflectAFM.
Note3:Maximumflaphandlesetting,indegrees(0‐50),requiredforsafetakeoff.FlapselectionmustreflectAFM.
Note4:EASACRI
TheEASACRIstatesthatanAbnormal/Non‐normaloperatingprocedureshouldbeestablishedanddocumentedintheAirplaneFlightManualSupplement(AFMS)tosilence(inhibit)theTakeoffFlapConfigurationalertwhenanticipatingTakeoffwithoutaLandingFlapselection.
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5.7 Long Landing Monitor (Product Description 8)
TheLongLandingMonitoraddstwoannunciationstoenhancecrewawarenessofaircraftalong‐trackpositionrelativetotherunwayend.Oneprovidesannunciationiftheaircrafthasnottoucheddownbeforeaconfigurabledistanceandthesecondprovidesairborneonlyauralannunciationsofcurrentdistanceoftheaircrafttotherunwaystopend.
AnnunciationCriteria
TheLongLandingandairborneonlyDistanceRemainingalertsaregeneratedwhenthefollowingconditionsaremet:
Aircraftiswithin100ftAGL,beyondacustomerspecifieddistance.
Aircraftisairborneabove5ftAGL,orweightonwheelsisfalse.
ThecallouttriggersaredefinedbyseveralRCDitems:
1. Calloutactivationrelativetodistancefromapproachendofrunway.2. Percentageofrunwayremainingtotriggercallouts.3. Fixeddistancefromstopendofrunwaytotriggerthedistanceremaining
calls.
MessageContent
Iftheaircrafthasnottoucheddownbeforeaconfigurablethreshold,theEGPWSwillissuethedefaultaural“LongLanding‐LongLanding”(themessagecanbeconfiguredto“DeepLanding–DeepLanding”).Inaddition,airborneonlyauralannunciationsofcurrentdistancefromaircrafttotherunwaystopendcanbeenabled.
AdvicetoOperator
I. Selectionof“LongLanding”or“DeepLanding”calloutinstigationpoints.SelectedasaDistancefromtheapproach(threshold)end:Ifitcanbeascertainedthatbyfarthemajorityoflandingsareonrunwaysgreaterthan8000feet(~2400m)thentherelevantdistancetochooseis3000feet(~900m).Thiswillensurethatthecrewareadvisedwhentheaircraftisairbornebeyondtheassociated3000feettouchdownzoneonan8000feetorlongerrunway.
Ifthemajorityoflandingsareonrunwayslessthan8000feet(~2400m),thentherelevantdistanceis2000feet(~600m).Thiswillensurethatthecrewareadvisedwhentheaircraftisairbornebeyondtheassociated2000feettouchdownzone.
Note:ReceivingLongLanding/DeepLandingcalloutswhileoverthetouchdownzonewouldtypicallybeconsiderednuisancealertsandtherefore,shouldbeavoided.Howeverconsistentlylandingonshorterrunwaylengthsmaybeasufficientreasontoestablishadistancelessthan3000feet.Inthiscase,theoperatorshouldestablishadistanceconsistentwiththeirSOP.
SelectedasaPercentagefromthedeparture(stop)end:
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Accordingtoindustrystandards,theaircraftshouldtypicallytouchdowninthefirstonethirdoftherunway.Therefore,therelevantminimumpercentagetobeselectedfromthestopendshouldbe67%.ThiswillensurethattheLongLandingalertwillbeprovidedinaccordancewiththisstandardwhenlandingonshorterrunways.
II. Selectionofinstigationpointofdistanceremainingcallouts.SelectedasaDistancefromthedeparture(stop)end:
TherearetwoconsiderationswhenselectingtheLongLandingDistanceRemaining(LLDREM)callout.
1. PriortotheadditionoftheLongLandingDistanceRemaining(LLDREM)function,theRAASDREMLanding&Rollout(L&R)function(seeSection5.2.4)wouldhavetypicallybeensetat50%oftherunwaylength.WiththeadditionoftheLLDREMfunction,therelevantDREML&Rtriggershouldbe2000feetorlessfromthestopend.TheLLDREMDistancewouldbeselectedatgreaterthantheDREML&RsoastoprovideadequateDREMcoveragewithoutsignificantlyoverlappingcalloutranges.
2. ThetimebetweentheLLcalloutandtheLLDREMcalloutmustbesufficientsoastoallowtimefortheLLcallouttocomplete(approximately3seconds)plussufficienttimeforthecrewtointeractbeforetheLLDREMcalloutismade.Thisdistanceisontheorderof1000‐2000feetbetweencallouts.
ThediagrambelowrepresentswhatmightbearelevantrangefortheLL,LLDREM,andDREML&Rcalloutsonan8000feetrunway.
SelectedasaPercentagefromthedeparture(stop)end:
ThediscussionabovefortheLLDREMtriggeralsoappliestotheLLDREMPercentagetriggervalue.Forrunways8000feetorgreaterwithaLLcalloutof3000feetbeyondthethreshold,aLLDREMPercentageof60%fromstopendwouldprovideaLLDREMcalloutwithatleast4800feetremaining.Notethatwhen600feetorlessareavailablebetweentheLLandLLDREMcallouts,it’spossibletheLLcalloutwillnothavecompletedits
2000ft
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announcementbeforetheLLDREMistriggeredtooccur.TheLongLandingfunctionisdesignedtosuppresstheLLDREMcalloutuntiltheLLcalloutcompletes.Therefore,thefirstLLDREMcalloutmaybesuppressedresultinginaLLDREMcallouttooccur1000feetlaterthanexpected(atthenext1000feetLLDREMcallout).Note:HoneywellprovidesasimpleExcelspreadsheetthatcanassisttheapplicantin
determiningtheoptimalLongLandingDistanceandDistanceRemainingtriggerpoints.Itisavailablefordownloadviathefollowinglink:
http://www51.honeywell.com/aero/common/documents/egpws‐documents/raas‐documents/LongLanding.xls
Thefollowingexamplesdemonstratetheconceptsintroducedabove:Scenarios1and2inthetablesbelow,demonstratehowtheLongLanding(LL)DistanceandLLPercentagevaluesworktogethertoensureproperalertinginresponsetovaryingrunwaylengths.Inasimilarway,theLLDistanceRemaining(DREM)andLLDREMPercentagevaluesworktogether.
OnlongerrunwaysasinScenario1,theLLDistancetriggerissettoensuretheLLcalloutdoesnotoccurwhileinthetouchdownzone(Threshold+3000feet).HoweverwhenlandingonashorterrunwayasinScenario2,theLLPercentagetriggerisreachedbeforetheLLDistancetrigger.
Similarly,onthelongerrunwayinScenario1,theDREMPercentageensurestheLLDREMcalloutwilloccurwithasufficientamountofremainingrunway. OntheshorterrunwayinScenario2,theLLDREMisreachedbeforetheLLDREMPercentage.
Scenario 1: Long Landing Callout on a long runway lengthParameter Value/Setting Trigger Point
from Stop End
Result
Runway Length 10000 feet n/a n/a LL Distance 3000 feet from Approach
End 7000 feet 7000 > 6700 so LL Distance is the
source of the alert, not the LL Percentage LL Percentage 67% from Stop End 6700 feet
LL DREM 4000 feet from Stop End 4000 feet 6000 > 4000 so LL DREM Percentage is the source of the alert, not the LL DREM
LL DREM Percentage
60% from Stop End 6000 feet
DREM Landing & Rollout (L&R) (see Section 6.2.4)
2000 feet from Stop End 2000 feet On touchdown, DREM L&R is now the active callout and will alert at 2000 feet if groundspeed > 40 knots
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Scenario3belowdemonstrateshowtheLLPercentageandLLDREMvaluescanoperatewithoutspecifyingtheircorrespondingLLDistanceandLLDREMPercentage
values.
LongLandingMonitor
EnableLongLandingMonitor
(SeeNotes1,2,&3,below)
OFF ON
SelectVoiceGender FemaleVoice MaleVoice
Scenario 2: Long Landing Callout on a short runway lengthParameter Value/Setting Trigger Point
from Stop End
Result
Runway Length 6000 feet n/a n/a LL Distance 3000 feet from Approach
End 3000 feet 4020 > 3000 so LL Percentage is
the source of the alert, not the LL Distance (Note 1) LL % 67% from Stop End 4020 feet
LL DREM 4000 feet from Stop End 4000 feet 4000 > 3600 so LL DREM is the source of the alert, not the LL DREM Percentage (Note 1)
LL DREM % 60% from Stop End 3600 feet
DREM Landing & Rollout (L&R) (see Section 6.2.4)
2000 feet from Stop End 2000 feet On touchdown, DREM L&R is now the active callout and will alert at 2000 feet if groundspeed > 40 knots
Note 1 – When the LL callout (4020 feet) and LL DREM callout (4000 feet) are less than 600 feet apart, the LL DREM callout may not occur until 1000 feet later than expected (3000 feet) due to LL DREM callout suppression until the LL callout has completed its spoken message (approximately 3 seconds).
Scenario 3: LL Percentage and LL DREMParameter Value/Setting Trigger Point
from Stop End
Result
Runway Length 10000 feet n/a n/a LL Distance Not specified n/a n/a LL % 67% from Stop End 6700 feet LL callouts always occur with two
thirds of the runway remaining regardless of runway length
LL DREM 4000 feet from Stop End 4000 feet LL DREM callouts always occur with 4000 feet remaining. In this case, with plenty of time for the LL callout to output its spoken message and allow some crew dialog
LL DREM % Not specified n/a DREM Landing & Rollout (L&R) (see Section 6.2.4)
3000 feet from Stop End 3000 feet On touchdown, DREM L&R is now the active callout and will alert at 3000 feet
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LongLandingMonitor
Configurecallout “LongLanding”callout “DeepLanding”callout
LongLandingDistance FromApproachEnd FromDepartureEnd
Enterdistancefromselectedendinthetablebelow[1to3000feet(900meters)].
LongLandingpercentage OFF ON
SpecifyusingthesameendselectedforLongLandingDistance.
Enterpercentage(%)ofrunwayremaininginthetablebelow.
PercentageRemaining(0<K<1)–Thisisthe%ofrunwaythatwouldtriggertheauralifaircraftisnotontherunway. Forexample,asettingof0.60(60%)wouldtriggertheauraliftheaircrafthasnottoucheddowninthefirst40%oftherunway.
LongLandingDistanceRemainingCallout(LongRunway)
OFF ON
FromApproachEnd FromDepartureEnd
EnterDistancefromselectedendinthetablebelow[1to10,000feet(3000meters)].
LongLandingDistanceRemainingCalloutPercentage.
OFF ON
SpecifyusingthesameendselectedforLongLandingDistanceRemaining
Enterpercentage(%)ofrunwayinthetablebelow.
PercentageRemaining(0<K<1)–Thisisthe%ofrunwaythatwouldtriggertheDistanceRemainingCalloutsiftheaircraftisstillairborne. Forexample,asettingof0.60(60%)wouldtriggertheauraliftheaircrafthasnottoucheddowninthefirst40%oftherunway.
Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
LongLandingDistance(feetorm)fromThreshold
3000ft
LongLandingPercentage(%)of
67%
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LongLandingMonitor
RunwayLength
LongLandingDistanceRemaining(feetorm)fromStopEnd
4000ft
LongLandingDistanceRemainingPercentage(%)ofRunwayLength
60%
Notes
Note1:RAAS,TakeoffFlapsMonitor,andLongLandingMonitorsharethesameRAASProgramPinEnableDiscrete.SeetheRAASCommonSelectionsTableinsection5.1regardingtheRAASProgramPinEnableDiscrete.
Note2:TheLongLandingMonitorwillbetriggeredwheneithertheaircraftreachesthespecifieddistancefromtheselectedendoftherunwayorthespecifiedpercentageofrunwayremaining,whicheveroccursfirst.
Note3:EASACRI
TheEASACRIstatesthatanAbnormal/Non‐normaloperatingprocedureshouldbeestablishedanddocumentedintheAirplaneFlightManualSupplement(AFMS)tosilence(inhibit)theLongLandingalertwhenanticipatinglandingonarunwaywithatemporarydisplacedthresholdthusexceedingtheLongLandingtriggervalue.
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
5.8 Volume Requirements
TheOperatorwillselectavolumelevelfromwithinthecertifiedrangeofvolumelevelsasdefinedinthe‐003document(refertosection2–ApplicableHoneywellSTCDocuments).
AdvisoryaudioshouldnotbesoloudastointerferewithATCcommunications.Cautionaudiowillneedtobelouderthanadvisoriestoemphasizethesituationtothecrew.Therelevantvolumesshouldbeevaluatedonatestflightandadjustedappropriately.
GuidanceforadjustingandtestingvolumelevelscanbefoundintheHoneywellTestProcedureforAdjustableVolumeSettingsofRAASFunctions,document060‐4314‐080.ContactyourHoneywellFieldServiceRepresentativeortheTechnicalOperationsCenterforassistance.
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ReconfigureRCDVolume NO YES(IfYes,enterthevaluesbelowindecibels)
Ex:
2.2‐ApproachingRunwayonGround ‐6 dB
2.3‐OnRunway/InsufficientRunway– OnGnd ‐6 dB
2.4–ExtendedHoldingInitialandRepeated ‐6 dB
2.5–DistanceRemaining–RejectedTakeoff 0 dB
2.6–RunwayEnd 0dB
2.7–TaxiwayTakeoff +3dB
2.8–ApproachingRunway/ShortRunwayAir ‐6 dB
2.9–DistanceRemaining‐Landing 0 dB
2.10–TaxiwayLanding +3dB
2.11–StabilizedApproachFlapsFlaps 0dB
2.12–StabilizedApproachTooHigh 0dB
2.13‐StabilizedApproachTooFast 0dB
2.14–StabilizedApproachUnstable 0dB
2.15–AltimeterSetting 0dB
2.16–TakeoffFlapsMonitorFlapsFlaps 0dB
2.17–LongLanding 0dB
2.17–LongLandingDistanceRemaining 0dB
OperatoraddsabriefdescriptionofthemethodologyforchoiceofparametertotheRCDWorksheet
5.9 Adding Additional Comments
AdditionalcommentsmaybeaddedtotheCommentSectionatthebottomoftheRCDWorksheet(seeAppendixA).
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IfadditionalcustomizationofitemssuchasVisualMessageColororAlertAdvisoryCurvesisrequired,contactyourFieldServiceRepresentativeortheTechnicalOperationsCenter.
5.10 Additional Considerations
Warning/CautionLampFormat
TwoLampformatsaredefinedasafunctionofaircrafttype.ThelampformatdefinedforeachaircrafttypecanbefoundinthetablesofICDAppendixF.LampFormat1configuresEGPWStoactivateanamberannunciator(typically“BelowG/S”)forMode5Glideslopealerts.Allotheralerts(exceptWindshear)willactivatearedannunciator(typically“PullUp”).IfactivatingRAAScautionlevelalerts,LampFormat1maybedeemedacertificationriskasredannunciatorsareactivatedforcautionlevelalerts.AnotheroptionmaybetorequestRAAScautionsdonotactivateanyannunciatorviatheAdditionalCommentssectionabove.Toaddressthis,LampFormat2shouldbeusedifactivatingRAAScautionlevelalerts.LampFormat2configuresEGPWStoactivatearedannunciatoronlyforPullUpwarnings.Allotheralerts(exceptWindshear)willactivateanamberannunciator(typically“GPWS”).ThiswillensureRAAScautionlevelalertsareaccompaniedbyanamberannunciator.
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6 NOTES
6.1 Acronyms and Abbreviations
AFE Above Field Elevation
AGL Above Ground Level
CAM Corrected Altimeter Monitor
CRI Certification Review Item
EGPWS Enhanced Ground Proximity Warning System
FOQA Flight Operations Quality Assurance
ISA International Standard Atmosphere
LL Mon Long Landing Monitor
PCMCIA Personal Computer Memory Card International Association
RAAS Runway Awareness and Advisory System
RCD Reloadable Customer Definitions
RTO Rejected Take Off
SAM Stabilized Approach Monitor
SL SmartLanding®
SOPs Standard Operating Procedures
SR SmartRunway®
UOM Unit of Measure
USB Universal Serial Bus
V1 Takeoff Decision Speed
Vref Landing Reference Speed
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Appendix – RCD Worksheet
TheRCDWorksheetaccompanyingthisRCDSelectionGuideisa.pdfformattachment.ThisrequiresAdobeProtosavethedataenteredintheworksheet.IfAdobeProisnotavailabletheworksheetbelowshouldbeprintedasameansofsavingtheselections.
CompletedworksheetscanbesubmittedtoHoneywellOrderAdministration:
viafaxinUSA(913‐712‐1335)orINTL(+420234625777)
viaemailtoorders@honeywell.com
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 1 of 10
INSTRUCTIONS:
1) Refer to the RCD Selection Guide for the EGPWS Runway Advisory and Awareness System, Drawing Number 060-4314-082, for assistance is completing this worksheet.
2) Return the completed worksheet to Honeywell Order Administration. Fax in USA: 913-712-1335. Fax outside USA: +420-234-625-777
General Information Aircraft Operator
Date (MM/DD/YYYY)
Customer name/Company
Customer Phone/Fax/email
Ordering Information Customer: P.O. #: Requested Ship Date:
EGPWS P/N:
EGPWS S/N:
Model and Part Number Selection
Ex:
Columns are provided for up to nine separate aircraft types AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
OEM Aircraft Model 737-500
OEM Aircraft TN or SN (leave blank for fleet)
EGPWS Aircraft Type number 194
MK V, MK VII, or MKV-A EGPWS MK V
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 2 of 10
General RCD Information
Select RCD Enable Method RCD Master Key Enable Key Card
Add RAAS/SAM/CAM Program Pin Enable ICD Appendix D-15 (-230/-054/-004 and on) NO YES
EASA CRI Settings NO YES
Visual Messages on Terrain Display for Non-TSO Functions
Enable Visual Messages All Messages Non-routine Messages Only
Cautions Only None
Runway Awareness and Advisory System (RAAS) Common Selections
Select RAAS Enable On Off
Select RAAS Enable / Inhibit Discrete
None
Ground or 28V = Inhibit
Ground or 28V = Enable
BOTH 1ST : Ground or 28V = Enable 2nd : Ground or 28V = Inhibit NOTE: Only valid for MKV-A
RAAS Discrete Connector Pin (ex: TP1A) 1ST 2ND
RAAS Enable / Inhibit Switch Configuration
If installing a RAAS Enable / Inhibit Discrete, select one Option
Option 1: RAAS Discrete(s) applies to: Rwy + LL + T/O Flaps
Option 2: RAAS Discrete(s) applies to: Rwy + LL + T/O Flaps + SAM
Option 3: RAAS Discrete(s) applies to: Rwy + LL + T/O Flaps + CAM*
Option 4: RAAS Discrete(s) applies to: Rwy + LL + T/O Flaps + SAM +CAM*
*NOTE: Options including CAM can only be selected for an “Inhibit” Discrete
Add RAAS INOP Indicator NO YES
Select voice gender Female Male
Select Annunciation of Unit of Measure (UOM) Off First
Select Distance Unit of Measure (UOM) Feet Meters
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 3 of 10
Runway Awareness and Advisory System (RAAS) Common Selections
Ex:
AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
Select Advisory Suppress Window
450-550 (ft)
350-450 (ft)
GPS Antenna Location 35 ft
RAAS Routine Alerts
Enable Approaching Runway - in air (4.2.1) OFF ON
Enable Approaching Runway – on ground (4.2.2) OFF ON
Enable On Runway – on ground (4.2.3) OFF ON
Select Distance Remaining, Landing and Rollout (4.2.4)
OFF 50% of runway
1000 ft (300m)
2000 ft (600m)
3000 ft (900m)
4000 ft (1200m)
5000 ft (1500m)
Add a brief description of the methodology for choice of parameter
Enable Runway End advisory (4.2.5) OFF ON
RAAS Non-Routine Alerts
Select approaching short runway length – in air advisory (4.3.1)
OFF ON
(Enter nominal runway length below)
ALWAYS
(Enter a runway length of 99,999 ft making this a
Routine Alert) Short Runway Length - in air (ft or m) Ex:
AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
4500 ft
Add a brief description of the methodology for choice of parameter
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 4 of 10
Select Caution short runway in air (4.3.2) OFF ON
(if ON, enter nominal runway length below)
Caution Short Runway Length - in air (ft or m)
Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
4500 ft
Add a brief description of the methodology for choice of parameter
Select insufficient runway length on ground advisory (4.3.3)
OFF
ON
(Enter nominal runway length below)
ALWAYS
(Enter a runway length of 99,999 ft making this a
Routine Alert) Insufficient Runway Length – on ground (ft or m)
Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
4500 ft
Add a brief description of the methodology for choice of parameter
Select Caution short runway on ground (4.3.4)
OFF ON
(if ON, enter nominal runway length below)
Caution Short Runway Length – on ground (ft or m)
Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
4500 ft
Add a brief description of the methodology for choice of parameter
Select extended holding time on runway, initial (in seconds) (4.3.5)
OFF 60 90 120 180 240 300
Select extended holding time on runway, repeats (in seconds) (4.3.5)
OFF 30 60 90 120 180 240 300
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
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Select distance remaining Rejected takeoff (4.3.7)
OFF 50% of runway
1000 ft (300m)
2000 ft (600m)
3000 ft (900m)
4000 ft (1200m)
5000 ft (1500m)
Add a brief description of the methodology for choice of parameter
Enable Taxiway takeoff (4.3.6) OFF ON
Select Alert Status (4.3.6) Advisory Caution
Enable Taxiway Landing (4.3.8) OFF ON
Stabilized Approach Monitor Enable stabilized approach monitor (SAM)
OFF (if OFF, skip Landing Flap, Excessive
Approach Angle, and Excessive Approach Speed Monitors)
ON
Select SAM Enable / Inhibit Discrete
None*
Ground or 28V = Inhibit
Ground or 28V = Enable
BOTH 1ST : Ground or 28V = Enable 2nd : Ground or 28V = Inhibit NOTE: Only valid for MKV-A
*Select “None” if SAM was already selected as part of the RAAS Enable / Inhibit Switch Configuration SAM Discrete Connector Pin (ex: TP1A) 1st 2nd
SAM Enable / Inhibit Switch Configuration
If installing a SAM Enable / Inhibit Discrete, select one Option
Option 1: SAM
Option 2: SAM +CAM*
*NOTE: Options including CAM can only be selected for an “Inhibit” Discrete
Select Voice Gender Female Voice Male Voice
Enable Landing Flap Monitor (5.2.1)
Upper Flap gate Alert OFF ON
Lower Flap Gate Alert OFF ON
Flap Gate Maximum Altitude Ex:
AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
Upper Flap Gate (ft) 950 ft
Lower Flap Gate (ft) 600 ft
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 6 of 10
Add a brief description of the methodology for choice of parameter
Enable Excessive Approach Angle Monitor Advisory (5.2.2)
OFF ON
Enable Excessive Approach Speed Monitor Advisory (5.2.3)
OFF ON
Checklist: Do the Aircraft and EGPWS support Excessive Approach Speed Monitor?
EGPWS ICD Aircraft Type supports Approach/Reference Speed? YES NO Aircraft FMS/FMGC, AIMS, or EFIS matches the EGPWS interface For example, an FMS may not provide the needed data unless the Speed Tape option is activated.
YES NO
Aircraft FMS/FMGC, AIMS or EFIS part number:
Aircraft FMS/FMGC, AIMS or EFIS Software level: Use this area if more than one FMS type used:
SAM Speed Curve – Select one of the three options below IF “Enable Excessive Approach Speed Monitor Advisory” is ON
Curve A (Airbus) YES NO
300ft.–15Kts. 500ft.–15Kts. 950ft.–40Kts. 950ft.–40Kts. 950ft.–40Kts.
Curve B (Boeing and all other OEM) YES NO
300ft.–30Kts. 500ft.–30Kts. 950ft.–40Kts. 950ft.–40Kts. 950ft.–40Kts.
Custom- If selecting this option, fill-in the points below (Altitude(ft.)-Excessive Speed(Kts.))
YES NO
Corrected Altimeter Monitor Enable Altimeter Monitor (6.) OFF ON
Select Voice Gender Female Voice Male Voice
Select CAM Inhibit Discrete None*
Inhibit NOTE: Only valid for MKV-A
*Select “None” if CAM was already selected as part of the RAAS or SAM Enable / Inhibit Switch Configuration
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 7 of 10
Corrected Altimeter Monitor CAM Discrete Connector 2 Pin (ex: TP1A) – If installing a CAM Inhibit Discrete
Enable Altimeter Monitor Below Transition Altitude (6.2.1)
OFF ON
Enable Altimeter Monitor Above Transition Altitude (6.2.2)
OFF ON
CAM Discrete Connector Pin (ex: TP1A) – If transition altitude controlled by Discrete Enable
Takeoff Flap Configuration Monitor Enable Takeoff Flap Configuration Monitor (7.) OFF ON
Select Voice Gender Female Voice Male Voice
Select Enable/Inhibit discrete Takeoff Flap Configuration Monitor (and Long Landing Monitor) uses the same Enable/Inhibit discrete as RAAS. RAAS must be activated to activate this Takeoff Flap Configuration Monitor even if no RAAS functions are selected.
Ex:
AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
Takeoff Flap Handle Minimum Setting 5 °
Takeoff Flap Handle Maximum Setting 10 °
Flap Angle Checklist Do Aircraft and EGPWS support Takeoff Flap Configuration Monitor?
EGPWS ICD Aircraft Type supports Flap Angle? YES NO
Aircraft interface matches the EGPWS interface? YES NO
Long Landing Monitor
Enable Long Landing Monitor OFF ON
Select Voice Gender Female Voice Male Voice
Configure callout “Long Landing” callout “Deep Landing” callout
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 8 of 10
Long Landing Distance From Approach End From Departure End
Enter distance from selected end in the table below (1 to 3000 ft (900 meters)).
Long Landing percentage OFF ON
Enter percentage (%) of runway remaining in the table below.
Percentage Remaining (0<K<1) – This is the % of runway remaining that would trigger the aural if aircraft is not on the runway. For example, a setting of 0.60 (60%) would trigger the aural if the aircraft is not down and has reached the point of having used 40% of the runway. Long Landing Distance Remaining Callout (Long Runway) OFF ON
From Approach End From Departure End
Enter Distance from selected end in the table below (1 to 10,000 ft (3000 meters)).
Long Landing Distance Remaining Callout Percentage. OFF ON
Enter percentage (%) of runway remaining in the table below.
Percentage Remaining (0<K<1) – This is the % of runway remaining that would trigger the Distance Remaining Callouts if the aircraft is still airborne. For example, a setting of 0.60 (60%) would trigger the Distance Remaining callouts if the aircraft is not down and passed the point of having 60% of the runway remaining.
Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
Long Landing Distance (ft or m) from Threshold 3000ft
Long Landing Percentage (%) of Runway Length 67%
Long Landing Distance Remaining (ft or m) from Stop End
4000ft
Long Landing Distance Remaining Percentage (%) of Runway Length
60%
Add a brief description of the methodology for choice of parameter
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 9 of 10
Volume Settings See Section 6.4 in the RCD Selection Guide
Reconfigure RCD Volume NO YES (If Yes, enter the values below in decibels)
060-4314-080 Reference Ex: AC #1
AC #2
AC #3
AC #4
AC #5
AC #6
AC #7
AC #8
AC #9
2.2 - Approaching Runway on Ground -6dB
2.3 - On Runway/Insufficient Runway – On Gnd -6dB
2.4 – Extended Holding Initial and Repeated -6dB
2.5 – Distance Remaining – Rejected Takeoff 0dB
2.6 – Runway End 0dB
2.7 – Taxiway Takeoff +3dB
2.8 – Approaching Runway / Short Runway Air -6dB
2.9 – Distance Remaining - Landing 0dB
2.10 – Taxiway Landing +3dB
2.11 – Stabilized Approach Flaps Flaps 0dB
2.12 – Stabilized Approach Too High 0dB
2.13 - Stabilized Approach Too Fast 0dB
2.14 – Stabilized Approach Unstable 0dB
2.15 – Altimeter Setting 0dB
2.16 – Takeoff Flaps Monitor Flaps Flaps 0dB
2.17 – Long Landing 0dB
2.17 – Long Landing Distance Remaining 0dB
Add a brief description of the methodology for choice of parameter
Reloadable Customer Definitions (RCD) Worksheet for the Runway Awareness and Advisory System (RAAS)
Page 10 of 10
Comments