rcd selection guide for the egpws runway advisory and … · 2019. 9. 26. · the egpws...

Redmond, WA 060-4314-082 Rev -

CAGE Code 97896 11/19/13

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This document is an unpublished work.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

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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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PROPRIETARY NOTICE ON TITLE PAGE APPLIES

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)


DistanceRemaining,LandingandRoll‐out(4.2.4)(Off/50%ofRunway)

(1000,2000,3000,4000,5000feet)

RAAS Routine Advisory 5.2.4

RunwayEnd(4.2.5)



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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


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)


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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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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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


EnableApproachingRunway– onground(4.2.2) OFF ON

5.2.3 On Runway – On Ground advisory (Product Description 4.2.3)

ThepurposeoftheOnRunwayadvisoryistoprovidethecrewwithawarenessofwhichrunwaytheaircraftislinedupwithduringgroundoperations.


TheOnRunwayadvisoryisgeneratedwhenthefollowingconditionsaremet:

Aircraftentersontorunway,and

Aircraftheadingiswithin±20degreesoftherunwayheading.

MessageContent

Theauralmessageconsistsofthewords“OnRunway”followedbytherunwayidentifier,forexample,“OnRunwayTwo‐Four”.Thisadvisoryisannunciatedonceeachtimetheaircraftentersarunway.

AdvicetoOperator


EnableOnRunway–onground(4.2.3) OFF ON

5.2.4 Distance Remaining – Landing and Rollout advisory (Product Description 4.2.4)

ThepurposeoftheDistanceRemainingadvisoriesistoenhancecrewawarenessofaircraftalong‐trackpositionrelativetothestopendoftherunway.


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.


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.


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.


5.3.2 Approaching Short Runway – In Air Caution (Product Description 4.3.2)

Thepurposeofthisannunciationistoprovidethecrewwithanimmediateawarenessthattheavailablerunwaylengthforlandingislessthantherunwaylengthdefinedforthecautionmessage(ProductDescription4.3.1).

TheavailablerunwaylengthisdeterminedbytheEGPWSRunwayDatabase.

TheselectionofaCaution,inadditiontotheexistingadvisory,isconfigurableviatheRCD.

Ifthecautionisdesired,itisrecommendedthatboththeadvisoryandcautionareenabled.


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.



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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.


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”.


5.3.4 Insufficient Runway Length – On Ground caution (Product Description 4.3.4)

Thepurposeofthisannunciationistoprovidethecrewwithimmediateawarenessthattherunwaylengthavailablefortakeoffislessthanthedefinednominaltakeoffrunwaylengthwhenthetakeoffiscontinuedasnotedbelowaftertheremaininglengthfortakeoffhasbeenprovided.

Theavailablerunwaylengthisdeterminedbycomparingtheaircraft’spositionontherunwaywiththedistanceavailabledefinedintheEGPWSRunwayDatabase.



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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.


5.3.5 Extended Holding On Runway advisory (Product Description 4.3.5)

ThepurposeoftheExtendedHoldingOnRunwayadvisoryistoprovidecrewawarenessofanextendedholdingperiodontherunway.


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.


Theadvisoryisgeneratedif:

Groundspeedoftheaircraftexceeds40knots,and

Aircraftisnotalignedwiththerunway.

Note: RAASfunctionsarebasedonadatabaseofrunwaylocations.Thesystemdoesnothaveknowledgeofthelocationsoftaxiways.

MessageContent

Theauralmessagestring“OnTaxiwayOnTaxiway”isannunciatedeachtimetheadvisoryisgenerated.

5.3.6.2 Taxiway Takeoff caution

ItmaybedesiredtoclassifytaxiwaytakeoffasaCautionconditionratherthanadvisory.


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Sameasfortheadvisoryconditionabove.

MessageContent

Theauralstring“CautionOnTaxiwayOnTaxiway”isannunciatedonceeachtimethecautionisgenerated.

AdvicetoOperator

Someairfieldsuseataxiwayasasubstituterunwayonatemporarybasis.Whenusingsuchtaxiwaysasarunway,thecrewproceduresshouldindicateabriefingtoexpectamessageduringthesubsequenttakeoffcanbeexpectedandthatitmaybeignored.


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).


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)


5.3.8 Taxiway Landing caution (Product Description 4.3.8)

Thepurposeofthetaxiwaylandingcautionistoprovidecrewawarenessthattheaircraftisnotlinedupwitharunwayatlowaltitudes.


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


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*


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)


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


5.4.2 Excessive Approach Angle Monitor (Product Description 5.2.2)

ThepurposeoftheExcessiveApproachAngleMonitorannunciationistoprovidetheflightcrewwithawarenessofapossibleunstabilizedapproachiftheapproachangletothedestinationbecomestoosteep.


Thefunctionprovidesa“TooHigh‐TooHigh”annunciationiftheapproachangletotherunwaybecomestoosteep.

Theaircraftmustbelinedupwithdestinationrunwayonfinalapproachtoenablethisfunction.Whenacirclingapproachisflown,theaircraftcanflyovertherunwayonadownwindleg,whichmakesthecomputedangletotherunwayverylarge.Therefore,theExcessiveApproachAngleMonitorisnotenableduntil600feetAFE(minimumcirclingminima)unlesstheaircraftisfullyconfiguredtoland.

Note:thereisaneffective450feetlowerlimitwheretheunstablevoicewouldtakeprecedence.

MessageContent

Theauralmessageconsistsofthephrase“TooHigh‐TooHigh”andisissuedoncewhentheaircraftmeetstheconditionsdescribedin5.2.2.1oftheProductDescription.

AdvicetoOperator



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EnableExcessiveApproachAngleMonitorAdvisory(5.2.2)

OFF ON

5.4.3 Excessive Approach Speed Monitor – (Product Description 5.2.3)

ThepurposeoftheExcessiveApproachSpeedMonitorannunciationistoprovidetheflightcrewwithawarenessofapossibleunstableapproachduetoexcessiveapproachspeeds.


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


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





Curve B YES NO


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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 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.


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


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.


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.


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


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)

[email protected]

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:


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


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


Select RAAS Enable On Off

Select RAAS Enable / Inhibit Discrete

None



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*


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


Page 3 of 10


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



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


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


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


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


Page 5 of 10

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)


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*



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*



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


Page 6 of 10


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 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


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 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


Configure callout “Long Landing” callout “Deep Landing” callout


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%



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



Page 10 of 10

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