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Honeywell MKXXII installation manual MK Xxii Egpws Configuration Module

Models: MKXXII

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	Honeywell
	MK XXII EGPWS Installation Manual
STEP 6	Organize and dress wiring exiting from backshell. Route Configuration Module wires
	exiting from connector, then coil as shown in figure 2-1.6 below. Install item 1.9 (Cable
	Clamp) as shown. Do not tighten screws yet.

FIGURE 2-1.6 MK XXII EGPWS CONFIGURATION MODULE

CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225

REV: C SHEET 42

Image 42

Honeywell MKXXII installation manual MK Xxii Egpws Configuration Module

Contents

Release Date 12/14/00 REV C Sheet ALL Revisions REV Description Honeywell MK Xxii Egpws Installation Manual Table of Contents Honeywell MK VI MK Viii Egpws Installation Design Guide Honeywell MK VI MK Viii Egpws Installation Design Guide 104 Section V Certification 158 143149 160Aircraft Application Data Section General Information Honeywell MK Xxii Egpws Installation Manual Section I General Information License Requirements How To Use This Docu ment IntroductionApplicability Reference Documents Description of Equipm ent GPS Antenna MK Xxii Egpws Comp uterMK Xxii Egpws Conf iguration Module OAT SensorSmart Cable Pcmcia Interface MK Xxii Egpws Smart Cable Technical Characteris ticsConfiguration Module Units SuppliedMK Xxii Egpws Honeywell MK Xxii Egpws Installation Manual 2 RS-232 Cable Installation and Acces sories KitsNew Egpws installation with Internal GPS Smart CableTerrain Database Card s Flight History CardGPS Antenna & cable Circuit BreakerAnnunciators & Switc h/Annunciators Cockpit Speaker Opti onal Insertion/Removal Too l P1, P2, P3 Tools Required Crimping Tool P1, P 2, P3Contact Positioner P 1, P2, P3 Spare Contacts P1, P 2, P3Honeywell MK Xxii Egpws Installation Manual Section Installation Honeywell MK Xxii Egpws Installation Manual Section II Installation Equipment Installation 2.3.1 General Unpacking and Inspec ting the EquipmentMK Xxii Computer Loc ation MK Xxii Computer Ins tallationConfiguration Module Location Configuration Module InstallationConfiguration Module Assembly RequiredInstallation Assembly Sequence 1 MK Xxii Egpws Configuration Module2 MK Xxii Egpws Configuration Module 3 MK Xxii Egpws Configuration Module 4 MK Xxii Egpws Configuration Module 5 MK Xxii Egpws Configuration Module 6 MK Xxii Egpws Configuration Module 7 MK Xxii Egpws Configuration Module Cockpit Annunciators / Switches GPS Antenna Installat ionOAT Sensor Installatio n GPS Antenna locationDescription Egpws cautionGPWS G/S CancldLocation Gpws warning red & Gpws alert amber8 MK Xxii Egpws Annunciators/Switches Location Terrain Inhibit Inhibit Switch Functio ns and SelectionLow Altitude Mode Audio Inhibit TimedMK Xxii Egpws Outline MK Xxii Egpws Mounting Tray Honeywell P/N 405-0383-001Honeywell MK Xxii Egpws Installation Manual Section System Planning Honeywell MK Xxii Egpws Installation Manual Section III System Planning Category 8 Radio Altitude Input Select Category 14 Audio Output Level System Wiring/ Electr ical Interfaces Primary Power InputChassis Ground Analog and Digital Inp uts Discrete InputsSerial Outputs Audio Output Discrete OutputsAircraft / Mode Type Configurable Interface sCategory 1 Aircraft / Mode Type Select InstructionsCategory 2 Air Data Input Select Examples Analog altitude and 500 ohm OAT Egpws MKDigital Arinc 429 Cat ID 5, 1 Digital -ARINC 575 Cat ID ArincShadin 2000 Cat ID Digital Arinc 429 Dual IOC Buses Cat . ID Category 3 Position Input Select Arinc 743 FormatExamples Arinc 429 BUS Cat ID 0,1,4,5 3.2 RS-232 Transmit-Receive, 9600 baud Cat IDDual Arinc 429 BUS Cat ID Category 4 Altitude Callouts Category 5 Audio Menu Select Category 6 Terrain Display Select TAD SelectionTerrain Display Configuration Group Type of sweep used for terrain data fan, standard, etc6-1 Single Tube Wx/Terrain Display Display Input Control Group Output 429 Bus GroupExample Egpws TRA-45AJ101 Egpws Avidyne FSD Honeywell Radar Indicator Honeywell WRX R/TAvtech DSU Arinc 429 Range #1 Arinc 429 Range #2 Kcpb Video #1 OutCategory 7 Options Select Group #1 Steep Approach Not Available in the Mk7.3 TA&D Alternate Pop-up Peaks Mode Obstacle AwarenessBank Angle Callout Enabling WOW Reversal GPS Altitude ReferenceCategory 8 Radio Altitude Input Select Example Digital Radio Altitude InterfaceDH Discrete Gnd Valid Radio Altimeter Indicator Analog Radio Altitude InterfaceCategory 9 Navigation Inputs Select Example Analog Glideslope Interface cat ID 0,1,5 RNA-34ADigital Glideslope/Localizer Interface Dual Glideslope ReceiverAttitude Signals Category 10 Attitude Input SelectExample Analog Roll Angle Synchro Vertical GyroDigital Arinc 429 High Speed AhrsCategory 11 Heading Input Select Magnetic HeadingExample Analog Heading Synchro CAT ID Directional GyroHeading High Speed Category 12 Windshear Input Select InstructionCategory 13 Input / Output Discrete Type Select Input/Output DiscretesWeight on Wheels WOW Discrete Audio Inhibit DiscreteLanding Gear Discrete Glideslope Cancel Discrete Mode 6 Low Volume DiscreteAutopilot Engaged Discrete Terrain Awareness Inhibit Self Test DiscreteGlideslope Inhibit Discrete Output Discretes Low Altitude Mode Select DiscreteTimed Audio Inhibit Discrete Lamp FormatGpws Warning Discrete Gpws Inop DiscreteTAD Inop Discrete Gpws Alert DiscreteLow Altitude Mode Discrete Terrain Display Select #1 & #2 DiscreteREV C Sheet Category 14 Audio Output Level OhmCategory 15, Autorotation Threshold Autorotation Threshold 107 108 Egpwc Initialization a nd Configuration Harness Checkout and Power CheckUnit Installation 1 RS-232 Communicatio n with the MK Xxii EgpwsEgpwc Front Panel T est Connector WinVIEWSConfiguration Module Programming WinVIEWS Operation112 CUW and CMR Comm ands CFG CUW 0/15 128 3 2 134 128 3 29 1 0 2 0 0 129 0Configuration Module Reprogramming CATspacecategory #spaceID#spaceT or FEnterRegional Terrain Data base Loading 4.6.1 Effectivity ApprovalMaterial Cost and Av ailability Accomplishment Instr uctions Verification of the Ter rain Database Version END of Test 120 Section Certification Honeywell MK Xxii Egpws Installation Manual Section V Certification FAA Requirements Certification Procedur e Equipment Compatibi lityEquipment Location Ground TestPilots Guide Failure Modes, Effects , and Safety AnalysisFlight Test Existing STC’sHoneywell MK Xxii Egpws Installation Manual Appendix a Customer Worksheet Honeywell MK Xxii Egpws Installation Manual MK Xxii Egpws Cockpit DisplaysGPS Discrete Inputs ParameterGeneric Model Information System REV C Sheet REV C Sheet REV C Sheet REV C Sheet REV C Sheet Appendix B Sample Wiring Diagrams DWG no 060-4314-225 Revc Sheet Honeywell MK Xxii Egpws Installation Manual Honeywell MK Xxii Egpws Installation Manual Appendix C Honeywell MK Xxii Egpws Installation Manual RS-232 Communication with the Egpws Baud, No Parity, 8 bits, and 1 stop bitREV C Sheet REV C Sheet Honeywell MK Xxii Installation Manual Appendix D Vendor Drawings Honeywell MK Xxii Egpws Installation Manual Vendor Contact Information AMPFor orders and AOG requirements, contact D1-1 Edmo GPS RF Cable Sets D1-2 EmteqPer 100 ft Inches Bend Radius Minimum1 Connectors for Tflx cable series GPS 1 Connectors for Pflx cable series GPS Tool Frame and Die Part Numbers Installation Considerations Aerospace Optics Inc D1-3 Aerospace OpticsMail switches@vivisun.com StacoSwitch Honeywell MK Xxii Egpws Installation Manual Appendix E Interface Description DocumentHoneywell MK Xxii Egpws Installation Manual Connector Interface Introduction Part Number PurposeSystem Overview Electrical Interface Introduction Signal InterfacesPrimary Power Input Chassis GroundLOW Level Glideslope DC Analog InputsRadio Altitude Localizer Deviation or LOW Level Glideslope Validity2.4 Outside AIR TemperatureConfiguration Defined DC Inputs Barometric AltitudeSynchro Roll Attitude AC Analog Inputs2.7.1 2.7.2Configuration Defined Synchro Inputs Signal Timing Reference Inputs2.9 Arinc 429/575 Digital Serial BUS Inputs2.9.1 RS-232 / RS-422 Digital Serial BUS Inputs GPS RS-232 Digital Serial BUS Serial PortGPS RS-422 Digital Serial BUS Serial Port AIR Data RS-422 Digital Serial BUS Serial Port +28 VDC Discrete CharacteristicsAIR Data RS-232 Digital Serial BUS Serial Port SCI Range RS-422 Digital Serial BUS Serial PortConfiguration Module Interface Ground Discrete CharacteristicsGPS Antenna Input OAT Voltage Reference Output Monitor Output CharacteristicsDiscrete Output Characteristics Lamp Driver OutputsArinc Digital Serial Output Busses High Level Speaker Audio OutputLOW Level Interphone Audio Output Arinc 429 Output BUS2.18.1 RS-232 Maintenance Port Serial Port Arinc 453 Output BUSFront Panel Test Interface Front Panel Status Indicators Pcmcia / Smartcable PortGSE Present Discrete Input Configuration Types Configuration SelectionAircraft Application Data Signal Selection Table E 3 Category ID Selection ProcedureInstruction Configuration Selection Tables Category 1, Aircraft / Mode Type Select Torque Type Table E Effectivity App CfgFault Designation Engine 1 BUS Bus Type Basic Fault Designation Engine 2 BUS Bus Type BasicEngine Torque Data Selection Fault Designation Engine 1 BUS Bus Type RS-422 9600 baud Fault Designation Engine 2 BUS Bus Type RS-422 9600 baudTorque Data Select 10 Bell Summary Data Torque Data Select 8 AS365 Dauphin N3Torque Data Select 9 Bell Torque Data Select 11 Bell 212/412 Summary DataTorque Data Select 16 Common DC Torque Fault Designation Engine 1 BUSTorque Data Select 14 Coast Guard HH-65 Summary Data Connection Summary DataCategory 2, AIR Data Input Select Table E DescriptionTable E 3.1.2 AIR Data Input Select for Egpws Mkxxii Configuration Data Fault Designation AIR Data BUS Bus Type BasicType Summary Data Table E 3.1.2-3 AIR Data Input Select #3 Summary Data Table E 3.1.2-4 AIR Data Input Select #4 Summary Data Table E 3.1.2-5 AIR Data Input Select #5Connect to Channel Channel Connect to Channel 429RX2Table E 3.1.2-6 AIR Data Input Select #6 Table E 3.1.2-10 AIR Data Input Select #10Table E 3.1.2-11 AIR Data Input Select #11 Summary Data 3.3 Category 3, Position Input SelectPosition Input Type TableE Description Fault Designation GPS BUS Bus Type Basic UTCFault Designation Internal GPS Bus Type Basic InternalFault Designation GPS BUS Bus Type BasicCategory 4, Altitude Callouts App CfgTable E 3.1.4 Altitude Callouts for Egpws Mkxxii Honeywell MK Xxii Egpws Installation Manual Table E 3.1.5 Audio Menu Type Category 5, Audio Menu SelectEffectivity App Cfg 006 Table E 3.1.5-128 Audio Menu Type 128 Basic HelicopterSection Overview IDand TCF Disable Application NotesCategory 6, Terrain Display Select Defined ByHoneywell MK Xxii Egpws Installation Manual Table E KC Picture Bus Table Table E 3.1.6-1 No Display TAD and TCF Enabled Table Table E 3.1.6-2 TA&D / TCF DisabledChannel Table Table E 3.1.6-3 Collins ProLine II Fault Designation Display BUS Bus Type BasicDisplay Configuration Group 6 Collins PRO-LINE II Integration noteDisplay Configuration Group 1 Bendix RDR 4A/B PPI with MOD Table Table E 3.1.6-4 Bendix PPI-4A/4BDisplay Configuration Group 2 Collins Proline II Table E Collins ProLine IIDisplay Configuration Group 3 Collins Proline II, 5X4 Table E Collins ProLine II 5x4,5x5Display Configuration Group 7 NON-INTEGRATED Efis 40/50 Table E Non-Integrated Efis 40/50 Honeywell/BendixPeaks Always Enabled Display Configuration Group 8 Integrated Efis 40/50Table E 3.1.6-10 Integrated Efis 40/50 Honeywell/Bendix Honeywell MK Xxii Egpws Installation Manual Table E 3.1.6-12 Collins WXI-701/711, without Auto Range Terrain Display BUS #2 Integration note PinsTerrain Display BUS #1 453TX1 Reference NameTable E 3.1.6-14 Bendix PPI-4A/4B without Auto Range Terrain Display BUS #2 453TX26.2-3 Display Input Control Group Reference Name PIN Function6.3-0OUTPUT 429 BUS Group Traceability Table E 3.1.6-16 Bendix IN182A/IN812A Radar display RDR Reference sectionPins Comments Output 429 Bus GroupCategory 7, Options Select Group #1 Table E Bendix IN842A/IN862A Radar display RDRFunction Value TA&D Alternate Pop Up False TA&D Alternate Pop Up TrueDisplay Input Control Group Display Input Control Group Honeywell Fault Designation IOC BUS Table E3.1.6-236 Display Configuration Collins ProLine IV Honeywell Channel 429RX8 Table E 3.1.6-246 Non-Integrated Efis 10 Bendix/Honeywell Connect to DC811 #1 Display Input Control Group Channel 422RX2Connect to DC811 #2 Honeywell MK Xxii Egpws Installation Manual SCI Bus RS-422 12K baud Category 7, Options 1 Select Altitude Reference6 Effectivity App CfgTable E 317 Options Select Group #1 True False WGS-84 Category 8, Radio Altitude Input Select Radio Altitude Type Table E DescriptionDescription Value PIN Function Connection PIN Type Channel Designation ReferenceTable E 3.1.8-5 Radio Altitude Input Select Type 5 ALT Reference Summary DataTable E 3.1.9-0 Navigation Inputs Select Summary Data Category 9, Navigation Input SelectTable E 3.1.9 Navigation Input Select for Egpws Mkxxii Connection PIN TypeFault Designation ILS BUS Bus T ype Basic Fault Designation ILS BUSTable E 3.1.10 Attitude Input Select for Egpws MK Category 10, Attitude Input SelectAttitude Input Select Table E 3.1.10-0 Attitude Input Select TypeFault Designation Ahrs BUS Table E 3.1.10-4 Attitude Input Select TypeTable E 3.1.10-128 Attitude Input Select Type Connect to Heading Input Select Table E Description Fault Designation Ahrs BUS Bus Type BasicCategory 11, Heading Input Select Table E 3.1.11 Heading Input Select for Egpws MKEffectivity App Cfg 003 Category 12, Windshear Input SelectNo Windshear Table E 3.1.12 Windshear Input SelectCategory 13, Input / Output Discrete Type Select Input/Output Discrete Type Table EConfiguration Data Possible States StateTable E 3.1.13-128 INPUT/OUTPUT Discrete Type Table E 3.1.13-129 INPUT/OUTPUT Discrete Type Volume Select Category 14, Audio Output LevelTable E 3.1.14 Audio Output Level Category 15, Autorotation Threshold Autorotation Threshold TorqueTable E 3.1.15 Autorotation Threshold for Egpws MK SYN1X SYN1Z SYN2Z Connector Pin Refer to Category 13 where multiple uses are possible Honeywell MK Xxii Egpws Installation Manual Figure E 4.1, Connector Pin References J1, J2, J3 AcronymInterpretation DefinitionsAcronym Interpretation Pcmcia