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Honeywell MKXXII installation manual Category 6 Terrain Display Select, TAD Selection

Models: MKXXII

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Honeywell

MK XXII EGPWS Installation Manual

3.3.6 Category 6 – Terrain Display Select

Category 6 defines the Terrain Display options available.

Appendix E Table E 3.1.6 defines the Terrain Display Select options (Display Configuration Group Tables, Display Input Control Group Tables and Output 429 Bus Group Tables) and identifies the first MK XXII EGPWS version in which the option was available (see the Effectivity entry).

Note: TA&D mode enabling/disabling is controlled by Category 6. Chose ID 2 for aircraft without

TA&D.

3.3.6.1 Instructions

1.Using Appendix E Tables E3.1.6 and E 3.1.6-xselect the Terrain Display Select Type (ID) that matches the aircraft configuration, feature preferences and version (part number) being installed. Record the ID number for the Terrain Display Select Type from Appendix E Table E 3 under the Ident No. heading for Step (Category) 6 .

2.Using the I D number Table E 3.1.6 as “x”, go to the Table E 3.1.6-x.The electrical interfaces (pin-outs) for the Display are shown in the Display Configuration Group, Display Input Control Group, and Output 429 Bus Group, Table E 3.1.6-x are used to generate the installation wiring diagrams. Determine the wiring interconnects and record it on Appendix A Fig A1-1.

Figure 3.8-1 is an example of single tube Wx/Terrain display wiring connections.

3.3.6.2 TAD Selection

The Terrain Awareness & Display feature consists of a Terrain Awareness Alerting feature and a Terrain Awareness Display feature. The Terrain Awareness Alerting feature continuously computes terrain clearance envelopes ahead of the aircraft and issues alerts if the boundaries of these envelopes conflict with terrain elevation data in the terrain database. The Terrain Awareness Display feature displays the terrain data relative to aircraft altitude.

A “False” entry in Appendix ETable E 3.1.6 for “TAD Disable” indicates that TA&D is ENABLED (the “Disable” is disabled).

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

REV: C SHEET 72

Image 72

Honeywell MKXXII installation manual Category 6 Terrain Display Select, TAD Selection

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 143 149158 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 MK Xxii Egpws Comp uter MK Xxii Egpws Conf iguration ModuleGPS Antenna OAT SensorSmart Cable Pcmcia Interface MK Xxii Egpws Smart Cable Technical Characteris ticsConfiguration Module Units SuppliedMK Xxii Egpws Honeywell MK Xxii Egpws Installation Manual Installation and Acces sories Kits New Egpws installation with Internal GPS2 RS-232 Cable Smart CableTerrain Database Card s Flight History CardGPS Antenna & cable Circuit BreakerAnnunciators & Switc h/Annunciators Cockpit Speaker Opti onal Tools Required Crimping Tool P1, P 2, P3 Contact Positioner P 1, P2, P3Insertion/Removal Too l P1, 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 GPS Antenna Installat ion OAT Sensor Installatio nCockpit Annunciators / Switches GPS Antenna locationDescription Egpws cautionGPWS G/S CancldLocation Gpws warning red & Gpws alert amber8 MK Xxii Egpws Annunciators/Switches Location Inhibit Switch Functio ns and Selection Low Altitude ModeTerrain Inhibit 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 OutputsConfigurable Interface s Category 1 Aircraft / Mode Type SelectAircraft / Mode Type 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 Low Altitude Mode Select Discrete Timed Audio Inhibit DiscreteOutput Discretes Lamp FormatGpws Inop Discrete TAD Inop DiscreteGpws Warning 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 Harness Checkout and Power Check Unit InstallationEgpwc Initialization a nd Configuration 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 Certification Procedur e Equipment Compatibi lity Equipment LocationFAA Requirements Ground TestFailure Modes, Effects , and Safety Analysis Flight TestPilots Guide 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 Signal Interfaces Primary Power InputElectrical Interface Introduction Chassis GroundDC Analog Inputs Radio AltitudeLOW Level Glideslope Localizer Deviation or LOW Level Glideslope ValidityOutside AIR Temperature Configuration Defined DC Inputs2.4 Barometric AltitudeAC Analog Inputs 2.7.1Synchro Roll Attitude 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 +28 VDC Discrete Characteristics AIR Data RS-232 Digital Serial BUS Serial PortAIR Data RS-422 Digital Serial BUS Serial Port SCI Range RS-422 Digital Serial BUS Serial PortConfiguration Module Interface Ground Discrete CharacteristicsGPS Antenna Input Monitor Output Characteristics Discrete Output CharacteristicsOAT Voltage Reference Output Lamp Driver OutputsHigh Level Speaker Audio Output LOW Level Interphone Audio OutputArinc Digital Serial Output Busses 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 8 AS365 Dauphin N3 Torque Data Select 9 BellTorque Data Select 10 Bell Summary Data Torque Data Select 11 Bell 212/412 Summary DataFault Designation Engine 1 BUS Torque Data Select 14 Coast Guard HH-65 Summary DataTorque Data Select 16 Common DC Torque 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 429RX2 Table E 3.1.2-6 AIR Data Input Select #6Channel Connect to 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 Category 5, Audio Menu Select Effectivity App Cfg 006Table E 3.1.5 Audio Menu Type Table E 3.1.5-128 Audio Menu Type 128 Basic HelicopterIDand TCF Disable Application Notes Category 6, Terrain Display SelectSection Overview 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 Fault Designation Display BUS Bus Type Basic Display Configuration Group 6 Collins PRO-LINE IITable Table E 3.1.6-3 Collins ProLine 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 Integration note Pins Terrain Display BUS #1 453TX1Terrain Display BUS #2 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 GroupTable E Bendix IN842A/IN862A Radar display RDR Function ValueCategory 7, Options Select Group #1 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 DataCategory 9, Navigation Input Select Table E 3.1.9 Navigation Input Select for Egpws MkxxiiTable E 3.1.9-0 Navigation Inputs Select Summary Data Connection PIN TypeFault Designation ILS BUS Bus T ype Basic Fault Designation ILS BUSCategory 10, Attitude Input Select Attitude Input SelectTable E 3.1.10 Attitude Input Select for Egpws MK 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 Fault Designation Ahrs BUS Bus Type Basic Category 11, Heading Input SelectHeading Input Select Table E Description Table E 3.1.11 Heading Input Select for Egpws MKCategory 12, Windshear Input Select No WindshearEffectivity App Cfg 003 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