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Honeywell MKXXII installation manual MK Xxii Egpws Smart Cable, Technical Characteris tics

Models: MKXXII

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Honeywell

MK XXII EGPWS Installation Manual

FIGURE 1-1 MK XXII EGPWS SMART CABLE

1.6 Technical Characteris tics

MK XXII EGPWS

TSO Compliance:

TSO-C92c, TSO-C151a, class A

Physical size (HxWxD):

6.20” x 3.04” x 10.30”

Weight:

3.9 pounds maximum

Mounting:

Standard 3 inch King Radio rack

Temperature (operational):

-55°C to +70°C (F2)

Altitude range:

55,000 feet (F2)

Cooling:

No cooling necessary

Shock:

No shock mounting required

Power Consumption (28 VDC):

3 Amps

9 watts – no warning

+7 watts – with warning over 8 ohm speaker

+3 watts – with GPS card

+49 watts – with heater blanket on

Configuration Module

TSO Compliance:

same as MK XXII EGPWS

CAGE CODE: 97896 SCALE: NONE

SIZE: A DWG NO: 060-4314-225

REV: C SHEET 21

Image 21

Honeywell MKXXII installation manual MK Xxii Egpws Smart Cable, Technical Characteris tics

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 149 143158 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 Conf iguration Module MK Xxii Egpws Comp uterGPS Antenna OAT SensorSmart Cable Pcmcia Interface Technical Characteris tics MK Xxii Egpws Smart CableConfiguration Module Units SuppliedMK Xxii Egpws Honeywell MK Xxii Egpws Installation Manual New Egpws installation with Internal GPS Installation and Acces sories Kits2 RS-232 Cable Smart CableFlight History Card Terrain Database Card sGPS Antenna & cable Circuit BreakerAnnunciators & Switc h/Annunciators Cockpit Speaker Opti onal Contact Positioner P 1, P2, P3 Tools Required Crimping Tool P1, P 2, 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 Unpacking and Inspec ting the Equipment Equipment Installation 2.3.1 GeneralMK Xxii Computer Ins tallation MK Xxii Computer Loc ationConfiguration Module Installation Configuration Module LocationRequired Configuration Module Assembly1 MK Xxii Egpws Configuration Module Installation Assembly Sequence2 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 OAT Sensor Installatio n GPS Antenna Installat ionCockpit Annunciators / Switches GPS Antenna locationEgpws cautionGPWS G/S Cancld DescriptionGpws warning red & Gpws alert amber Location8 MK Xxii Egpws Annunciators/Switches Location Low Altitude Mode Inhibit Switch Functio ns and SelectionTerrain Inhibit Audio Inhibit TimedMK Xxii Egpws Outline Honeywell P/N 405-0383-001 MK Xxii Egpws Mounting TrayHoneywell 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 Discrete Outputs Audio OutputCategory 1 Aircraft / Mode Type Select Configurable Interface sAircraft / Mode Type InstructionsCategory 2 Air Data Input Select Egpws MK Examples Analog altitude and 500 ohm OATDigital Arinc 429 Cat ID 5, 1 Arinc Digital -ARINC 575 Cat IDShadin 2000 Cat ID Digital Arinc 429 Dual IOC Buses Cat . ID Arinc 743 Format Category 3 Position Input Select3.2 RS-232 Transmit-Receive, 9600 baud Cat ID Examples Arinc 429 BUS Cat ID 0,1,4,5Dual Arinc 429 BUS Cat ID Category 4 Altitude Callouts Category 5 Audio Menu Select TAD Selection Category 6 Terrain Display SelectType of sweep used for terrain data fan, standard, etc Terrain Display Configuration Group6-1 Single Tube Wx/Terrain Display Display Input Control Group Output 429 Bus GroupExample TRA-45A EgpwsJ101 Egpws Avidyne FSD Honeywell WRX R/T Honeywell Radar IndicatorArinc 429 Range #1 Arinc 429 Range #2 Kcpb Video #1 Out Avtech DSUCategory 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 GPS Altitude Reference WOW ReversalExample Digital Radio Altitude Interface Category 8 Radio Altitude Input SelectAnalog Radio Altitude Interface DH Discrete Gnd Valid Radio Altimeter IndicatorCategory 9 Navigation Inputs Select RNA-34A Example Analog Glideslope Interface cat ID 0,1,5Dual Glideslope Receiver Digital Glideslope/Localizer InterfaceCategory 10 Attitude Input Select Attitude SignalsVertical Gyro Example Analog Roll Angle SynchroAhrs Digital Arinc 429 High SpeedMagnetic Heading Category 11 Heading Input SelectDirectional Gyro Example Analog Heading Synchro CAT IDHeading High Speed Instruction Category 12 Windshear Input SelectInput/Output Discretes Category 13 Input / Output Discrete Type SelectWeight 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 Timed Audio Inhibit Discrete Low Altitude Mode Select DiscreteOutput Discretes Lamp FormatTAD Inop Discrete Gpws Inop DiscreteGpws Warning Discrete Gpws Alert DiscreteTerrain Display Select #1 & #2 Discrete Low Altitude Mode DiscreteREV C Sheet Ohm Category 14 Audio Output LevelCategory 15, Autorotation Threshold Autorotation Threshold 107 108 Unit Installation Harness Checkout and Power CheckEgpwc Initialization a nd Configuration 1 RS-232 Communicatio n with the MK Xxii EgpwsWinVIEWS Egpwc Front Panel T est ConnectorWinVIEWS Operation Configuration Module Programming112 CFG CUW 0/15 128 3 2 134 128 3 29 1 0 2 0 0 129 0 CUW and CMR Comm andsCATspacecategory #spaceID#spaceT or FEnter Configuration Module ReprogrammingApproval Regional Terrain Data base Loading 4.6.1 EffectivityMaterial 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 Equipment Location Certification Procedur e Equipment Compatibi lityFAA Requirements Ground TestFlight Test Failure Modes, Effects , and Safety AnalysisPilots Guide Existing STC’sHoneywell MK Xxii Egpws Installation Manual Appendix a Customer Worksheet Honeywell MK Xxii Egpws Installation Manual Cockpit Displays MK Xxii EgpwsGPS Parameter Discrete InputsGeneric 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 Baud, No Parity, 8 bits, and 1 stop bit RS-232 Communication with the EgpwsREV C Sheet REV C Sheet Honeywell MK Xxii Installation Manual Appendix D Vendor Drawings Honeywell MK Xxii Egpws Installation Manual AMP Vendor Contact InformationFor orders and AOG requirements, contact D1-1 Edmo D1-2 Emteq GPS RF Cable SetsInches Bend Radius Minimum Per 100 ft1 Connectors for Tflx cable series GPS 1 Connectors for Pflx cable series GPS Tool Frame and Die Part Numbers Installation Considerations D1-3 Aerospace Optics Aerospace Optics IncMail switches@vivisun.com StacoSwitch Appendix E Interface Description Document Honeywell MK Xxii Egpws Installation ManualHoneywell MK Xxii Egpws Installation Manual Connector Interface Introduction Part Number PurposeSystem Overview Primary Power Input Signal InterfacesElectrical Interface Introduction Chassis GroundRadio Altitude DC Analog InputsLOW Level Glideslope Localizer Deviation or LOW Level Glideslope ValidityConfiguration Defined DC Inputs Outside AIR Temperature2.4 Barometric Altitude2.7.1 AC Analog InputsSynchro Roll Attitude 2.7.2Signal Timing Reference Inputs Configuration Defined Synchro InputsArinc 429/575 Digital Serial BUS Inputs 2.92.9.1 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-232 Digital Serial BUS Serial Port +28 VDC Discrete CharacteristicsAIR Data RS-422 Digital Serial BUS Serial Port SCI Range RS-422 Digital Serial BUS Serial PortConfiguration Module Interface Ground Discrete CharacteristicsGPS Antenna Input Discrete Output Characteristics Monitor Output CharacteristicsOAT Voltage Reference Output Lamp Driver OutputsLOW Level Interphone Audio Output High Level Speaker 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 Effectivity App Cfg Torque Type Table EFault Designation Engine 1 BUS Bus Type Basic Fault Designation Engine 2 BUS Bus Type BasicEngine Torque Data Selection Fault Designation Engine 2 BUS Bus Type RS-422 9600 baud Fault Designation Engine 1 BUS Bus Type RS-422 9600 baudTorque Data Select 9 Bell Torque Data Select 8 AS365 Dauphin N3Torque Data Select 10 Bell Summary Data Torque Data Select 11 Bell 212/412 Summary DataTorque Data Select 14 Coast Guard HH-65 Summary Data Fault Designation Engine 1 BUSTorque 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 Table E 3.1.2-6 AIR Data Input Select #6 Channel 429RX2Channel 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 UTC Fault Designation GPS BUS Bus Type BasicInternal Fault Designation Internal GPS Bus Type BasicBus Type Basic Fault Designation GPS BUSCategory 4, Altitude Callouts App CfgTable E 3.1.4 Altitude Callouts for Egpws Mkxxii Honeywell MK Xxii Egpws Installation Manual Effectivity App Cfg 006 Category 5, Audio Menu SelectTable E 3.1.5 Audio Menu Type Table E 3.1.5-128 Audio Menu Type 128 Basic HelicopterCategory 6, Terrain Display Select IDand TCF Disable Application NotesSection 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 Display Configuration Group 6 Collins PRO-LINE II Fault Designation Display BUS Bus Type BasicTable Table E 3.1.6-3 Collins ProLine II Integration noteTable Table E 3.1.6-4 Bendix PPI-4A/4B Display Configuration Group 1 Bendix RDR 4A/B PPI with MODTable E Collins ProLine II Display Configuration Group 2 Collins Proline IITable E Collins ProLine II 5x4,5x5 Display Configuration Group 3 Collins Proline II, 5X4Table E Non-Integrated Efis 40/50 Honeywell/Bendix Display Configuration Group 7 NON-INTEGRATED Efis 40/50Peaks 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 #1 453TX1 Integration note PinsTerrain Display BUS #2 Reference NameTerrain Display BUS #2 453TX2 Table E 3.1.6-14 Bendix PPI-4A/4B without Auto Range6.2-3 Display Input Control Group Reference Name PIN Function6.3-0OUTPUT 429 BUS Group Traceability Reference section Table E 3.1.6-16 Bendix IN182A/IN812A Radar display RDROutput 429 Bus Group Pins CommentsFunction Value Table E Bendix IN842A/IN862A Radar display RDRCategory 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 Type Channel Designation Reference PIN Function ConnectionReference Summary Data Table E 3.1.8-5 Radio Altitude Input Select Type 5 ALTTable E 3.1.9 Navigation Input Select for Egpws Mkxxii Category 9, Navigation Input SelectTable E 3.1.9-0 Navigation Inputs Select Summary Data Connection PIN TypeFault Designation ILS BUS Fault Designation ILS BUS Bus T ype BasicAttitude Input Select Category 10, 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 Category 11, Heading Input Select Fault Designation Ahrs BUS Bus Type BasicHeading Input Select Table E Description Table E 3.1.11 Heading Input Select for Egpws MKNo Windshear Category 12, Windshear Input SelectEffectivity App Cfg 003 Table E 3.1.12 Windshear Input SelectInput/Output Discrete Type Table E Category 13, Input / Output Discrete Type SelectConfiguration 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 Definitions AcronymInterpretationAcronym Interpretation Pcmcia