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Honeywell MKXXII installation manual Honeywell WRX R/T, Honeywell Radar Indicator

Models: MKXXII

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CAGE CODE:

Honeywell WRX R/T

97896 SCALE: NONE SIZE:

		WU-440, 660, 880
	J2	71	72	3	4
EGPWS		71	72	3	4
EGPWS
RS-422 Serial Range #1 In	A 36
RS-422 Serial Range #1 In	B 37
	B 37
Range #2 In	A 41
Range #2 In	NC
	B 40

Honeywell

Radar Indicator

F P

SCI Bus

GN

M P

WXPD Bus

L N

MK XXII

A

J1

X EGPWS Selected

DWG NO: 060-4314-225

ARINC 453 Video #1 Out

ARINC 453 Video #2 Out

A58

B59

	A	56	TERR
			NC
	B	57
			ON

momentary

WI-440, 660, 880 7007700-X1X

28V EGPWS PWR Bus

EGPWS Installation	Honeywell
Manual

REV:

Terrain Display Select (in) 32

Terrain Display Select (out) 54

Lamp Test

28V Lamp Dimming Bus

C SHEET 79

Terrain Inhibit (in) 12

Terrain INOP (out) 55

MK XXII 965-1590-006 or later.

TERR

INHIB

TERR

INOP

Alternate Action

Note:

For interface and operation of the Honeywell Weather Radar Indicator WI-440, 660, 880 see Honeywell Service Bulletin 7007700-34-15

IntP880.vsd

Integrated

Primus 440/660/880

Image 79

Honeywell MKXXII installation manual Honeywell WRX R/T, Honeywell Radar Indicator

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 160 143149 158Aircraft Application Data Section General Information Honeywell MK Xxii Egpws Installation Manual Section I General Information License Requirements Introduction How To Use This Docu mentApplicability Reference Documents Description of Equipm ent OAT Sensor MK Xxii Egpws Comp uterMK Xxii Egpws Conf iguration Module GPS AntennaSmart Cable Pcmcia Interface Technical Characteris tics MK Xxii Egpws Smart CableUnits Supplied Configuration ModuleMK Xxii Egpws Honeywell MK Xxii Egpws Installation Manual Smart Cable Installation and Acces sories KitsNew Egpws installation with Internal GPS 2 RS-232 CableFlight History Card Terrain Database Card sCircuit Breaker GPS Antenna & cableAnnunciators & Switc h/Annunciators Cockpit Speaker Opti onal Spare Contacts P1, P 2, P3 Tools Required Crimping Tool P1, P 2, P3Contact Positioner P 1, P2, P3 Insertion/Removal Too l P1, P2, 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 GPS Antenna location GPS Antenna Installat ionOAT Sensor Installatio n Cockpit Annunciators / SwitchesEgpws cautionGPWS G/S Cancld DescriptionGpws warning red & Gpws alert amber Location8 MK Xxii Egpws Annunciators/Switches Location Audio Inhibit Timed Inhibit Switch Functio ns and SelectionLow Altitude Mode Terrain InhibitMK 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 Primary Power Input System Wiring/ Electr ical InterfacesChassis Ground Discrete Inputs Analog and Digital Inp utsSerial Outputs Discrete Outputs Audio OutputInstructions Configurable Interface sCategory 1 Aircraft / Mode Type Select Aircraft / Mode TypeCategory 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 Output 429 Bus Group Display Input Control 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 DSUSteep Approach Not Available in the Mk Category 7 Options Select Group #17.3 TA&D Alternate Pop-up Obstacle Awareness Peaks ModeBank 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 SelectAudio Inhibit Discrete Weight on Wheels WOW DiscreteLanding Gear Discrete Mode 6 Low Volume Discrete Glideslope Cancel DiscreteAutopilot Engaged Discrete Self Test Discrete Terrain Awareness InhibitGlideslope Inhibit Discrete Lamp Format Low Altitude Mode Select DiscreteTimed Audio Inhibit Discrete Output DiscretesGpws Alert Discrete Gpws Inop DiscreteTAD Inop Discrete Gpws Warning 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 1 RS-232 Communicatio n with the MK Xxii Egpws Harness Checkout and Power CheckUnit Installation Egpwc Initialization a nd ConfigurationWinVIEWS 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 Ground Test Certification Procedur e Equipment Compatibi lityEquipment Location FAA RequirementsExisting STC’s Failure Modes, Effects , and Safety AnalysisFlight Test Pilots GuideHoneywell 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 Purpose Introduction Part NumberSystem Overview Chassis Ground Signal InterfacesPrimary Power Input Electrical Interface IntroductionLocalizer Deviation or LOW Level Glideslope Validity DC Analog InputsRadio Altitude LOW Level GlideslopeBarometric Altitude Outside AIR TemperatureConfiguration Defined DC Inputs 2.42.7.2 AC Analog Inputs2.7.1 Synchro Roll AttitudeSignal Timing Reference Inputs Configuration Defined Synchro InputsArinc 429/575 Digital Serial BUS Inputs 2.9GPS RS-232 Digital Serial BUS Serial Port 2.9.1 RS-232 / RS-422 Digital Serial BUS InputsGPS RS-422 Digital Serial BUS Serial Port SCI Range RS-422 Digital Serial BUS Serial Port +28 VDC Discrete CharacteristicsAIR Data RS-232 Digital Serial BUS Serial Port AIR Data RS-422 Digital Serial BUS Serial PortGround Discrete Characteristics Configuration Module InterfaceGPS Antenna Input Lamp Driver Outputs Monitor Output CharacteristicsDiscrete Output Characteristics OAT Voltage Reference OutputArinc 429 Output BUS High Level Speaker Audio OutputLOW Level Interphone Audio Output Arinc Digital Serial Output BussesArinc 453 Output BUS 2.18.1 RS-232 Maintenance Port Serial PortFront Panel Test Interface Pcmcia / Smartcable Port Front Panel Status IndicatorsGSE Present Discrete Input Configuration Selection Configuration TypesAircraft Application Data Table E 3 Category ID Selection Procedure Signal SelectionInstruction Configuration Selection Tables Category 1, Aircraft / Mode Type Select Effectivity App Cfg Torque Type Table EFault Designation Engine 2 BUS Bus Type Basic Fault Designation Engine 1 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 11 Bell 212/412 Summary Data Torque Data Select 8 AS365 Dauphin N3Torque Data Select 9 Bell Torque Data Select 10 Bell Summary DataConnection Summary Data Fault Designation Engine 1 BUSTorque Data Select 14 Coast Guard HH-65 Summary Data Torque Data Select 16 Common DC TorqueTable E Description Category 2, AIR Data Input SelectTable E 3.1.2 AIR Data Input Select for Egpws Mkxxii Fault Designation AIR Data BUS Bus Type Basic Configuration DataType Summary Data Table E 3.1.2-3 AIR Data Input Select #3 Summary Data Table E 3.1.2-5 AIR Data Input Select #5 Table E 3.1.2-4 AIR Data Input Select #4 Summary DataConnect to Channel Table E 3.1.2-10 AIR Data Input Select #10 Channel 429RX2Table E 3.1.2-6 AIR Data Input Select #6 Channel Connect toTable E 3.1.2-11 AIR Data Input Select #11 Summary Data Category 3, Position Input Select 3.3Position Input Type TableE Description UTC Fault Designation GPS BUS Bus Type BasicInternal Fault Designation Internal GPS Bus Type BasicBus Type Basic Fault Designation GPS BUSApp Cfg Category 4, Altitude CalloutsTable E 3.1.4 Altitude Callouts for Egpws Mkxxii Honeywell MK Xxii Egpws Installation Manual Table E 3.1.5-128 Audio Menu Type 128 Basic Helicopter Category 5, Audio Menu SelectEffectivity App Cfg 006 Table E 3.1.5 Audio Menu TypeDefined By IDand TCF Disable Application NotesCategory 6, Terrain Display Select Section OverviewHoneywell MK Xxii Egpws Installation Manual Table E KC Picture Bus Table Table E 3.1.6-2 TA&D / TCF Disabled Table Table E 3.1.6-1 No Display TAD and TCF EnabledChannel Integration note Fault Designation Display BUS Bus Type BasicDisplay Configuration Group 6 Collins PRO-LINE II Table Table E 3.1.6-3 Collins ProLine IITable 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 40/50Display Configuration Group 8 Integrated Efis 40/50 Peaks Always EnabledTable 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 Reference Name Integration note PinsTerrain Display BUS #1 453TX1 Terrain Display BUS #2Terrain Display BUS #2 453TX2 Table E 3.1.6-14 Bendix PPI-4A/4B without Auto RangeReference Name PIN Function 6.2-3 Display Input Control Group6.3-0OUTPUT 429 BUS Group Traceability Reference section Table E 3.1.6-16 Bendix IN182A/IN812A Radar display RDROutput 429 Bus Group Pins CommentsTA&D Alternate Pop Up False TA&D Alternate Pop Up True Table E Bendix IN842A/IN862A Radar display RDRFunction Value Category 7, Options Select Group #1Display 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 Channel 422RX2 Connect to DC811 #1 Display Input Control GroupConnect to DC811 #2 Honeywell MK Xxii Egpws Installation Manual SCI Bus RS-422 12K baud Altitude Reference6 Effectivity App Cfg Category 7, Options 1 SelectTable E 317 Options Select Group #1 True False WGS-84 Radio Altitude Type Table E Description Category 8, Radio Altitude Input SelectDescription Value PIN Type Channel Designation Reference PIN Function ConnectionReference Summary Data Table E 3.1.8-5 Radio Altitude Input Select Type 5 ALTConnection PIN Type Category 9, Navigation Input SelectTable E 3.1.9 Navigation Input Select for Egpws Mkxxii Table E 3.1.9-0 Navigation Inputs Select Summary DataFault Designation ILS BUS Fault Designation ILS BUS Bus T ype BasicTable E 3.1.10-0 Attitude Input Select Type Category 10, Attitude Input SelectAttitude Input Select Table E 3.1.10 Attitude Input Select for Egpws MKTable E 3.1.10-4 Attitude Input Select Type Fault Designation Ahrs BUSTable E 3.1.10-128 Attitude Input Select Type Connect to Table E 3.1.11 Heading Input Select for Egpws MK Fault Designation Ahrs BUS Bus Type BasicCategory 11, Heading Input Select Heading Input Select Table E DescriptionTable E 3.1.12 Windshear Input Select Category 12, Windshear Input SelectNo Windshear Effectivity App Cfg 003Input/Output Discrete Type Table E Category 13, Input / Output Discrete Type SelectState Configuration Data Possible StatesTable E 3.1.13-128 INPUT/OUTPUT Discrete Type Table E 3.1.13-129 INPUT/OUTPUT Discrete Type Category 14, Audio Output Level Volume SelectTable E 3.1.14 Audio Output Level Autorotation Threshold Torque Category 15, Autorotation ThresholdTable 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