Manuals / Honeywell / Baby / Crib Toy

Honeywell MKXXII Audio Inhibit Discrete, Landing Gear Discrete, Weight on Wheels WOW Discrete

Models: MKXXII

1 254

Download 254 pages 42.79 Kb

Page 97

Honeywell

MK XXII EGPWS Installation Manual

3.3.13.3 Audio Inhibit Discrete

The Audio Inhibit discrete is an optional input to maintain audio and visual prioritization. When activated, this discrete inhibits all audio (Ground Proximity and Terrain Awareness). Activation of the Audio Inhibit input for more than 60 seconds will result in the “All Modes Inhibit” fault.

The Audio Inhibit discrete input can be connected to any or all of the following (as applicable to the aircraft configuration):

-a separately labeled guarded cockpit switch

For some existing GPWS installations, this discrete may have been tied to the analog Radio Altimeter Receiver-Transmitter Self-Test output. This connection is no longer required but may be left intact for this installation.

Discrete

Audio Inhibit +28

Position / Status

Inhibit = +28V

Not Inhibit = Gnd/Open

Connector Pin

J1-36

Honeywell does not recommend the use of this input for Helicopters.

3.3.13.4 Landing Gear Discrete

Landing Gear discrete is supplied by the Gear (or Gear handle) switch. The active position (+28V or GND) indicates “Gear Down” and should be connected to a contact that will indicate Gear Down when the Gear are lowered.

Discrete

Landing Gear +28

Landing Gear Gnd

Position / Status

Down = +28V

Not Down = Gnd/Open

Down = Gnd

Not Down = +28V /Open

Connector Pin

J1-35

J1-16

For fixed gear or skid equipped aircraft this input is not required.

3.3.13.5 Weight ON Wheels (WOW) Discrete

The Weight on Wheels (WOW) discrete is supplied by the WOW system in the aircraft. Connection can be made to the actual OLEO switch or relay logic later in the aircraft wiring.

For aircraft without WOW indication such as those with fixed gear or skids, this input discrete is not required.

Discrete

WOW +28

WOW Gnd

Position / Status

On Ground = +28V In Air = Gnd/Open

On Ground = Gnd

In Air = +28V /Open

Connector Pin

J1-37

J1-18

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

REV: C SHEET 97

Image 97

Honeywell MKXXII installation manual Audio Inhibit Discrete, Landing Gear Discrete, Weight on Wheels WOW Discrete

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 Introduction How To Use This Docu mentApplicability 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 CableUnits Supplied Configuration ModuleMK 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 sCircuit Breaker GPS Antenna & cableAnnunciators & 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 Primary Power Input System Wiring/ Electr ical InterfacesChassis Ground Discrete Inputs Analog and Digital Inp utsSerial 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 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 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 Purpose Introduction Part NumberSystem 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 2.9GPS 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 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 PortGround Discrete Characteristics Configuration Module InterfaceGPS 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 BUSArinc 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 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 DataTable 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 3.1.2-6 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 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 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 3.1.6-2 TA&D / TCF Disabled Table Table E 3.1.6-1 No Display TAD and TCF EnabledChannel 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 40/50Display 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 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 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 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 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 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 TypeTable E 3.1.10-4 Attitude Input Select Type Fault Designation Ahrs BUSTable 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 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