Table of Contents
1.0INTRODUCTIONANDDESCRIPTION
2.0INTERCHANGEABILITYSTANDARDS
3.0SYSTEMCHARACTERISTICS
4.0TRANSPONDERUNITDESCRIPTION
5.0BUILT-INTESTANDMAINTENANCEPROVISIONS
6.0CONTROLPANELDESIGN
7.0ANTENNA
ATTACHMENTS
ATTACHMENT1A-TRANSPONDERUNITCONNECTORPOSITIONING
ATTACHMENT1B-CONTROLUNITCONNECTORPOSITIONING
ATTACHMENT1C-INDEXPINCODING
ATTACHMENT1D-NOTESTOCONNECTORKEYING
ATTACHMENT2A-1-TIFANDMINIMUMSUBSETCONFIGURATIONS
PINALLOCATION-MINIMUMSUBSET
ATTACHMENT2A-2-TIFANDMINIMUMSUBSETCONFIGURATIONS
STANDARDINTERWIRING
ATTACHMENT2A-3-TIFANDMINIMUMSUBSETCONFIGURATIONS
NOTESAPPLICABLETOSTANDARDINTERWIRING
ATTACHMENT2B-1-MINIMUMSUBSET,SINGLE-SIDEDCONFIGURATION
PINALLOCATION
ATTACHMENT2B-2-MINIMUMSUBSET,SINGLE-SIDEDCONFIGURATION
STANDARDINTERWIRING
ATTACHMENT2B-3-MINIMUMSUBSET,SINGLE-SIDEDCONFIGURATION
NOTESAPPLICABLETOSTANDARDINTERWIRING
ATTACHMENT2C-1-MINIMUMTIF,DOUBLESIDEDCONFIGURATION
PINALLOCATION
ATTACHMENT2C-2-MINIMUMTIF,DOUBLE-SIDEDCONFIURATION
STANDARDINTERWIRING
ATTACHMENT2C-3-MINIMUMTIF,DOUBLE-SIDEDCONFIGURATION
NOTESAPPLICABLETOSTANDARDINTERWIRING
ATTACHMENT2D-TRANSPONDER/CONTROLPANELWIRING
ATTACHMENT2E-TRANSPONDERDATASOURCESELECTIONSWITCHING
ATTACHMENT3-SOURCESFORGICBREGISTERLOADINGANDSAMPLE
INTERFACES
ATTACHMENT3A-PRIMARYSOURCESOFARINC429INPUTDATA
ATTACHMENT3A-1-NOTESTOTHEPRIMARYSOURCESOFARINC429
INPUTDATA
ATTACHMENT3B-ARINC429OUTPUTDATA
ATTACHMENT3C-ADDITIONALARINC429INPUTANDOUTPUT
ATTACHMENT3D-SAMPLEINTERFACECONFIGURATIONS
ATTACHMENT4-ARINC429DATAWORDS
ATTACHMENT5-DLPINTERFACE
ATTACHMENT6-SUPPRESSIONPULSESYSTEMCHARACTERISTICS
ATTACHMENT7-DIVERSITYANTENNASELECTION
ATTACHMENT8-TYPICALBLADEANTENNA
ATTACHMENT9-AIRPLANEPERSONALITYMOUDLE(APM)IMPLEMENTATION
GUIDELINESFORTHETRANSPONDER
ATTACHMENT10-EXAMPLEGICBREGISTERLOADINGARCHITECTURE
ATTACHMENT11-MODEAREPLYCODECOMBINATIONS
APPENDICES
APPENDIXA-ACRONYMLIST
APPENDIXB-OPTIONALCONTROLPANELCONFIGURATION Abstract
Describes the interface definitions necessary to use the Extended Squitter capability of the Mark 4 Transponder to provide ADS-B parameters as required by RTCA DO-260A and ICAO Doc. 9871.
