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ARINC 542A:1988

ARINC 542A:1988 Digital Flight Data Recorder Includes specific requirements necessary to support flight data recording and other flight data acquisition needs. Design details necessary to ensure interchangeability of equipment in a standard airc

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Table of Contents

1.0PURPOSEOFTHISDOCUMENT
1.1PurposeofThisDocument
1.2RelatedDocuments
1.2.1RelationshiptoOtherARINCCharacteristics
1.2.2OtherDocuments
1.3SystemFunctions
1.3.1BasicFunctions
1.3.2EnhancedFunctions
1.4UnitFunctions
1.4.1FlightDataRecorder
1.4.2Accelerometer
1.5ReliabilityandMaintainability
1.5.1Reliability
1.5.2Maintainability
1.6Interchangeability
1.7RegulatoryApproval
2.0INTERCHANGEABILITYSTANDARDS
2.1ImportanceofInterchangeability
2.2FormFactorsandConnectors
2.2.1FlightDataRecorder
2.2.2Accelerometers
2.3InputandOutputSignalCharacteristics
2.4StandardInterwiring
2.4.1WireSize
2.4.2ShieldingorSpecialCabling
2.4.3StandardCategoryWiring
2.4.4RadioJunctionBox
2.5PowerCircuitry
2.5.1PrimaryPowerInput
2.5.2PowerInterlocksandPowerControl
2.5.3SensorExcitation
2.6Weights
2.7EnvironmentalSpecification
2.8AbnormalConditions
2.8.1PowerInterruptsandLowPowerLevels
3.0SYSTEMDESIGN
3.1General
3.2SystemInterwiring
3.3Units
3.3.1FlightDataRecorder
3.3.2Accelerometer
3.4DataSources
3.5DataMultiplexing
3.6InputCircuitProtection
3.7SystemAccuracy
3.8MonitorOutput
3.9PowerMalfunctionIndication
3.10TripandDataEncoder
3.11RecordingTime
3.12AdditionalBinaryRecordingChannels
4.0STANDARDSIGNALCHARACTERISTICS
4.1General
4.2HeadingSensors
4.3Accelerometers
4.3.1ACAccelerometer
4.3.2OptionalDCAccelerometer
4.4DataCharacteristics
4.5SensorInputs
4.6ElapsedTime
ATTACHMENTS
1FAARequiredDataParameters
2ConnectorLocations
3FrontPanelHoseConnectors
4ARemoteAccelerationSensor
4BDCAccelerationFormFactor
5-1ARINC542AFDRStandardInterwiring
5-2NotestoStandardInterwiring
6TypicalDataCharacteristics
7DCAccelerometerPinAssignments
8ProgrammableInputWiring
APPENDICES
1DCAccelerometerDesign

Abstract

Includes specific requirements necessary to support flight data recording and other flight data acquisition needs. Design details necessary to ensure interchangeability of equipment in a standard aircraft installations is included.

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