190-01499-02 GTX 3X5 Transponder TSO Installation ManualRev. 9 Page E-9CS-ACNS Compliance MatrixE.3 ADS-BTable E-3 ADS-BCS ACNS.D.EHS.020 IntegrityThe Mode S EHS airborne surveillance systemintegrity is designed commensurate with a 'minor'failure condition for the downlink aircraftparameters listed in CS ACNS.D.EHS.015.The GTX 3X5 is designed to meet design assurancelevel C which exceeds the “minor” failureclassification for Mode S EHS.CS ACNS.D.EHS.025 ContinuityThe Mode S EHS airborne surveillance systemcontinuity is designed to an allowable qualitativeprobability of “probable” for the downlink aircraftparameters listed in CS ACNS.D.EHS.015.The GTX 3X5 units have a design assurance level ofC 'remote' for listed functions which exceeds theallowable qualitative probability of “probable.”The GTX units have a maximum EHS system failurerate of no less than 5000 hrs using the MTBF rates,or 2.0E-04 failure rate.CS-ASNS SECTION CS-ACNS DESCRIPTION COMPLIANCE SUMMARYCS ACNS.D.ADSB.001 Applicability This section provides standards for 1090 MHzExtended Squitter (ES) ADS-B Out installations.Information only, no compliance statementnecessary.CS ACNS.D.ADSB.010 ADS-B Out SystemApprovalThe equipment contributing to the ADS-B Outfunction is approved.The GTX units are TSO Class 1 Level 2 transponderwith Level C (Major) Failure classification with SImode capability. They are 1090ES capabletransponders that require a valid pressure altitudesource, a valid GPS source, and meet ELSrequirements.CS ACNS.D.ADSB.020 ADS-B Out DataParametersa) The ADS-B Out system provides the followingminimum set of data parameters:1. Aircraft Identification 1. Supported in BDS (0,8) Aircraft Identificationand Category, and sourced from the operator viathe GTX panel, a compatible control device, ortransponder configuration settings. Priority: (1)Flight ID, (2) Aircraft RegistrationCS-ACNS SECTION CS-ACNS DESCRIPTION COMPLIANCE SUMMARY
