Ads-B - Garmin GTX 3X5 Series Installation Manual

CS-ACNS SECTION
CS ACNS.D.EHS.020 Integrity
CS ACNS.D.EHS.025 Continuity
E.3

ADS-B

CS-ASNS SECTION
CS ACNS.D.ADSB.001 Applicability
CS ACNS.D.ADSB.010 ADS-B Out System
Approval
CS ACNS.D.ADSB.020 ADS-B Out Data
Parameters
190-01499-02
Rev. 9
CS-ACNS DESCRIPTION
The Mode S EHS airborne surveillance system
integrity is designed commensurate with a 'minor'
failure condition for the downlink aircraft
parameters listed in CS ACNS.D.EHS.015.
The Mode S EHS airborne surveillance system
continuity is designed to an allowable qualitative
probability of "probable" for the downlink aircraft
parameters listed in CS ACNS.D.EHS.015.
Table E-3 ADS-B
CS-ACNS DESCRIPTION
This section provides standards for 1090 MHz
Extended Squitter (ES) ADS-B Out installations.
The equipment contributing to the ADS-B Out
function is approved.
a) The ADS-B Out system provides the following
minimum set of data parameters:
1. Aircraft Identification
CS-ACNS Compliance Matrix
COMPLIANCE SUMMARY
The GTX 3X5 is designed to meet design assurance
level C which exceeds the "minor" failure
classification for Mode S EHS.
The GTX 3X5 units have a design assurance level of
C 'remote' for listed functions which exceeds the
allowable qualitative probability of "probable."
The GTX units have a maximum EHS system failure
rate of no less than 5000 hrs using the MTBF rates,
or 2.0E-04 failure rate.
COMPLIANCE SUMMARY
Information only, no compliance statement
necessary.
The GTX units are TSO Class 1 Level 2 transponder
with Level C (Major) Failure classification with SI
mode capability. They are 1090ES capable
transponders that require a valid pressure altitude
source, a valid GPS source, and meet ELS
requirements.
1. Supported in BDS (0,8) Aircraft Identification
and Category, and sourced from the operator via
the GTX panel, a compatible control device, or
transponder configuration settings. Priority: (1)
Flight ID, (2) Aircraft Registration
GTX 3X5 Transponder TSO Installation Manual
Page E-9