190-01499-02
GTX 3X5 Transponder TSO Installation Manual
Rev. 9
Page E-11
CS-ACNS Compliance Matrix
CS ACNS.D.ADSB.020 ADS-B Out Data
Parameters
(continued)
5. Pressure Altitude (incl. NICbaro)
5.
Supported in BDS (0,5) Airborne Position. An
encoding altimeter or other altitude source
provides this data to the transponder. NICbaro
is provided in BDS register (6,2) and (6,5).
6. Special Position Identification (SPI)
6.
Supported in BDS (6,5) Aircraft Operational
Status. SPI data is sourced from transponder
internal IDENT status. The IDENT function is
controlled via GTX or via remote located
button, which can also be activated via
approved control source.
7.
7.
a.
Emergency Status
a.
Supported in BDS (6,1) Emergency/
Priority Status.
b.
Emergency Indication
b.
Data is sourced from current Mode A
code status. The Mode A code is entered
and displayed via the GTX panel or a
compatible control device.
8. 1090 ES Version Number
8.
Supported in BDS (6,5) Aircraft Operational
Status, Bits 41-43 are populated with '2'.
9.
9.
a.
Airborne velocity over Ground - (East/
West and North/South
a.
Supported in BDS (0,9) Airborne Velocity
Subtype 1&2.
b.
Airborne/Surface Navigation Accuracy
Category for Velocity: NACv
b.
Supported in BDS (0,9) Airborne Velocity
Subtype 1&2.
10. Emitter Category
10. Supported in BDS (0,8) Extended Squitter
Identification and data source from
transponder configuration.
11. Vertical Rate
11. Supported in BDS (0,9) Airborne Velocity
12.
12.
CS-ASNS SECTION
CS-ACNS DESCRIPTION
COMPLIANCE SUMMARY
Содержание GTX 335
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