Garmin GTX 33 Installation Manual - Page 55

GTX 33 Installation Manual, Rev. F, B-3, AMC Item, Compliance Summary

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Item # 7. Table B-1. Version 1 ADS-B Field Approval Compliance Matrix AMC Section # AMC Item Compliance Summary Supported in BDS (0,8) Aircraft Identification and Category. 7.1 Aircraft Identification; Aircraft data is sourced from transponder internal configuration settings. Supported in BDS (6,5) Aircraft Operational Status. 8. 7.1 Special Position Identification (SPI); SPI data is sourced from transponder internal IDENT status. The IDENT function is controlled via GTX 33 control and display device. Supported in BDS (6,1) Emergency/Priority Status. 9. 7.1 Emergency Status and Emergency Indicator; Data is sourced from current Mode A code status. The Mode A code is entered via GTX 33 control and display device. Version Number (in aircraft operational status message, if Supported in BDS (6,5) Aircraft 10. 7.1 avionics are DO-260A Operational Status. compliant). In line with ED-126 (section 4), it is Supported in BDS (0,5) recommended that the ADS-B Sys- Airborne Velocity. 11. 7.2 tem meets the following optional sur- veillance The GPS source sends this data to data transmission requirement: the transponders when it has a Ground Velocity position solution. [Section heading, no 12. 8 Airworthiness Considerations compliance statement req'd] 190-00906-00 Rev. F GTX 33 Installation Manual Page B-3

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190-00906-00
GTX 33 Installation Manual
Rev. F
Page B-3
7.
7.1
Aircraft Identification;
Supported in BDS (0,8) Aircraft
Identification and Category.
Aircraft data is sourced from
transponder internal
configuration settings.
8.
7.1
Special Position Identification (SPI);
Supported in BDS (6,5) Aircraft
Operational Status.
SPI data is sourced from
transponder internal IDENT
status. The IDENT function is
controlled via GTX 33 control and
display device.
9.
7.1
Emergency Status and
Emergency Indicator;
Supported in BDS (6,1)
Emergency/Priority Status.
Data is sourced from current
Mode A code status. The Mode
A code is entered via GTX 33 con-
trol and display device.
10.
7.1
Version Number (in aircraft
operational status message, if
avionics are DO-260A
compliant).
Supported in BDS (6,5) Aircraft
Operational Status.
11.
7.2
In line with ED-126 (section 4), it is
recommended that the ADS-B Sys-
tem meets the following optional sur-
veillance
data transmission requirement:
Ground Velocity
Supported in BDS (0,5)
Airborne Velocity.
The GPS source sends this data to
the transponders when it has a
position solution.
12.
8
Airworthiness Considerations
[Section heading, no
compliance statement req’d]
Table B-1.
Version 1 ADS-B Field Approval Compliance Matrix
Item #
AMC
Section #
AMC Item
Compliance Summary