Garmin GTX 330 Installation Manual page 75

AMC
Item #
Section #
9. 7.1 Emergency Status and Emergency Indicator;
Version Number (in aircraft operational status
10. 7.1
message, if avionics are DO-260A compliant).
In line with ED-126 (section 4), it is
recommended that the ADS-B System meets
11. 7.2
the following optional surveillance data
transmission requirement: Ground Velocity
12. 8 Airworthiness Considerations
Airworthiness Certification Objectives
For the purposes of the ADS-B-NRA
application, the ADS-B System installed in the
13. 8.1
aircraft needs to be designed to deliver data that
satisfy the airborne domain requirements in line
with ED-126 Section 3.4, (Appendix 3 provides
a summary for information purposes).
Horizontal Position and Horizontal Position
Quality Indicator(s)
14. 8.1
Requirement: 10
ADS-B System Continuity
15. 8.1
Requirement: 2*10
Horizontal Position Latency
16. 8.1 Requirement: 1.5 sec/95% (Appendix 3, Table
1)
190-00207-02
Rev. U
Table B-1 Compliance Matrix
AMC Item
-5
/fh (Appendix 3, Table 1)
-4
/fh (Appendix 3, Table 1)
Compliance Summary
Supported in BDS (6,1)
Emergency/Priority Status.
Data is sourced from current Mode
A code status. The Mode A code is
entered via transponder code keys.
Supported in BDS (6,5) Aircraft
Operational Status.
Supported in BDS (0,5) Airborne
Velocity.
The GPS source sends this data to
the transponders when it has a
position solution.
[Section heading, no compliance
statement req'd]
See items below compiled from
AMC 20-24 Appendix 3 Tables:
Garmin GNS Equipment: GPS/
SBAS engine meets the 10
hour requirement.
Other:
____________________________
____________________________
____________________________
____________________________
_____________
The GTX 330 meets the continuity
-4
requirement of 2*10
See Item 28 Response.
GTX 330/330D Installation Manual
-5
per
/fh.
Page B-3