Garmin GTX 330 Installation Manual page 78

AMC
Item #
Section #
The latency of the horizontal position data,
including any uncompensated latency,
introduced by the (overall) ADS-B System does
28. 8.2.3
not exceed 1.5 second in 95% and 3 seconds in
99.9% of all ADS-B message transmission
cases (refer also to Table 1 in Appendix 3).
29. 8.3 ADS-B Transmit System
Compliance with the air-ground interoperability
requirements, as specified in ED-126 and
30. 8.3.1
presented in Section 7.1 and Appendix 4, needs
to be demonstrated.
31. 8.3.1 Aircraft identification
32. 8.3.1 SPI
33. 8.3.1 Emergency indicator
34. 8.3.1 Barometric altitude
35. 8.3.1 Quality indicator (NUC/NIC)
36. 8.3.1 Airborne Position Latitude
37. 8.3.1 Airborne Position Longitude
38. 8.3.1 Emergency status
39. 8.3.1 Quality indicator (NACp)
40. 8.3.1 Quality indicator (SIL)
41. 8.3.1 Version Indicator
GTX 330/330D Installation Manual
Page B-6
Table B-1 Compliance Matrix
AMC Item Compliance Summary
Garmin GNS Equipment: Total
position data latency is ≤ 1 second:
GPS antenna signal to Time of
Applicability: ≤500 ms
Position solution relayed to the
transponder ≤200 ms
Potential position solution update
delay until the next solution
overwrite is relayed to the
transponder ≤300 ms (given a 200
ms update rate)
Other:
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____________________________
____________________________
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[Section heading, no compliance
statement req'd]
See items below:
Supported in BDS (0,8) Aircraft
Identification and Category.
Supported in BDS (6,5) Aircraft
Operational Status.
Supported in BDS (6,1)
Emergency/Priority Status.
Supported in BDS (0,5) Airborne
Position.
Supported in BDS (0,5) Airborne
Position.
Supported in BDS (0,5) Airborne
Position.
Supported in BDS (0,5) Airborne
Position.
Supported in BDS (6,1)
Emergency/Priority Status.
Supported in BDS (6,5) Aircraft
Operational Status.
Supported in BDS (6,5) Aircraft
Operational Status.
Supported in BDS (6,5) Aircraft
Operational Status.
190-00207-02
Rev. U