Garmin GTX 33 Installation Manual - Page 60

GTX 33 Installation Manual, B-8, Rev. F

Page 60 highlights

Item # Table B-1. Version 1 ADS-B Field Approval Compliance Matrix AMC Section # AMC Item Compliance Summary Garmin GNS/GTN Equipment: Total position data latency is ≤ 1 second: GPS antenna signal to Time of Applicability: ≤500 ms The latency of the horizontal position data, including any uncompensated latency, Position solution relayed to the transponder ≤200 ms introduced by the (overall) ADS-B 28. 8.2.3 System does not exceed 1.5 second Potential position solution update in 95% and 3 seconds in 99.9% of all delay until the next solution over- ADS-B message write is relayed to the transponder ≤300 ms (given a 200 ms update transmission cases (refer also to rate) Table 1 in Appendix 3). Other: 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) GTX 33 Installation Manual Page B-8 [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. 190-00906-00 Rev. F

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GTX 33 Installation Manual
190-00906-00
Page B-8
Rev. F
28.
8.2.3
The latency of the horizontal
position data, including any uncom-
pensated latency,
introduced by the (overall) ADS-B
System does 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).
Garmin GNS/GTN 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 over-
write is relayed to the transponder
300 ms (given a 200 ms update
rate)
Other:
29.
8.3
ADS-B Transmit System
[Section heading, no
compliance statement req’d]
30.
8.3.1
Compliance with the air-ground
interoperability requirements, as
specified in ED-126 and
presented in Section 7.1
and Appendix 4, needs to be
demonstrated.
See items below:
31.
8.3.1
Aircraft identification
Supported in BDS (0,8) Aircraft
Identification and Category.
32.
8.3.1
SPI
Supported in BDS (6,5) Aircraft
Operational Status.
33.
8.3.1
Emergency indicator
Supported in BDS (6,1)
Emergency/Priority Status.
34.
8.3.1
Barometric altitude
Supported in BDS (0,5)
Airborne Position.
35.
8.3.1
Quality indicator (NUC/NIC)
Supported in BDS (0,5)
Airborne Position.
Table B-1.
Version 1 ADS-B Field Approval Compliance Matrix
Item #
AMC
Section #
AMC Item
Compliance Summary