Garmin GTX 33 Installation Manual - Page 54

Table B-1., Version 1 ADS-B Field Approval Compliance Matrix, GTX 33 Installation Manual, B-2

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Item # 1. 2. 3. Table B-1. Version 1 ADS-B Field Approval Compliance Matrix AMC Section # 7.0 7.1 7.1 AMC Item Compliance Summary Functional Criteria In line with ED-126 (section 4), the ADS-B System needs to meet the following surveillance data transmission requirements, as a minimum; A unique ICAO 24 bit aircraft address (contained within each ADS-B message transmission); [Section heading, no compliance statement req'd] [Section heading, no compliance statement req'd] Supported in all Mode S transmissions from the GTX 33. Aircraft address data is sourced from transponder internal configuration settings. Supported in BDS (0,5) Airborne Position. Supported in BDS (0,5) Surface 4. 7.1 Horizontal Position (latitude and longitude); Position. The GPS source sends this data to the transponder when it has a position solution. Supported in BDS (0,5) Airborne Position. Horizontal Position Quality Supported in BDS (0,5) Surface Indicator(s) (position integrity for both Position. ED-102/DO-260 and 5. 7.1 DO-260A based ADS-B transmit systems, as well as accuracy for DO- Supported in BDS (6,5) Aircraft 260A based ADS-B transmit sys- Operational Status. tems); The GPS source sends this data to the transponder when it has a position solution. Supported in BDS (0,5) Airborne Position. 6. 7.1 Barometric Altitude; An encoding altimeter or other altitude source provides this data to the transponder. GTX 33 Installation Manual Page B-2 190-00906-00 Rev. F

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GTX 33 Installation Manual
190-00906-00
Page B-2
Rev. F
Table B-1.
Version 1 ADS-B Field Approval Compliance Matrix
Item #
AMC
Section #
AMC Item
Compliance Summary
1.
7.0
Functional Criteria
[Section heading, no
compliance statement req’d]
2.
7.1
In line with ED-126 (section 4), the
ADS-B System needs to meet the fol-
lowing surveillance data
transmission requirements, as a mini-
mum;
[Section heading, no
compliance statement req’d]
3.
7.1
A unique ICAO 24 bit aircraft address
(contained within each ADS-B mes-
sage transmission);
Supported in all Mode S
transmissions from the
GTX 33. Aircraft address data
is sourced from transponder
internal configuration settings.
4.
7.1
Horizontal Position (latitude and
longitude);
Supported in BDS (0,5) Airborne
Position.
Supported in BDS (0,5) Surface
Position.
The GPS source sends this data to
the transponder when it has a
position solution.
5.
7.1
Horizontal Position Quality
Indicator(s) (position integrity for both
ED-102/DO-260 and
DO-260A based ADS-B transmit
systems, as well as accuracy for DO-
260A based ADS-B transmit sys-
tems);
Supported in BDS (0,5)
Airborne Position.
Supported in BDS (0,5) Surface
Position.
Supported in BDS (6,5) Aircraft
Operational Status.
The GPS source sends this data to
the transponder when it has a
position solution.
6.
7.1
Barometric Altitude;
Supported in BDS (0,5)
Airborne Position.
An encoding altimeter or other
altitude source provides this
data to the transponder.