Garmin GTX 33, Installation Manual, Page: 54 / 83

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.