Table B-1 Compliance Matrix - Garmin GTX 330 Installation Manual

AMC
Item #
Section #
1. 7.0 Functional Criteria
In line with ED-126 (section 4), the ADS-B
System needs to meet the following
2. 7.1
surveillance data transmission requirements, as
a minimum:
A unique ICAO 24 bit aircraft address
3. 7.1 (contained within each ADS-B message
transmission);
4. 7.1 Horizontal Position (latitude and longitude);
Horizontal Position Quality Indicator(s)
(position integrity for both ED-102/DO-260 and
5. 7.1 DO-260A based ADS-B transmit systems, as
well as accuracy for DO-260A based ADS-B
transmit systems);
6. 7.1 Barometric Altitude;
7. 7.1 Aircraft Identification;
8. 7.1 Special Position Identification (SPI);
GTX 330/330D Installation Manual
Page B-2

Table B-1 Compliance Matrix

AMC Item Compliance Summary
[Section heading, no compliance
statement req'd]
[Section heading, no compliance
statement req'd]
Supported in all Mode S
transmissions from the GTX 330.
Aircraft address data is sourced
from transponder internal
configuration settings.
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.
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.
Supported in BDS (0,5) Airborne
Position.
An encoding altimeter or other
altitude source provides this data to
the transponder.
Supported in BDS (0,8) Aircraft
Identification and Category.
Aircraft data is sourced from
transponder internal configuration
settings.
Supported in BDS (6,5) Aircraft
Operational Status.
SPI data is sourced from
transponder internal IDENT status.
The IDENT function is controlled
via GTX 330 or via remote located
button.
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Rev. U