Table 5-1: Gdl 82 Configuration Settings - Garmin GDL 82 Installation Manual

5.2.2 Configuration Settings
The Configuration / System page displays configuration data and allows the installer to change the
installation configuration. Once the configuration options are selected, power-cycle the GDL 82 unit to
apply the settings. The configuration settings can be saved to a plain text file for logging purposes by
selecting the Save Configuration To File button.
Go to the Configuration / System page in the GDL 8X Install Tool and apply the settings listed in Table
5-1.
ITEM
Aircraft
Tail Number: [1]
ICAO Address: [1]
Emitter Category:
Light Category Stall Speed: [2] 30 – 100 (Knots)
Squat Switch:
Transponder
VFR Squawk Code:
GPS
Source:
Lon Antenna Offset:
ADS-B
Anonymous Mode Switch: [3]
1090 ES Receive Capable:
UAT Receive Capable:
GDL 82 Mooney M20( ) Series STC Installation Manual

Table 5-1: GDL 82 Configuration Settings

CONFIGURATION
Enter Aircraft Tail Number
HEX
OCTAL
Light
Not Installed
GND (0V) = On Ground
GND (0V) = Airborne
1200
Internal
GNS Series
ADS-B+ Format 2
1 – 50
(Feet from nose)
Not Installed
Installed
Capable
Not Capable
Capable
Not Capable
Page 38 of 49
NOTES
This is the US registration number (N-
number).
Sets the ICAO address in octal or hex
format. Verify value with aircraft
registration records.
Only approved setting under this STC. For
aircraft with a maximum gross weight less
than 15,500 lbs.
Stall speed is used in the air/ground
determination. Select closest option.
This input determines the on-ground status
of the aircraft (i.e., airborne/on-ground
switch).
Only approved setting under this STC.
Select if GDL 82 with GPS/SBAS is used.
Select if external GPS source (via RS-232)
is a GNS 400W/500W Series Navigator.
Select if external GPS source (via RS-232)
is a GTN 6XX/7XX or GNS 480.
Installer must measure to determine an
accurate GPS (longitudinal) Antenna
Offset from the nose of the aircraft.
Select if optional switch is installed and
connected to discrete.
Select Capable if there is an ADS-B IN
receiver in the aircraft, such as a GDL 39()
or GDL 51/52.
190-01810-10
Rev. 1