Garmin G5 Installation Manual page 127

Electronic flight instrument, part 23 aml stc
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Config Page
Magnetometer
Flight Controls
Backlight
Display
Battery
GPS
Navigation
Units
RS-232
ARINC 429
Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual
Config Option
VY
VG
VR
VMC
VYSE
Magnetometer
Orientation
Garmin Autopilot Servos
Analog Autopilot Interface
Current Mode
Default Mode
Minimum Photocell Input
Minimum Display Brightness
Maximum Photocell Input
Maximum Display Brightness
Filter Time Constant
HSI Page
Power Up Page
Show Battery Status
Automatic Power Off
Internal GPS Receiver
GPS Data Fields
Navigation Data
Selected Course
Selected Course 1
Selected Course 2
VNAV Deviation Scale
Altitude
Distance
Airspeed
Ground Speed
Ground Track
Vertical Speed
Pressure
Input Format
Output Format
Output 1
Page 127
Configuration Setting
(1)(2)(3)
(1)(2)(3)
(1)(2)(3)
(1)(2)(3)
(1)(2)(3)
Enabled
Connector Aft
Or
Connector Forward
Or
Connector Port
Or
Connector Starboard
None
None
Or
See Section 5.23 if a Non-Garmin Autopilot is interfaced
Automatic
Automatic
Default
Default
Default
Default
Default
Enabled
HSI
When Using Battery
On Ground Only
Disabled (WAAS Units)
Enabled (Non WAAS Units)
Show
Enabled
Note: If an autopilot interface is configured, this
configuration page is set to ENABLED by default.
Enabled (5)
(6)
(6)
(5)
(1)(2)
(1)(2)
(1)(2)(3)
(1)(2)
Magnetic
(1)(2)
(1)(2)
MapMx (WAAS Units)
AVIATION (Non WAAS Units)
None
EFIS / AIRDATA 1 (SDI 1)
(Only used with GTN 6XX/7XX and GNS 4XX(W) /
5XX(W) with no autopilot or Garmin autopilot interfaced)
EFIS / AIRDATA 2 (SDI 1)
(Always used with GNS 480 and GTN 6XX / 7XX and
GNS 4XX(W) / 5XX(W) when Non-Garmin Autopilot is
interfaced)
190-01112-10
Rev. 21

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