Garmin G500 User Manual

AFMS, GARMIN G500 PFD/MFD SYSTEM 190-01102-01 Rev. 9
FAA APPROVED Page 29 of 40
3.3 Warnings, Cautions, and Advisories
The following tables show the color and significance of the warning, caution,
and advisory messages which may appear on the G500 displays.
NOTE
The G500 Cockpit Reference Guide and the G500 Pilot’s
Guide contain detailed descriptions of the annunciator system
and all warnings, cautions and advisories.
3.3.1 Warning annunciations – Red
Annunciation
Pilot Action
Cause
ATTITUDE FAIL
Use Standby
Attitude.
Display system is not receiving
attitude reference information from
the AHRS; accompanied by the
removal of sky/ground
presentation and a red X over the
attitude area.
AIRSPEED FAIL
Use Standby
Airspeed.
Display system is not receiving
airspeed input from the air data
computer; accompanied by a red X
through the airspeed display.
ALTITUDE FAIL
Use Standby
Altitude.
Display system is not receiving
altitude input from the air data
computer; accompanied by a red X
through the altimeter display.
VERT SPD FAIL
Cross check
instruments.
Display system is not receiving
vertical speed input from the air
data computer; accompanied by a
red X through the vertical speed
display.
HDG
Use Standby
Magnetic
Compass or GPS
track
information.
Display system is not receiving
valid heading input from the
AHRS; accompanied by a red X
through the digital heading display.
Red X
Reference the
data source or
alternate
equipment.
A red X through any display field,
indicates that display field is not
receiving data or is corrupted.

Garmin G500 Specifications

General

Operating Temperature	-20°C to +55°C
Display Size	6.5 inches
Display Type	LCD
Interface	RS-232, ARINC 429
Certification	TSO
Power Input	11-33 VDC