Airplane Flight Manual Supplement

AFMS, GARMIN G500/G600 SYSTEM 190-00601-01 Rev. K
FAA APPROVED Page 34 of 51
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/G600 displays.
NOTE
The G500/G600 Cockpit Reference Guide and the
G500/G600 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.