Garmin G1000 Quest Kodiak - Manual (Page 87)

190-00590-03 Rev. A Garmin G1000 Pilot’s Guide for the Quest KODIAK 100 75
FLIGHT INSTRUMENTS
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
The Annunciation Window appears to the right of the Vertical Speed Indicator (Figure 2-34) and displays
abbreviated annunciation text for aircraft alerts. Warnings appear in red, cautions in yellow, advisory alerts
in white, and safe operating annunciations in green. New alerts are displayed at the top of the Annunciation
Window, regardless of priority. Once acknowledged, they are sequenced based on priority.
Critical values generated by redundant sensors are monitored by comparators. If differences in the sensors
exceed a specified amount, the Comparator Window appears in the upper right corner of the PFD (Figure 2-34)
and the discrepancy is annunciated in the Comparator Window as a MISCOMP (miscompare). If one or both
of the sensed values are unavailable, it is annunciated as a NO COMP (no compare).
Reversionary sensor selection is annunciated in a window on the right side of the PFD (Figure 2-34). These
annunciations reflect reversionary sensors selected on one or both PFDs. Pressing the SENSOR Softkey accesses
the ADC1, ADC2, AHRS1, and AHRS2 softkeys. These softkeys allow switching of the sensors being viewed
on each PFD. With certain types of sensor failures, the system may make some sensor selections automatically.
The GPS sensor cannot be switched manually.
MARkER bEACON ANNUNCIATIONS
Marker Beacon Annunciations are displayed on the PFD to the left of the Selected Altitude. Outer marker
reception is indicated in blue, middle in yellow, and inner in white. Refer to the Audio Panel and CNS Section
for more information on Marker Beacon Annunciations.
Figure 2-35 Marker Beacon Annunciations
Inner Marker Outer Marker
Altimeter
Middle Marker