System status, Hazard avoidance – Garmin G1000 Quest Kodiak User Manual
Page 342
Garmin G1000 Pilot’s Guide for the Quest Kodiak 100
190-00590-02 Rev. A
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
330
HAZARD AVOIDANCE
Figure 6-65 Negative Climb Rate (NCR) Sink Rate
0
100
200
300
400
500
600
700
800
900
1000
0
500
1000
1500
2000
2500
3000
3500
4000
4500
5000
5500
6000
6500
7000
Sink Rate (FPM)
Height
Above
Terr
ain (F
eet)
“DON’T SINK”
or
“TOO LOW, TERRAIN”
SYSTEM STATUS
During G1000 power-up, TAWS conducts a self-test of its aural and visual annunciations. The system test can
also be manually initiated. An aural alert is issued at test completion. TAWS System Testing is disabled when
ground speed exceeds 30 knots.
Alert Type
PFD/MFD Alert
Annunciation
TAWS Page
Annunciation
Aural Message
System Test in Progress
TAWS TEST
None
System Test Pass
None
None
“TAWS System Test OK”
TAWS System Test Fail
TAWS FAIL
“TAWS System Failure”
Table 6-12 TAWS System Test Status Annunciations