Garmin G1000 Quest Kodiak - Manual (Page 342)

Garmin G1000 Pilot’s Guide for the Quest KODIAK 100 190-00590-03 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-B 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-B System Testing is disabled
when ground speed exceeds 30 knots.
Alert Type
PFD/MFD Alert
Annunciation
TAWS-B 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 6-6 TAWS-B System Test Status Annunciations
Manually testing the TAWS-B System:
1) Select the TAWS-B Page.
2) Press the MENU Key (Figure 6-66).
3) Select ‘Test TAWS System’ and press the ENT Key to confirm the selection.
Figure 6-66 TAWS-B Page Menu