Garmin G1000 Piper PA-46 Matrix - Manual (Page 399)

190-01108-00 Rev. B Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix 385
HAZARD AVOIDANCE
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
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-B System Test Fail TAWS FAIL “TAWS System Failure”
Table 6-13 TAWS-B System Test Status Annunciations
Manually testing the TAWS-B System:
1) Select the TAWS-B Page.
2) Press the MENU Key.
3) Select Test TAWS System and press the ENT Key to confirm the selection (Figure 6-106).
Figure 6-106 TAWS-B Page Menu