190-02692-00 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-32 Saratoga
337
HAZARD AVOIDANCE
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
Figure 6-75 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 T
err
ain
(Feet)
“DON’T SINK”
SYSTEM STATUS
During initialization, TAWS-B conducts a self-test of its visual annunciations and voice alerts. The system test
can also be manually initiated. The system issues a voice alert when the test has concluded. TAWS-B System
Testing is disabled when ground speed exceeds 30 knots.
Alert Type
PFD/MFD Alert
Annunciation
TAWS-B
Page Center
Annunciation
Voice Alert
System Test in Progress
TAWS TEST
TAWS TEST
None
System Test Pass
None
None
“TAWS System Test OK”
TAWS-B System Test Fail
TAWS FAIL
TAWS FAIL
“TAWS System Failure”
Table 6-17 TAWS-B System Test Status Annunciations
Manually testing the TAWS-B System:
1)
Select the MAP - TAWS-B Page.
2)
Press the
MENU
Key.
3)
Select ‘Test TAWS System’ and press the
ENT
Key to confirm the selection.