190-00592-06 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA40/40F
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 6-81 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 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
Aural Message
System Test in Progress
None
System Test Pass
None
“TAWS System Test OK”
TAWS System Test Fail
“TAWS System Failure”
Table 6-11 TAWS System Test Status Annunciations
Manually testing the TAWS System:
1)
Select the TAWS-B Page.
2)
Press the
MENU
Key (Figure 6-82).
3)
Select ‘Test TAWS’ and press the
ENT
Key to confirm the selection.
Figure 6-82 TAWS-B Page Menu
Содержание Diamond DA40
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