Garmin G1000 PDAs & Smartphones User Manual


  Open as PDF
of 632
 
Garmin G1000 Pilot’s Guide for Cessna Nav III
190-00498-07 Rev. A
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
392
HAZARD AVOIDANCE
Figure 6-150 Negative Climb Rate (NCR) Altitude Loss
0
100
200
300
400
500
600
700
800
900
1000
0 20 40 60 80 100 120 140
Altitude Loss (Feet)
Height Above Terrain (Feet)
“DON’T SINK”
or
“TOO LOW, TERRAIN”
Figure 6-151 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 Terrain (Feet)
“DON’T SINK”
or
“TOO LOW, TERRAIN”
SYSTEM STATUS
Duringpower-up,TAWS-Bconductsaself-testofitsauralandvisualannunciations.Thesystemtestcanalso
bemanuallyinitiated.Anauralmessageisissuedattestcompletion.TAWS-BSystemTestingisdisabledwhen
groundspeedexceeds30knots.
Manually testing the TAWS-B System:
1) Select the TAWS-B Page.
2) Press the MENU Key (Figure 6-152).
3) Select ‘Test TAWS System’ and press the ENT Key to confirm the selection.
 previous next