System Status - Garmin G950 Pilot's Manual

HAZARD AVOIDANCE
1000
900
800
700
600
500
400
300
200
100
0
0
1000
900
800
700
600
500
400
300
200
100
0
0

SYSTEM STATUS

During power-up, TAWS-B conducts a self-test of its alerting capabilities. The system test can also be manually
initiated. A voice alert 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 6-64).
3) Select 'Test TAWS System' and press the ENT Key to confirm the selection.
344
20 40 60
Altitude Loss (Feet)
Figure 6-62 Negative Climb Rate (NCR) Altitude Loss
"DON'T SINK"
"TOO LOW, TERRAIN"
500 1000 1500 2000 2500 3000
Sink Rate (FPM)
Figure 6-63 Negative Climb Rate (NCR) Sink Rate
Garmin G950 Pilot's Guide for the Pilatus PC-6
"DON'T SINK"
or
"TOO LOW, TERRAIN"
80 100 120
or
3500 4000 4500 5000 5500 6000
140
6500 7000
190-00870-02 Rev. A