Pilot's Guide

190-00663-02 Rev. B
Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT/GTi
365
HAZARD AVOIDANCE
Figure 6-92 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 6-93 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.Asinglechime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.
3) Select ‘Test TAWS System’ and press the ENT Key to confirm the selection. (Figure 6-94)