Garmin G1000 King Air C90GT - Manual (Page 96)

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-01 Rev. A 82
FLIGHT INSTRUMENTS
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
TAWS ANNUNCIATIONS
Terrain Awareness and Warning System (TAWS) annunciations appear on the PFD to the upper left of
the Altimeter. Refer to the Hazard Avoidance Section and Appendix A for information on TAWS alerts and
annunciations.
Figure 2-45 Traffic and Example TAWS Annunciations
Inset Map Enabled,
Displaying Traffic
When TA Detected
ALTITUDE ALERTING
The Altitude Alerting function provides the pilot with visual and aural alerts when approaching the Selected
Altitude. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is
independent of the GFC 700 AFCS, but alerting tones are generated only when the GFC 700 is installed. The
following occur when approaching the Selected Altitude:
• Upon passing through 1000 feet of the Selected Altitude, the Selected Altitude (shown above the Altimeter)
changes to black text on a light blue background, flashes for 5 seconds, and an aural tone is generated.
• When the aircraft passes within 200 ft of the Selected Altitude, the Selected Altitude changes to light blue text
on a black background and flashes for 5 seconds.
• After reaching the Selected Altitude, if the pilot flies outside the deviation band (±200 feet of the Selected
Altitude), the Selected Altitude changes to yellow text on a black background, flashes for 5 seconds, and an
aural tone is generated.
Figure 2-46 Altitude Alerting Visual Annunciations
Within 1000 ft Within 200 ft Deviation of ±200 ft