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Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are available relative to the position of the aircraft; the 360° default display and the radar-like ARC (120°) display. Map range is adjustable with the RANGE Knob from 1 to 200 nm, as indicated by the map range rings or arcs.
Displaying the TAWS Page:
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the TAWS Page.
Changing the TAWS Page view:
1) Select the VIEW Softkey.
2) Select the 360 or ARC Softkey to select the desired view.
Or:
1) Press the MENU Key.
2) Select ‘View 120º’ or ‘View 360º’, dependent on current state, and press the ENT Key to change the view.
Showing/hiding aviation information on the TAWS Page:
1) Press the MENU Key.
2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’, dependent on current state, and press the ENT Key.
336 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Hazard Avoidance voidance voidance
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Figure 6-60 TAWS Page, 360º View Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude)Red Terrain (Above or Within 100’ Below the Aircraft Altitude)Black Terrain (More than 1000’ Below the Aircraft Altitude)Terrain LegendMap Range RingsMap OrientationCurrent Aircraft GPS-derived MSL Altitude
Figure 6-61 TAWS Page (ARC View)Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude)Red Terrain (Above or Within 100’ Below the Aircraft Altitude)Black Terrain (More than 1000’ Below the Aircraft Altitude)Map Range ArcsTerrain Legend
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 337
Hazard Avoidance voidance voidance
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
TAWS Alerts
Alerts are issued when flight conditions meet parameters that are set within TAWS software algorithms. TAWS alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-6 shows TAWS alert types with corresponding annunciations and aural messages.
When an alert is issued, annunciations appear on the PFD and MFD. The TAWS Alert Annunciation is shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the TAWS Page is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the pop-up alert:
• Press the CLR Key (returns to the currently viewed page), or
• Press the ENT Key (accesses the TAWS Page)
Figure 6-62 Alert Annunciation on the PFDAlert Annunciation
Figure 6-63 Alert Pop-up on the MFD
338 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Hazard Avoidance voidance voidance
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Figure 6-64 TAWS PULL UP Alert Annunciation on the MFDAlert AnnunciationPotential Impact Point
TAWS Inhibit
PDA and FLTA aural and visual alerts can be manually inhibited. Use caution when inhibiting TAWS as the system should be enabled when appropriate. When TAWS is inhibited, the alert annunciation TAWS INHB is shown on the PFD and MFD.
Figure 6-65 TAWS Alerting Disabled (TAWS Inhibited) Annunciation
Inhibiting/enabling TAWS alerting:
1) Select the TAWS Page.
2) Select the INHIBIT Softkey to inhibit or enable TAWS (choice dependent on current state).
Or:
a) Press the MENU Key.
b) Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current state) and press the ENT Key.
If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint during a GPS WAAS approach, a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments Section for details.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 339
Hazard Avoidance voidance voidance
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
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Cessna Citation Mustang G1000 Integrated Flight Dec(119)
