Garmin Software Version 0829.00 Betriebsanweisung Seite 27

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700
190-01247-00 Rev. A 11
Engine & Airframe Systems
Flight
Instruments EAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
Left Fuel
Tank
Selected
Switching
Fuel Tank
Selection
Right
Fuel Tank
Selected
Unknown
Fuel Tank
Selection
Fuel
Selector
Off
Fuel Selector Status
If the auxiliary fuel boost pump is on, the symbol is displayed in green. The mode,
automatic (AUTO) or manual (MAN) is displayed next to the pump symbol. If the
boost pump is off, the symbol is shown in light blue (automatic mode) or red (manual
mode).
Fuel Boost Pump
On
Fuel Boost Pump
Off (Auto)
Fuel Boost Pump
Off (Manual)
Auxiliary Boost Pump Status
GENERAL SYSTEMS
1)
Select the SYSTEM Softkey to display the softkeys for the synoptics system.
2)
Select the GEN Softkey to display the Fuel System Page.
The General Synoptics Page aircraft diagram displays open doors in red (CAS mes-
sages also generated). Statuses of stall sensor, propeller, and pitot probes heat are also
indicated on the diagram:
• Whiteindicatesthatheatisoff(propeller)
• Greenindicatesheatison
• Yellowindicatesheathasfailed(stallsensor,propellerandpitottube).
Invalid sensor information is indicated with a red ‘X’.
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