Garmin G1000 Cockpit Reference Guide for the Socata TBM 850190-00708-02 Rev. A 9engine & Airframe systemsFlightInstruments EASNav/Com/XPDR/Audio AFCS GPS NavFlightPlanning ProceduresHazardAvoidanceAdditionalFeaturesAbnormalOperationAnnun/Alerts Appendix IndexStatus of the fuel selector is indicated between the fuel tank symbols. The mode,automatic (AUTO), manual (MAN), or off (no indication; CAS message ‘FUEL OFF’generated) is shown beneath the fuel selector symbol.Left FuelTankSelectedSwitchingFuel TankSelectionRightFuel TankSelectedUnknownFuel TankSelectionFuel Selector StatusIf 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 theboost pump is off, the symbol is shown in light blue (automatic mode) or red (manualmode).generAl sYstems1) 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 (CASmessages also generated). Statuses of propeller, stall sensor heater, pitot probe, andwindshield heat are also indicated on the diagram:• White indicates that heat is off (propeller and windshield)• Light blue indicates heat has been selected (windshield)• Green indicates heat is on• Yellow indicates heat has failed (propeller, pitot tube, and stall sensor).
