General Systems - Garmin SOCATA TBM850 Cockpit Reference Manual

Status 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 Fuel
Selected
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).

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
messages also generated). Statuses of propeller, stall sensor heater, pitot probe, and
windshield 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).
190-00708-02 Rev. A
Switching
Tank Fuel Tank
Selection
Fuel Selector Status
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
engine & Airframe systems
Right Unknown
Fuel Tank Fuel Tank
Selected Selection
9