Garmin Software Version 0719.00 Guide de l'utilisateur Page 51

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-00 Rev. A
3-5
SECTION 3 – ENGINE &
AIRFRAME SYSTEMS
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
Tank
Selected
Switching
Fuel Tank
Selection
Right
Fuel Tank
Selected
Unknown
Fuel Tank
Selection
Table 3-2 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 used and remaining are based on the fuel flow.
The aircraft’s gross weight (GW) is entered on the AUX
- Weight Planning Page (see the Flight Planning Section).
A red “X” over a component indicates invalid data or
a failed unit.
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