Garmin G1000 Socata TBM 850 - Manual (Page 111)

190-00709-02 Rev. B Garmin G1000 Pilot’s Guide for the Socata TBM 850 97
ENGINE & AIRFRAME SYSTEMS
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
Status of the fuel selector is indicated between the fuel tank symbols. The mode, automatic (AUTO) or
manual (MAN) is shown beneath the fuel selector symbol.
Left Fuel Tank
Selected
Switching Fuel
Tank Selection
Right Fuel Tank
Selected
Unknown Fuel
Tank Selection
Fuel Selector
Off
Table 3-1 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)
Table 3-2 Auxiliary Boost Pump Status
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 Management Section).
Figure 3-25 Fuel Flow Data
A red “X” over a component indicated invalid data or a failed unit.