Fuel system, Engine & airframe systems – Garmin G1000 Socata TBM 850 User Manual
Page 106
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Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. A
94
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
FUEL SYSTEM
The Fuel Synoptics Page displays the status of the fuel tanks and feed system. Fuel quantity is depicted
graphically; the color changes to yellow if the fuel quantity drops below the threshold level.
Figure 3-23 Fuel Synoptics Page
1
Left Fuel Tank
2
Left Fuel Line
3
Fuel Pressure
4
Engine Driven Boost Pump
5
Auxiliary Boost Pump
6
Fuel Selector
7
Right Fuel Tank
8
Right Fuel Line
9
Fuel Flow Data
5
4
8
7
1
2
3
6
9
Fuel Pressure is displayed using a gauge. If fuel pressure is low the readout is displayed in red.
Figure 3-24 Fuel Pressure Low
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