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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