Garmin G1000 Guide

190-00709-05 Rev. D
Garmin G1000 Pilot’s Guide for the Socata TBM 850/900
105
ENGINE & AIRFRAME SYSTEMS
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 3-28 Fuel Synoptics Page
1
Left Fuel Tank
2
Left Fuel Line
3
Fuel Pressure (if installed)
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 Display (if installed)
FUEL PRESSURE (IF INSTALLED)
Fuel Pressure is displayed using a gauge. If fuel pressure is low the readout is displayed in red.
Figure 3-29 Fuel Pressure Low

Garmin G1000 Specifications

General

Display Type	LCD
Primary Flight Display (PFD)	Yes
Multi-Function Display (MFD)	Yes
Terrain Awareness	Yes
Autopilot Integration	Yes
Integrated Flight Deck System	Yes
Weather Radar	Optional
Traffic Advisory System (TAS)	Optional
Terrain Awareness and Warning System (TAWS)	Yes
Resolution	1024 x 768 pixels
Weather Data	Yes
Navigation	Yes
AHRS	Yes
Air Data Computer (ADC)	Yes
Interfaces	ARINC 429, RS-232
Certification	TSO certified
Traffic Information	Optional (requires ADS-B or TCAS)