Garmin G1000 Guide

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900
190-00709-05 Rev. D
104
ENGINE & AIRFRAME SYSTEMS
Battery and essential bus voltages are displayed using gauges. DC buses are shown in green when energized.
When not energized, the connection line to the main bus is removed and the bus label is displayed in red.
Figure 3-25 Battery and Essential Bus Low Voltage
Figure 3-26 DC Bus Status
Bus Not Energized
The Emergency Buses switch has two positions, UP (open) and DN (ground). If the switch is in the UP
position, the essential bus is connected to the battery bus. If the switch is in the DN position, the essential bus
is connected to the main bus.
Figure 3-27 Essential Bus Connections
Essential Bus Connected
to the Battery Bus
Essential Bus Connected
to the Main Bus
A red “X” over a component indicates invalid data or a failed unit.

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)