Garmin G1000 Guide

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900
190-00709-05 Rev. D
92
ENGINE & AIRFRAME SYSTEMS
In the event of a display failure, depending on the failed display(s), the functioning display(s) may be re-
configured to present Primary Flight Display (PFD) symbology together with engine and CAS information
(refer to the System Overview for more information about Reversionary Mode). In Reversionary Mode, engine,
pressurization, fuel, electrical, and trim data is presented in an abbreviated format on the left of the display.
CAS messages appear in a window on the right of the display. Synoptics are not available while in Reversionary
Mode.
EIS
Display
CAS
Window
Figure 3-2 Reversionary Mode

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)