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Garmin G1000:Socata User Manual

Garmin G1000:Socata
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190-00709-00 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
1-17
SYSTEM OVERVIEW
Figure 1-10 Reversionary Mode (Manual)
Reversionary mode is activated by pressing the dedicated
DISPLAY BACKUP
button at the bottom of the
audio panel (see Figure 1-11 and refer to the Audio Panel section for further details). Pressing this button again
deactivates reversionary mode.
Figure 1-11 DISPLAY BACKUP Button
Pressing the D I S P L AY
BACKUP button activates/
deactivates reversionary
mode for both the on-side
PFD and the MFD.
Each display can be configured to operate in reversionary mode, as follows:
PFD1
– By pressing the
DISPLAY BACKUP
button on the left audio panel.
MFD
– By pressing the
DISPLAY BACKUP
button on the left or the right audio panel.
PFD2
– By pressing the
DISPLAY BACKUP
button on the right audio panel.
Should the connection between a PFD and the on-side GIA 63W become inoperative, the on-side GIA 63W
can no longer communicate with the remaining PFD (refer to Figure 1-
1). As a result, the NAV and COM
functions provided to the failed PFD by the on-side GIA 63W are flagged as invalid (red “x”) on the remaining
PFD (see Figure 1-12).
Figure 1-12 Inoperative Input (NAV1 Shown)
AHRS OPERATION
NOTE: Refer to the Appendices for specific AHRS alert information.
NOTE: Aggressive maneuvering in any of the three reversionary modes listed in Table 1-1 can degrade AHRS
accuracy.

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Garmin G1000:Socata Specifications

General IconGeneral
Display TypeLCD
Operating Temperature-20°C to +55°C
ManufacturerGarmin
TypeIntegrated Avionics System
Resolution1024 x 768 pixels
Display UnitsPrimary Flight Display (PFD) and Multi-Function Display (MFD)
CertificationFAA TSO certified
InterfacesARINC 429, RS-232
Screen Size10.4 inches

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