Garmin Legacy Software Versions Guía de usuario Pagina 75

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190-00498-00 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III
2-45
PRIMARY FLIGHT DISPLAY
2.7 REVERSIONARY MODE
NOTE: Refer to the System Overview for a
detailed description of Reversionary mode.
The PFD is designed to enter reversionary (backup)
mode based on automatic fault monitoring and detection,
internal switching. Reversionary mode can also be
activated manually by pressing the dedicated DISPLAY
BACKUP button at the bottom of the Audio Panel (refer
to the Audio Panel section).
Figure 2-73 PFD Reversionary Mode
In reversionary mode, the computer display units
(CDUs) are re-configured to present the PFD symbology
together with the engine parameters (engine parameters are
incorporated on the left side of the display). Reversionary
PFD parameters are presented in the same format as prior
to re-configuration. In the event of a display failure, the
pilot loses one NAV, one COM, and GPS:
PFD failure – NAV1, COM1 and GPS1 are lost
MFD failure – NAV2, COM2 and GPS2 are lost
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