5 system operation, Normal display operation, Reversionary display operation – Garmin G1000 Mooney M20TN User Manual

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190-00647-00 Rev. A

Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN

1-9

SYSTEM OVERVIEW

1.5 SYSTEM OPERATION

The displays are connected together via a single Ethernet bus for high-speed communication. As shown in

Figure 1-1, each IAU is connected to the on-side display. Normal and reversionary G1000 display operation, as
well as the various AHRS modes and G1000 System Annunciations are discussed here.

NORMAL DISPLAY OPERATION

In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed,

altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section
for more information). The MFD normally displays a full-color moving map with navigation information (see
the GPS Navigation Section), while the left portion of the MFD is dedicated to the Engine Indication System
(EIS; see the EIS Section). Both displays offer control for COM and NAV frequency selection.

Figure 1-6 G1000 Normal Operation

REVERSIONARY DISPLAY OPERATION

NOTE:

The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Refer to Appendix A

for further information regarding system-specific alerts.

NOTE:

In normal operating mode, backlighting can only be adjusted from the PFD. In Reversionary Mode, it

can be adjusted from the remaining display.

In the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In

Reversionary Mode, all important flight information is presented on the remaining display in the same format
as in normal operating mode.

If a display fails, the appropriate IAU-display Ethernet interface is cut off. Thus, the IAU can no longer

communicate with the remaining display (refer to Figure 1-1), and the NAV and COM functions provided to
the failed display by the IAU are flagged as invalid on the remaining display. The system reverts to backup
paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is
completely automated for all LRUs and no pilot action is required.

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