Garmin Software Version 0321.23 Manual Pagina 225

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G1000 System Maintenance Manual – Diamond DA40/40F Page 7-17
190-00545-01 Revision G
7.4.2 GEA 71 Testing
Apply power to the G1000 and allow system to initialize.
On the PFD, open the ALERT window and verify there are no GEA MANIFEST or configuration error
messages.
On the MFD, check the indication for each of the sensor or monitor inputs with the aircraft engine off.
In general, verify all engine and system instruments show valid and reasonably true data, with no red Xs
or erratic indications.
Full Page Engine Instrument Check:
1. Observe the EIS strip on the MFD and check each display gauge value against.
2. Press the ENGINE softkey and observe the full-page EIS display. Check each display gauge
value against Table 7-1.
Figure 7-9. Engine Instrument Pages
3. Press the RED reversionary mode button on the GMA 1347 audio panel.
4. Press the ENGINE softkey, and then press the LEAN softkey and verify that the display
gauges change to show EGT and CHT bar indicators as shown below. Verify information
agrees with the conditions of Table 7-1.
5. Press the SYSTEM softkey and verify that the display changes to show the digital equivalent
of the normal EIS page (oil temp, oil pressure, etc), as shown below. Verify the information
presented agrees with the conditions of Table 7-1.
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