Garmin G1000 Nxi System Maintenance Manual page 169

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System Failure Troubleshooting
The following table provides basic troubleshooting guidance for LRU failures. Refer to G1000
Wiring Diagram, listed in Table 1-1, as needed to verify interconnects.
Invalid Data Field
Low Speed Awareness Band
permanently displayed
Low Speed Awareness Band
permanently inhibited
NAV1 & COM1
G1000 NXi System Maintenance Manual
King Air 300 Series
190-00716-N1
Associated
LRU(s)
With aircraft weight on wheels and the G1000 in
Configuration Mode, check that the RH GEAR ON GROUND
Discrete In indication for GIA2, on GIA I/O CONFIGURATION
page is illuminated.
With aircraft weight on wheels and the G1000 in
Configuration Mode, check that the LH GEAR ON GROUND
Discrete In indication for GIA1, on GIA I/O CONFIGURATION
GDU
page is illuminated.
If both indications are illuminated Green, switch GIA1 and
GIA2, to verify location of problem:
If problem is resolved, replace faulty unit.
If indication is not illuminated, check for wiring faults
between the GIAs and aircraft squat switch system.
With aircraft weight on wheels and the G1000 in
Configuration Mode, check that the RH GEAR ON GROUND
Discrete In indication for GIA2, on GIA I/O CONFIGURATION
page is illuminated.
With aircraft weight on wheels and the G1000 in
Configuration Mode, check that the LH GEAR ON GROUND
Discrete In indication for GIA1, on GIA I/O CONFIGURATION
GDU
page is illuminated.
If both indications are illuminated Green, switch GIA1 and
GIA2, to verify location of problem:
If problem is resolved, replace faulty unit.
If indication is not illuminated, check for wiring faults
between the GIAs and aircraft squat switch system.
Check configuration settings for GIA1 and PFD1.
Swap GIA1 and GIA2, to verify location of problem:
GIA1
If problem follows GIA1, replace GIA1.
Check Ethernet interconnect from GIA1 to PFD1.
If problem persists, replace PFD.
Solution
Page 156
Revision 1

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