Garmin G1000 Checkout Procedure page 36

Post installation checkout procedure hawker / beechcraft king air c90
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2.17.1
System Communication Hierarchy
The following criteria must be satisfied to be able to perform the desired operation:
Desired Operation
Load Software to MFD or PFD Displays
Load AIRFRAME, SYSTEM, MFD1, PFD1, PFD2
and MANIFEST configuration files to MFD and
PFDs
Load Software/Configuration files to GIA 63Ws
Load Software/Configuration files to:
- GMA 1347D
- GDC 74B
- GEA 71
- GRS 77 (software only)
- GMU 44 (software only)
- GTX 33
Page 2-22
G1000/GFC 700 Post Installation Checkout Procedure - Hawker / Beechcraft King Air C90
Revision 5
Criteria for Success
G1000/C90 SW Loader Card must be inserted
in top slot for each display to be loaded.
CLR & ENT keys must be held during power
up of display.
Power on only one display at a time during
software loading.
G1000/C90 SW Loader Card must be inserted
in top slot of PFD1.
PFD1 and MFD must be powered on.
PFD1 and MFD must have correct software.
G1000/C90 SW Loader Card must be inserted
in top slot of PFD1.
G1000 system must be powered on.
PFD and MFD must have correct software.
PFD1 and MFD must be successfully
configured with AIRFRAME, SYSTEM,
MANIFEST, MFD1, PFD1 and PFD2
configuration files.
G1000/C90 SW Loader Card must be inserted
into PFD1 top slot.
G1000 must be powered on.
PFD1 and MFD must have correct software
and configuration settings.
GIA 63Ws must have correct software.
GIA 63Ws must be successfully configured
with GIA1 and GIA2 configuration files.
Data path from GIA1 to each LRU must be
operational.
190-00682-00

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