
Instructions for Continued Airworthiness G600, GNS 530W, GNS 430W, 190-01080-05 Rev. 2
GMA 347, GTX 330D, GMX 200, WSI AV-200 Cessna 208/208B Page 9 of 29
4. Start the GMA Configuration tool, GMA_CONFIG.EXE (Garmin P/N 006-A0115-00), on your
computer.
5. Power up the GMA 347.
Refer to the appropriate Modification Summary, Section 4, for further Configuration instructions.
2.3.4 GMX 200 and WSI AV-200
To enter configuration mode on the GMX 200, immediately after the self-test is complete press line select
keys 1, 4, and 6 in sequence before pressing any other keys (where 1 is the top line select key, 4 is the
fourth key down, and 6 is the lower most line select key).
Refer to the appropriate Modification Summary, Section 4, for further Configuration instructions.
2.3.5 GTX 330D
The #1 GTX330D receives power from Avionics Bus 1, and the #2 GTX330D receives power from
Avionics Bus 2.
The GTX 330D starts in normal mode when power is applied to the unit. To enter configuration mode
apply power to the GTX 330D while holding the FUNC key, then press the ON key to access the
configuration pages.
In order to perform maintenance tasks such as software updates and other diagnostic activities, a
Windows-compatible PC computer (preferably a laptop) is required. The maintenance port is located
below the instrument panel just immediately behind the throttle quadrant as shown in 190-01080-00,
Install Dwg 150, G600 GNS430W GMA347 Cessna 208/208B and 190-01080-01, Install Dwg 250, G600
GNS430W GMA347 Cessna 208/208B.
CAUTION:
The GNS 430W must be powered off prior to
programming transponders via the maintenance port.
Refer to the appropriate Modification Summary, Section 4, for further Configuration instructions.
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