Page 3-4 GIA 63/GIA 63W Installation Manual
Revision S 190-00303-05
3.7 Post Installation Configuration & Checkout
All configuration and checkout procedures take place upon completion of the installation of the Garmin
Integrated Flight Deck. The GDU serves as the graphics user interface to the installer configuring the
system. For sample configuration and checkout procedures, refer to the G1000 Line Maintenance and
Configuration Manual, Garmin part number 190-00303-04. Always use aircraft manufacturer approved
checkout documents when performing actual checkout.
3.8 Continued Airworthiness
Maintenance of the GIA 63(W) is “on condition” for all units installed in airframes that require power
interrupt Category B (50mS). For airframes that require the GIA 63(W) to comply with RTCA/DO-160D
power interrupt Category A (200mS), one of the following two actions must be taken to ensure backup
time is adequate:
• Comply with the applicable GIA 63(W) Mod Status (refer to Table 3-3).
Table 3-3. Long Term Power Interrupt Category A (200 mS) Mod Status
Unit Unit Part Number
Long Term
Power Interrupt
Category A (200 mS)
Mod Status
GIA 63 011-00781-00 4
GIA 63 011-00781-01 1
GIA 63W 011-01105-00 1
GIA 63W 011-01105-01 0
GIA 63W 011-01105-20 0
Or
• Perform the power interrupt annual inspection as described in Section 3.8.1.
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