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LMM for the Kodiak 100
190-02102-00 Rev.4
Figure 7-10. Configured Confirmation Box
h) Once verification is complete, the CURRENT CORRECTED VALUE should
be zero, within a range of fluctuation that is equal to or less than noted before
calibration. If this is the case the calibration has been successfully completed.
7.7 GDC 72 Air Data Computer
After software and configuration have been loaded to a replacement GDC, test per the
procedures in the OEM approved Aircraft Maintenance Manual.
NOTE
The GDC will not provide valid outputs until the aircraft post installation cal-
ibration procedures are completed.
7.8 GDL 69A SXM Testing
NOTE
The use of an external power cart is optional in order to prevent the aircraft
battery from discharging to a critically low level.
1. Move the aircraft outside and ensure there is an unobstructed view of the
southern sky.
2. Attach a ground power cart to the external power connector on the aircraft and
apply power.
3. Power on all systems and allow two to four minutes for initialization.
4. Make sure the displays and the audio processor are connected and operating
properly.
5. Make sure the circuit breaker for the GDL 69A SXM is closed.
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