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Page 8-4
LMM for the Kodiak 100
190-02102-00 Rev.4
Figure 8-1. GFC Status Page
NOTE
The displayed test results on the PFD are not stored in G1000NXi memory.
If power is cycled, these values will be lost. However, these test values are
not lost by changing configuration mode pages.
NOTE
Perform the following test at temperatures between 50° F and 120° F
1. Use the FMS knob to select the desired servo.
2. Verify the PFT status field shows PASSED.
3. Verify the aircraft control surface to be checked is free to travel throughout its
range of motion.
4. Press the ENG CLCH softkey on the PFD.
5. With the clutch engaged, take hold of the aircraft controls and manually
overcome the clutch. Move the control surface to be tested from stop to stop a
minimum of two times each direction.
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Summary of Contents for Cessna Caravan G1000
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