Garmin G1000 Checkout Procedure page 38

Post installation checkout procedure hawker / beechcraft king air c90
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19. Close ADC1 PRI CB. Verify ADC1 is powered by observing valid ADC1 air data information. Close
ADC1 SEC CB.
20. Open ADC2 CB. Verify ADC2 is not powered by observing red Xs are displayed for ADC2 air data
information.
21. Close ADC2 CB. Verify ADC2 is powered by observing valid ADC2 air data information
22. Open MFD CB. Verify MFD is not powered.
23. Close MFD CB. Verify MFD is powered.
24. Open COMM NO 1 CB. Verified COMM 1 is not powered by observing a red X is displayed in COMM
1 tuning window.
25. Close COMM NO 1 CB. Verify COMM1 is powered by observing a valid frequency in the COMM1
tuning window.
26. Open COMM No. 2 CB. Verified COMM2 is not powered by observing a red X is displayed in COMM
2 tuning window.
27. Close COMM No. 2 CB. Verify COMM2 is powered by observing a valid frequency in the COMM2
tuning window.
28. Open MODE CTL CB. Verify GMC 710 AFCS mode controller is not powered. Close AFCS CTL CB
when finished.
29. Open AFCS SERVOS CB. Verify AFCS servos are not powered by observing momentary Red/white
AFCS
annunciation.
30. Close AFCS SERVOS CB. Verify AFCS servos are powered by observing that the Red/white
annunciation extinguishes.
31. Open DATA LINK CB. Verify GDL 69 is not powered by observing related alert messages.
32. Close DATA LINK CB. Verify GDL 69 is powered.
33. Open FMS CTL CB. Verify the FMS controller is not powered.
34. Close FMS CTL. Verify the FMS controller is powered.
35. Verify STBY Battery power is OFF.
36. Open STBY ATT CB. Verify the standby attitude indicator is not powered.
37. Close STBY ATT CB. Verify the standby attitude indicator is powered.
38. Open STBY ALTM CB. Verify the standby altimeter vibrator is not powered.
39. Close STBY ALTM CB. Verify the standby altimeter vibrator is powered.
40. Open AUDIO 1 CB. Verify GMA1 is not powered.
41. Close AUDIO 1 CB. Verify GMA1 is powered.
42. Open AUDIO 2 CB. Verify GMA2 is not powered.
Page 3-2
G1000/GFC 700 Post Installation Checkout Procedure - Hawker / Beechcraft King Air C90
Revision 5
AFCS
190-00682-00

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