G1000/GFC 700 Post Installation Checkout Procedure – Hawker / Beechcraft King Air C90
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Revision 5
3. Return PFD1 and MFD to normal mode by pressing the red “
DISPLAY BACKUP
” button on the
GMA1. Return PFD1 to normal mode by cycling power.
3.13.3
Static Port Vertical Speed (Rate of Climb) Test
1. Command ADTS to change the altitude at the rates shown in the table below.
2. Wait for ADTS to report that target rates have been achieved.
3. Verify that the Rate of Climb reported by the Vertical Speed field on PFD1 and PFD2 are within
the tolerances specified in the table below:
Vertical Speed, feet/minute
Allowed tolerance, ±feet/minute
2000 100
1000 50
500 45
200 45
0
N/A (No VS Display)
-200 45
-500 45
-1000 50
-2000 100
3.13.4
OAT Probe Check
Ensure on-side sensors for PFD1 and PFD2. Verify that the outside air temperature (OAT) measurement
shown on PFD1 and PFD2 indicates ambient temperature.
