Garmin G1000 Checkout Procedure page 101

Post installation checkout procedure hawker / beechcraft king air c90
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8. Simulate a Localizer/Glideslope signal. Tune this signal on NAV 1 and NAV 2 receiver. Set the
PFD1 HSI to LOC1 and PFD2 HSI to LOC2 by pressing CDI softkey until LOC1 and LOC2 is
selected. Use the test equipment to center the deviation bars (localizer and glideslope) on PFD1 and
PFD2.
9. Press the APR key on the AFCS mode controller. Verify that the LOC and GS annunciations are
green on PFD1 and PFD2. Apply right/left and up/down localizer/glideslope signals using the test
equipment. Verify that the Flight Director and flight controls respond appropriately.
10. Couple FD to PFD1 by pressing the XFR button on the AFCS mode controller. Verify FD is coupled to
PFD1 as indicate by a left pointing arrow on the AFCS mode controller next to the XFR button.
11. Repeat step 10 using while coupled to PFD2.
G1000/GFC 700 Post Installation Checkout Procedure – Hawker / Beechcraft King Air C90
190-00682-00
Page 7-5
Revision 5

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