Garmin G1000 Pilot's Manual page 59

Beechcraft a36/g36 integrated flight deck
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The following annunciations appear in yellow on the HSI to indicate abnormal GPS conditions:
• 'INTEG': Loss of Integrity–GPS integrity is insufficient for the current phase of flight
• 'WARN': GPS position error
A
UTOMATIC
On the AUX - System Setup Page, 'ILS CDI Capture' may be changed to 'Manual'. In 'Auto' (default)
setting, the system automatically switches from GPS to LOC navigation source and changes the CDI scaling
accordingly when:
• A localizer or ILS approach has been loaded into the active flight plan
• The final approach fix (FAF) is the active leg, the FAF is less than 15 nm away, and the aircraft is moving
toward the FAF
• A valid localizer frequency has been tuned
• The GPS CDI deviation is less than 1.2 times full-scale deflection
GPS steering guidance is still provided after the HSI automatically switches to LOC until LOC capture, up
to the Final Approach Fix (FAF) for an ILS approach, or until GPS information becomes invalid. Activating
Vector-to-Final (see the GPS Navigation Section) also causes the HSI to switch to LOC navigation source,
although the change is not considered automatic to the system and GPS steering guidance is not provided
after this switch.
Changing the ILS CDI Capture setting:
1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the 'ILS CDI Capture' field in the 'GPS CDI' Box (Figure 2-21).
4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key.
190-00595-00 Rev. A
N
S
S
AVIGATION
OURCE
WITCHING
Figure 2-21 System Setup Page,
Garmin G1000 Pilot's Guide for the Beechcraft A36/G36
ILS CDI Capture Setting
FLIGHT INSTRUMENTS
2-13

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