Garmin Software Version 0500.00 User's Guide Page 59

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-19
Go-Around / Missed Approach
1. When the decision is made to execute a missed
approach, apply full power and press the
GA
button. The autopilot will disconnect and the
flight director command bars will establish
a 7 degree nose-up climb. Note when the
autopilot disconnects the AP’ annunciation
flashes yellow for five seconds. Manually fly
the aircraft to the command bars.
2. Following the published Missed Approach
Procedure, climb to the prescribed altitude.
Press the
AP
key, re-engaging the autopilot.
To have the autopilot fly to the hold point, set
the CDI to GPS by pressing the
CDI
softkey,
then press the
NAV
key. The autopilot flies
direct to Clovis VORTAC according to the
loaded approach while maintaining the current
attitude.
3. During the climb, set a desired hold altitude
in the Selected Altitude box by turning the
ALT
knob. The
CWS
button may be used to
manually set a new pitch attitude. Doing this
causes the autopilot to revert to the default
Pitch Hold (PIT) mode and Altitude Hold is
armed. When the selected altitude is reached,
Altitude Hold mode will become active and the
autopilot will maintain the selected altitude.
4. Upon reaching the holding pattern, set the
Selected Heading to 307 degrees using the
HDG
knob and press the
HDG
key. The
HDG
knob is used for the remainder of the hold to
guide the aircraft.
0
3
6
9
12
15
18
21
24
27
30
3
3
1.
2.
3.
GA Mode
4.
HDG Mode
GPS Mode
KFAT
CZQ
307
Figure 6-27 Go Around / Missed Approach
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