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3) There are two options available at this point, as the autopilot flies the ILS approach:
• Push the AP DISC Switch at the decision height and land the aircraft. • Use the GA Switch to execute a missed approach.
HDG ModeLOC APR/GS ModePETEY123GPS NAV ModeKCOSPYNON
Figure 7-43 ILS Approach to KCOS
408 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Flying a RNAV GPS approach with vertical guidance:
1) Arm flight director modes for a RNAV GPS approach with vertical guidance:
a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source).
b) Select the Runway 35R LPV approach for KCOS. Load and activate the approach into the flight plan.
2) Press the APR Key once clearance for approach has been received. GPS Approach Mode is activated and Glidepath Mode is armed.
3) Once the glidepath is captured, Glidepath Mode becomes active. The flight director now provides guidance to the missed approach point.
4) There are two options available at this point, as the autopilot flies the approach:
• Push the AP DISC Switch at the decision height and land the aircraft. • Use the GA Switch to execute a missed approach.
4GPS APR/GP ModeFALUR123GPS NAV ModeKCOSHABUKPYNONCEGIX
Figur
e 7-44 LPV Approach to KCOS
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 409
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Go Around/Missed Approachpproachpproach Noteote: As a result of calculations performed by the system while flying the holding pattern, the display may re-size automatically and the aircraft may not precisely track the holding pattern as depicted on the PFD and MFD.
Flying a missed approach:
1) Push the GA Switch at the Decision height and apply go around power to execute a missed approach. The flight director Command Bars establish a nose-up climb to follow. If flying an ILS or LOC approach, the CDI also switches to GPS as the navigation source.
Note that when the GA Switch is pushed, the missed approach is activated and the autopilot disconnects, indicated by the ‘AP’ annunciation flashing yellow for 5 seconds.
Flashes 5 sec
2) Start the climb to the prescribed altitude in the published Missed Approach Procedure (in this case, 10,000 ft).
a) Press the AP Key to re-engage the autopilot.
b) Press the NAV Key to have the autopilot fly to the hold.
3) Use the ALT SEL Knob to set a Selected Altitude to hold.
To hold the current airspeed during the climb, press the FLC Key.
As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode, indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.
The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft.
4) The autopilot flies the holding pattern after the missed approach is activated. Annunciations are displayed in the Navigation Status Box, above the AFCS Status Box.
410 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Figure 7-45 Go Around/Missed Approach3412KCOSMOGALGA ModeGPS NAV Mode
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 411
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
7.7 AFCS Annunciationsnnunciations and Alerts
AFCS Statustatustatus Alerts
The annunciations in Table 7-6 (listed in order of increasing priority) can appear on the PFDs above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality.
Figure 7-46 AFCS Status AnnunciationAFCS Status Annunciation
Alert Condition
Annunciation
Description
Rudder Mistrim Right
Yaw servo providing sustained force in the indicated direction
　
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