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• System failure• Invalid sensor data• Yaw damper failure while both are engaged• Stall warning (YD also disengages)• Inability to compute default flight director modes (FD also disengages automatically)
Yaw damper disengagement is indicated by a five-second flashing yellow ‘YD’ annunciation. Automatic yaw damper disengagement occurs when autopilot disengagement is caused by failure in a parameter also affecting the yaw damper. This means the yaw damper can remain operational in some cases where the autopilot automatically disengages. A localized failure in the yaw damper system or invalid sensor data also cause yaw damper disengagement.
Figure 7-35 Automatic Autopilot and Yaw Damper Disengagement
398 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
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AUDIO PANEL EICAS INSTRUMENTS
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INDEX APPENDICES FEATURES
7.6 Example Flight Plan Noteote: The following example flight plan and diagrams (not to be used for navigation) in this section are for instructional purposes only and should be considered not current. Numbered portions of accompanying diagrams correspond to numbered procedure steps.
This scenario-based set of procedures (based on the example flight plan found in the Flight Management Section) shows various GFC 700 AFCS modes used during a flight. In this scenario, the aircraft departs Charles B. Wheeler Downtown Airport (KMKC), enroute to Colorado Springs Airport (KCOS). After departure, the aircraft climbs to 12,000 ft and airway V4 is intercepted, following ATC vectors.
Airway V4 is flown to Salina VOR (SLN) using VOR navigation, then airway V244 is flown using a GPS Navigation. The ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach is executed.
Figure 7-36 Flight Plan Overview0369121518212427303303691215182124273033SalinaVOR(SLN)KMKCLamarVOR(LAA)03691215182124273033HaysVOR(HYS)KCOSV 244V 4V 24403691215182124273033TopekaVOR(TOP)
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 399
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Departureeparture
Climbing to the Selected Altitude and flying an assigned heading:
1) Before takeoff:
a) Use the ALT SEL Knob to set the Selected Altitude to 12,000 feet.
b) Push the GA Switch to activate Takeoff Mode. The flight director Command Bars establish a pitch up attitude to follow.
c) Press the AP Key to engage the autopilot in a climb, holding the pitch angle commanded in Takeoff Mode and wings level.
2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Flight Level Change Mode may be used).
a) Press the VS Key to activate Vertical Speed and Roll Hold modes and arm Selected Altitude Capture Mode.
The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP/DN Wheel or pushing the CWS Button while hand-flying the aircraft to establish a new Vertical Speed Reference.
3) Use the HDG Knob to set the Selected Heading, complying with ATC vectors to intercept Airway V4.
Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb. The autopilot follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading.
4) 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.
At 50 feet from the Selected Altitude, the green ‘ALT’ annunciation flashes for up to 10 seconds; the autopilot transitions to Altitude Hold Mode and levels the aircraft.
400 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
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AUDIO PANEL EICAS INSTRUMENTS
& CNS
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ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Figure 7-37 DepartureSelected Altitude of 12,000 MSL1234HDG ModeVS ModeALT ModeTO ModeTO ModeKMKC
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 401
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INSTRUMENTS EICAS AUDIO PANEL
& CNS
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MANAGEMENT
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AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
　
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