Cirrus SR2x

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AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW FLIGHT INSTRUMENTS After manual disengagement, the autopilot disconnect aural alert and the flashing ‘AP’ annunciation may be cancelled by pushing the AP DISC Button. Automatic autopilot disengagement is indicated by a flashing red and white ‘AP’ annunciation and by the autopilot disconnect aural alert, which continue until acknowledged by pushing the AP DISC Button. Automatic autopilot disengagement occurs due to: • System failure • Invalid sensor data • Inability to compute default flight director modes (FD also disengages automatically) EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES 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 may also cause yaw damper disengagement. REVERSIONARY MODE Figure 7-30 Automatic Autopilot and Yaw Damper Disengagement In the event of a PFD failure, the MFD goes into reversionary mode. The autopilot remains engaged but reverts to pitch hold and roll hold modes; all other modes are available for selection. If the MFD fails, the PFD goes into reversionary mode and the autopilot continues to function. EXAMPLE FLIGHT PLAN NOTE: 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 GPS Navigation. The ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach is executed. INDEX 526 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 190-00820-11 Rev. A
21 15 12 AUTOMATIC FLIGHT CONTROL SYSTEM 33 0 3 30 33 0 3 30 33 0 3 6 KMKC SYSTEM OVERVIEW KCOS 27 24 30 33 0 Lamar VOR (LAA) 3 6 9 V 244 27 24 30 21 18 Hays VOR (HYS) 15 12 6 9 V 244 27 24 21 18 Salina VOR (SLN) 15 12 6 9 V 4 27 24 21 18 Topeka VOR (TOP) 15 12 9 FLIGHT INSTRUMENTS 18 Figure 7-31 Flight Plan Overview EIS DEPARTURE 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. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-11 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 527
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® Cirrus SR2x Integrated Avionics
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SYSTEM OVERVIEW SYSTEM OVERVIEW FLI
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APPENDIX A SYSTEM OVERVIEW FLIGHT I
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INDEX SYSTEM OVERVIEW FLIGHT INSTRU
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INDEX SYSTEM OVERVIEW FLIGHT INSTRU
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INDEX AUDIO PANEL & CNS EIS FLIGHT
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