Cirrus SR2x

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AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT DIRECTOR MODES Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise specified, all mode keys are alternate action (i.e., press on, press off). In the absence of specific mode selection, the flight director reverts to the default pitch and/or roll modes. Armed modes are annunciated in white and active in green in the AFCS Status Box. Under normal operation, when the control for the active flight director mode is pressed, the flight director reverts to the default mode(s) for the axis(es). Automatic transition from armed to active mode is indicated by the white armed mode annunciation moving to the green active mode field and flashing for 10 seconds. If the information required to compute a flight director mode becomes invalid or unavailable, the flight director automatically reverts to the default mode for that axis. A flashing yellow mode annunciation and annunciator light indicate loss of sensor (ADC) or navigation data (VOR, LOC, GPS, VNV, SBAS) required to compute commands. When such a loss occurs, the system automatically begins to roll the wings level (enters Roll Hold Mode) or maintain the pitch angle (enters Pitch Hold Mode), depending on the affected axis. The flashing annunciation stops when the affected mode key is pressed or another mode for the axis is selected. If after 10 seconds no action is taken, the flashing annunciation stops. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Figure 7-3 Loss of VOR Signal The flight director is automatically disabled if the attitude information required to compute the default flight director modes becomes invalid or unavailable. COMMAND BARS Upon activation of the flight director, Command Bars are displayed in magenta on the PFD. If the aircraft is being flown by hand, the command bars are displayed hollow (Figure 7-4). The Command Bars do not override the Aircraft Symbol. The Command Bars move together vertically to indicate pitch commands and bank left or right to indicate roll commands. Command Bars (Autopilot Engaged) Command Bars Command Bars (Pilot Hand Flying Aircraft) ADDITIONAL FEATURES Aircraft Symbol Figure 7-4 Command Bars APPENDICES If the attitude information being sent to the flight director becomes invalid or unavailable, the Command Bars are removed from the display. INDEX 502 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 190-00820-11 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM VERTICAL MODES Table 7-2 lists the vertical modes with their corresponding controls and annunciations. The mode reference is displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Indicated Airspeed modes. The NOSE UP/DN Wheel can be used to change the vertical mode reference while operating under Pitch Hold, Vertical Speed, Indicated Airspeed, or Altitude Hold modes. Increments of change and acceptable ranges of values for each of these references using the NOSE UP/DN Wheel are also listed in the table. Pitch Hold Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude; may be used to climb/ descend to the Selected Altitude (default) Selected Altitude Capture Captures the Selected Altitude * ALTS Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn ft Vertical Speed Indicated Airspeed (IAS) Vertical Path Tracking (If equipped) VNV Target Altitude Capture Glidepath Glideslope Takeoff Go Around Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude Maintains the current aircraft airspeed in IAS while the aircraft is climbing/descending to the Selected Altitude Captures and tracks descent legs of an active vertical profile Captures the Vertical Navigation (VNV) Target Altitude Captures and tracks the SBAS glidepath on approach Captures and tracks the ILS glideslope on approach Commands a constant pitch angle and wings level on ground in preparation for takeoff Commands a constant pitch angle and wings level in the air PIT VS Key VS nnnn fpm IAS Key IAS nnn kt VNV Key VPTH ** ALTV APR Key GA Button GP GS Reference Range -15° to +20° Reference Change Increment 0.5° ± 150 ft 10 ft -3000 to +1500 fpm 80 to 185 kt TO 7° GA 7° 100 fpm * ALTS armed automatically when PIT, VS, IAS, or GA active, and under VPTH when Selected Altitude is to be captured instead of VNV Target Altitude ** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of Selected Altitude Table 7-2 Flight Director Vertical Modes 1 kt SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS 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 503
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® Cirrus SR2x Integrated Avionics
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Copyright © 2008-2015 Garmin Ltd.
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WARNINGS, CAUTIONS, AND NOTES WARNI
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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 AUDIO PANEL & CNS EIS FLIGHT
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