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Cirrus SR2x

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AUTOMATIC FLIGHT CONTROL SYSTEM<br />

Roll Axis<br />

The autopilot roll axis uses roll rate to stabilize aircraft roll attitude during flight director maneuvers. The<br />

flight director roll commands are rate- and attitude-limited, combined with roll damper control, and sent<br />

to the roll servo motor.<br />

Yaw Axis<br />

The yaw damper uses yaw rate and roll attitude to dampen the aircraft’s natural Dutch roll response. It<br />

also uses lateral acceleration to coordinate turns and reduce or eliminate the need for the pilot to use rudder<br />

pedal force to maintain coordinated flight during climbs and descents.<br />

ENGAGEMENT<br />

When the AP Key is pressed, the autopilot, yaw damper, and flight director (if not already active) are<br />

activated. The flight director engages in Pitch and Roll Hold Modes when initially activated. When the YD<br />

Key is pressed, the system engages the yaw damper independently of the autopilot (if not already engaged).<br />

Autopilot and yaw damper status are displayed in the center of the AFCS Status Box. Engagement is indicated<br />

by green ‘AP’ and ‘YD’ annunciations, respectively.<br />

DISENGAGEMENT<br />

Autopilot<br />

Engaged<br />

Yaw Damper<br />

Engaged<br />

Figure 7-27 Autopilot and Yaw Damper Engaged<br />

NOTE: The autopilot does not disengage when the MET Switch is pressed.<br />

Pushing the AP Key on the AFCS Control Panel disengages the autopilot. Manual autopilot disengagement<br />

is indicated by a five-second flashing yellow ‘AP’ annunciation and a three-second autopilot disconnect aural<br />

alert.<br />

SYSTEM<br />

OVERVIEW<br />

FLIGHT<br />

INSTRUMENTS<br />

EIS<br />

AUDIO PANEL<br />

& CNS<br />

FLIGHT<br />

MANAGEMENT<br />

HAZARD<br />

AVOIDANCE<br />

AFCS<br />

Figure 7-28 Manual Autopilot Disengagement<br />

Pushing the AP DISC button disengages the autopilot, yaw damper, and flight director. Pushing the YD<br />

Key disengages the yaw damper and the autopilot. When the yaw damper and autopilot are manually<br />

disengaged, both the ‘AP’ and ‘YD’ annunciation turn yellow and flash for 5 seconds and a three-second<br />

autopilot disconnect aural alert is generated.<br />

Figure 7-29 Autopilot and Yaw Damper Disengagement<br />

ADDITIONAL<br />

FEATURES<br />

APPENDICES INDEX<br />

190-00820-11 Rev. A Pilot’s Guide for the <strong>Cirrus</strong> <strong>SR2x</strong> with <strong>Cirrus</strong> Perspective by Garmin 525

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