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Cirrus SR2x

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ADDITIONAL FEATURES<br />

SYSTEM<br />

OVERVIEW<br />

Once engaged, ESP force will be applied between 30° and 75°, as illustrated in Figure 8-131. The force<br />

increases as roll attitude increases and decreases as roll attitude decreases. The applied force is intended to<br />

encourage pilot input that returns the airplane to a more normal roll attitude. As roll attitude decreases, ESP <br />

will disengage at 30°.<br />

FLIGHT<br />

INSTRUMENTS<br />

30º<br />

20º<br />

10º<br />

0º<br />

10º<br />

20º<br />

30º<br />

45º<br />

45º<br />

AUDIO PANEL<br />

& CNS<br />

ADDITIONAL<br />

FEATURES<br />

FLIGHT<br />

MANAGEMENT<br />

AFCS<br />

EIS<br />

60º<br />

60º<br />

75º<br />

75º<br />

HAZARD<br />

AVOIDANCE<br />

90º<br />

Figure 8-131 ESP Roll Operating Range When Engaged<br />

(Force Increases as Roll Increases & Decreases as Roll Decreases)<br />

ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75°<br />

(Figure 8-132).<br />

ESP Upper Disengage Limit (75°)<br />

Aircraft Roll Attitude = 74°<br />

90º<br />

APPENDICES<br />

INDEX<br />

PITCH ENGAGEMENT<br />

Figure 8-132 Roll Attitude Autopilot Engagement Limit (ESP Engaged)<br />

ESP engages at 17.5° nose-up and 15.5° nose-down. Once ESP is engaged, it will apply opposing force<br />

between 17.5° and 50° nose-up and between 15.5° and 50° nose-down, as indicated in Figure 8-133. Maximum<br />

opposing force is applied between 22.5° and 50° nose-up and between 20.5° and 50° nose-down.<br />

656<br />

Pilot’s Guide for the <strong>Cirrus</strong> <strong>SR2x</strong> with <strong>Cirrus</strong> Perspective by Garmin<br />

190-00820-11 Rev. A

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