Cirrus SR2x

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ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 8.13 HYPOXIA RECOGNITION WITH AUTOMATIC DESCENT MODE The optional Hypoxia Recognition detects pilot incapacitation due to the affects of hypoxia or other physical conditions. This is accomplished by monitoring pilot interaction with the Perspective ® system. If the system determines the pilot is not responding, Automatic Descent Mode is activated placing the aircraft in a descent to a lower altitude to provide the pilot and passengers an opportunity to recover from the effects of hypoxia. The system is operative when the aircraft altitude is above 14,900 feet (pressure altitude) and the Garmin AFCS autopilot is engaged. Pilot interaction with the Perspective ® system is monitored by detecting key presses and turns of the knobs (Audio Panel and push-to-talk switch excluded). If a period of inactivity (time dependent on altitude, see Figure 8-128) is detected, Hypoxia Recognition initiates an automatic descent. Upon activation, there are three sequential phases employed by the system; determining pilot alertness, descent to 14,000 feet MSL, and descent to 12,500 feet MSL. DETERMINING PILOT ALERTNESS When the system detects a sufficient period of inactivity (Figure 8-128) the Advisory Annunciation ‘ARE YOU ALERT?’ is displayed. Selecting the ALERT Softkey will acknowledge the message and reset the system. Pressing any other softkey, or turning a knob will also reset the system. When no pilot interaction is detected for an additional 60 seconds, the Caution Annunciation ‘HYPOXIA ALERT’ is displayed. Again, selecting the ALERT Softkey will acknowledge the message and reset the system. Pressing any other softkey, or turning a knob will also reset the system. When no pilot interaction is detected for an additional 60 seconds, the Warning Annunciation ‘AUTO DESCENT’ is displayed in the Annunciation Window and ‘Automatic descent to 14,000FT in 60 seconds’ is displayed in the Alerts Window. Once again, selecting the ALERT Softkey will acknowledge the message and reset the system. Pressing any other softkey, or turning a knob will also reset the system. When no interaction is detected for another 60 seconds, the system will automatically proceed with the descent. 35 Period Time of of Detected Useful Conciousness Inactivity (Minutes) (min) 30 25 20 15 10 5 0 15000 18000 21000 24000 27000 30000 Aircraft Aircraft Altitude Altitude (Feet) (ft) Figure 8-128 Hypoxia Recognition Activation Times 652 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 190-00820-11 Rev. A
ADDITIONAL FEATURES AUTOMATIC DESCENT MODE NOTE: Automatic Descent Mode does not account for terrain elevation. As the system prepares for descent, the Selected Altitude is set to 14,000 and the AFCS enters Indicated Airspeed (IAS) mode with the airspeed reference set to the maximum allowable airspeed setting for the specific aircraft model. Refer to the Flight Director Vertical Modes in the AFCS section. AFCS lateral mode settings are not affected. As the descent begins, an ‘AUTO DESCENT’ warning is displayed in the Annunciation Window. ‘AUTO DESCENT - Aircraft Descending to 14,000FT’ is displayed in the Alerts Window. ‘EDM’ is shown as an AFCS Status Annunciation indicating the system has entered Automatic Descent Mode. ‘EDM’ (Emergency Descent Mode) is the AFCS mode that is activated when Hypoxia Recognition initiates an automatic descent. A continuous repeating chime will be heard as long as Automatic Descent Mode is active. After the descent begins, Automatic Descent Mode can only be canceled by disconnecting the autopilot. As the aircraft reaches 14,000 feet the system sets the AFCS to Altitude Hold mode. The AFCS will also remain in Automatic Descent Mode as indicated by ‘EDM’ continuing to be displayed as an AFCS Status Annunciation. The system again begins monitoring for pilot interaction. If no pilot interaction is detected for four minutes, the system initiates the second descent. As the system prepares for this descent, the Selected Altitude is set to 12,500 and the AFCS again enters IAS mode with the airspeed reference set to the maximum allowable airspeed for the specific aircraft model. As the descent begins, an ‘AUTO DESCENT’ warning is displayed in the Annunciation Window. ‘AUTO DESCENT - Aircraft Descending to 12,500FT’ is displayed in the Alerts Window. ‘EDM’ is shown as an AFCS Status Annunciation. Also, the continuous repeating chime is heard. As the aircraft reaches 12,500 feet the system sets the AFCS to Altitude Hold mode. The AFCS will also remain in Automatic Descent Mode as indicated by ‘EDM’ continuing to be displayed as an AFCS Status Annunciation as well as the continuing presence of the repeating chime. At this point, the AFCS must be disconnected to cancel Automatic Descent Mode. 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 653
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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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INDEX SYSTEM OVERVIEW FLIGHT INSTRU
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INDEX AUDIO PANEL & CNS EIS FLIGHT
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