Cirrus SR2x

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HAZARD AVOIDANCE SYSTEM OVERVIEW Figures 6-161 and 6-162 shows the NCR alerting parameters as defined by TSO-C151b based on Altitude Loss and Sink Rate respectively. 1000 FLIGHT INSTRUMENTS EIS Height Above Terrain (Feet) 900 800 700 600 500 400 300 200 “DON’T SINK” or “TOO LOW, TERRAIN” AUDIO PANEL & CNS 100 0 0 20 40 60 80 100 120 140 Altitude Loss (Feet) FLIGHT MANAGEMENT 1000 900 Figure 6-161 Negative Climb Rate (NCR) Altitude Loss HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES INDEX APPENDICES 800 Height Above Terrain (Feet) 700 600 500 400 300 200 100 “DON’T SINK” or “TOO LOW, TERRAIN” 0 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000 Sink Rate (FPM) Figure 6-162 Negative Climb Rate (NCR) Sink Rate 442 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 190-00820-11 Rev. A
HAZARD AVOIDANCE SYSTEM STATUS During power-up, TAWS-B conducts a system test of its alerting capabilities. The system test can also be manually initiated. A single chime is issued at test completion. TAWS-B system testing is disabled when ground speed exceeds 30 knots. System Condition PFD/MFD Alert Annunciation TAWS-B Page Annunciation Voice Alert System Test in Progress TAWS TEST None System Test Pass None None Single Chime TAWS System Test Fail TAWS FAIL “TAWS System Failure” SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS Table 6-24 TAWS-B System Test Status Annunciations Manually testing the TAWS-B System: 1) Select the TAWS-B Page. 2) Press the MENU Key (Figure 6-163). 3) Select ‘Test TAWS System’ and press the ENT Key to confirm the selection. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-163 TAWS-B Page Menu TAWS-B continually monitors several system-critical items such as database validity, hardware status, and GPS status. If the terrain/obstacle database is not available, the voice alert “TAWS System Failure” is generated along with the ‘TAWS FAIL’ alert annunciation. TAWS-B requires a 3-D GPS navigation solution along with specific vertical accuracy minimums. Should the navigation solution become degraded or if the aircraft is out of the database coverage area, the annunciation ‘TAWS N/A’ is generated in the annunciation window and on the TAWS-B Page. The voice alert “TAWS Not Available” is generated. When the GPS signal integrity is restored and the aircraft is within the database coverage area, the voice alert “TAWS Available” is generated. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-11 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 443
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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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APPENDIX E SYSTEM OVERVIEW HAZARD A
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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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