Cirrus SR2x

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AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW Prior to descent path interception, the Selected Altitude must be set below the current aircraft altitude by at least 75 feet. In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the PFD Navigation Status Box and the “Vertical track” voice message, VNV indications (VNV Target Altitude, vertical deviation, and vertical speed required) appear on the PFD in magenta (Figure 7-11). FLIGHT INSTRUMENTS GPS Navigation Mode Active Altitude Hold Mode Active EIS Selected Altitude VNV Target Altitude AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE GPS is Selected Navigation Source Terminal Phase of Flight Vertical Deviation Indicator Figure 7-11 Vertical Path Capture Required Vertical Speed Bug INDEX APPENDICES ADDITIONAL FEATURES AFCS 510 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 190-00820-11 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM When a descent leg is captured (i.e., vertical deviation becomes valid), Vertical Path Tracking becomes active and tracks the descent profile (Figure 7-12). An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate. SYSTEM OVERVIEW Vertical Path Tracking Active Selected Altitude Capture Armed FLIGHT INSTRUMENTS VNV Target Altitude EIS GPS is Selected Navigation Source Terminal Phase of Flight Command Bars Indicate Descent to Maintain Required Vertical Speed Figure 7-12 Vertical Path Tracking Mode Vertical Deviation Indicator (VDI) Required Vertical Speed Indication If the altimeter barometric setting is adjusted while Vertical Path Tracking is active, the flight director increases/decreases the descent rate by up to 500 fpm to re-establish the aircraft on the descent path (without commanding a climb). Adjusting the altimeter barometric setting creates discontinuities in VNV vertical deviation, moving the descent path. For large adjustments, it may take several minutes for the AFCS to re-establish on the descent path. If the change is made while nearing a waypoint with a VNV Target Altitude, the aircraft may not re-establish on the descent path in time to meet the vertical constraint. Automatic Reversion to Pitch Hold Mode Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode: • Vertical deviation exceeds 200 feet during an overspeed condition. • Vertical deviation experiences a discontinuity that both exceeds 200 feet in magnitude and results in the vertical deviation exceeding 200 feet in magnitude. Such discontinuities are usually caused by flight plan changes that affect the vertical profile. • Vertical deviation becomes invalid (the Vertical Deviation Indicator is removed from the PFD). • A display enters Reversionary Mode (this does not apply to an active vertical direct-to). Unless VNV is disabled, Vertical Path Tracking Mode and the appropriate altitude capture mode become armed following the reversion to Pitch Hold Mode to allow for possible profile recapture. 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 511
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® Cirrus SR2x Integrated Avionics
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INDEX SYSTEM OVERVIEW FLIGHT INSTRU
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INDEX AUDIO PANEL & CNS EIS FLIGHT
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