Cirrus SR2x

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FLIGHT MANAGEMENT SYSTEM OVERVIEW FLIGHT INSTRUMENTS ACTIVATE COMPENSATION? Highlighted CANCEL COMPENSATION? Highlighted EIS Figure 5-103 Activating/Cancelling Temperature Compensation AUDIO PANEL & CNS FLIGHT MANAGEMENT Compensated Altitudes Uncompensated Altitudes HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 5-104 Temperature Compensation in the Active Flight Plan Cancelling temperature compensated altitude: 1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed. 2) Turn the FMS Knob to highlight ‘Temperature Compensation’. 3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed. 4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted. 5) Press the ENT Key. The temperature compensated altitude at the FAF is cancelled. NOTE: Activating/cancelling temperature compensation for the loaded approach altitudes does not select/ deselect temperature compensated minimums (MDA/DH), nor does selecting/deselecting temperature compensated minimums activate/cancel temperature compensated approach altitudes. INDEX APPENDICES 282 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 190-00820-11 Rev. A
FLIGHT MANAGEMENT 5.9 TRIP PLANNING Perspective allows the pilot to view trip planning information, fuel information, and other information for a specified flight plan or flight plan leg based on automatic data, or based on manually entered data. Weight planning is also available, based on manually entered fuel data and the active flight plan (to estimate remaining fuel). TRIP PLANNING All of the input of data needed for calculation and viewing of the statistics is done on the Trip Planning Page located in the AUX Page Group. Preview of Selected Flight Plan/ Flight Plan Leg Trip Statistics Desired Track - Distance - Est. Time Enroute - Est. Time of Arrival - Enroute Safe Altitude - Sunrise Time (local) - Sunset Time (local) - Fuel Statistics Efficiency - Total Endurance - Remaining Fuel - Remaining Endurance - Fuel Required - Total Range - Selected Flight Plan Segment - FPL Number/Cumulative Legs (CUM or REM) or Leg Number (NN) - Waypoints Defining Selected Flight Plan/Flight Plan Leg Figure 5-106 Trip Planning Page Trip Planning Page Mode - Automatic/Manual Trip Input Data (sensor/pilot) - Departure Time (local) - Ground Speed - Fuel Flow - Fuel On Board Aircraft - Calibrated Airspeed - Indicated Altitude - Barometric Pressure - Total Air Temperature Other Statistics - Density Altitude - True Airspeed (TAS) Softkeys - Automatic/Manual Page Mode - Flight Plan/Waypoint Mode The trip planning inputs are based on sensor inputs (automatic page mode) or on pilot inputs (manual page mode). Some additional explanation of the sources for some of the inputs is as follows: • Departure time (DEP TIME) - This defaults to the current time in automatic page mode. The computations are from the aircraft present position, so the aircraft is always just departing. • Calibrated airspeed (CALIBRATED AS) - The primary source is from the air data system, and the secondary source of information is GPS ground speed. • Indicated altitude (IND ALTITUDE) - The primary source is the barometric altitude, and the secondary source of information is GPS altitude. 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 283
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® Cirrus SR2x Integrated Avionics
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Copyright © 2008-2015 Garmin Ltd.
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Blank Page Pilot’s Guide for the
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WARNINGS, CAUTIONS, AND NOTES WARNI
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TABLE OF CONTENTS 4.5 Additional Au
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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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