Cirrus SR2x

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SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS Viewing GPS receiver status information: 1) Turn the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.6 for information on navigating MFD page groups). 2) Turn the small FMS Knob to select AUX - GPS Status Page. 3) To change the selected GPS receiver: Press the desired GPS Softkey. Or: a) Press the MENU Key. b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key. AUDIO PANEL & CNS Satellite Constellation Diagram Satellite Signal Information GPS Receiver Status FLIGHT MANAGEMENT HAZARD AVOIDANCE RAIM Availability Prediction AFCS Satellite Signal Strength Bars APPENDICES INDEX ADDITIONAL FEATURES Figure 1-22 GPS Status Page 34 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 190-00820-11 Rev. A
SYSTEM OVERVIEW The GPS Status Page provides the following information: • Satellite constellation diagram Satellites currently in view are shown at their respective positions on a sky view diagram. The sky view is always in a north-up orientation, with the outer circle representing the horizon, the inner circle representing 45° above the horizon, and the center point showing the position directly overhead. Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification number). Satellites whose signals are currently being used are represented by solid ovals. • Satellite signal information status The accuracy of the aircraft’s GPS fix is calculated using Estimated Position Uncertainty (EPU), Dilution of Precision (DOP), and horizontal and vertical figures of merit (HFOM and VFOM). EPU is the radius of a circle centered on an estimated horizontal position in which actual position has 95% probability of laying. EPU is a statistical error indication and not an actual error measurement. DOP measures satellite geometry quality (i.e., number of satellites received and where they are relative to each other) on a range from 0.0 to 9.9, with lower numbers denoting better accuracy. HFOM and VFOM, measures of horizontal and vertical position uncertainty, are the current 95% confidence horizontal and vertical accuracy values reported by the GPS receiver. The current calculated GPS position, time, altitude, ground speed, and track for the aircraft are displayed below the satellite signal accuracy measurements. • GPS receiver status The GPS solution type (ACQUIRING, 2D NAV, 2D DIFF NAV, 3D NAV, 3D DIFF NAV) for the active GPS receiver (GPS1 or GPS2) is shown in the upper right of the GPS Status Page. When the receiver is in the process of acquiring enough satellite signals for navigation, the receiver uses satellite orbital data (collected continuously from the satellites) and last known position to determine the satellites that should be in view. ACQUIRING is indicated as the solution until a sufficient number of satellites have been acquired for computing a solution. When the receiver is in the process of acquiring a 3D differential GPS solution, 3D NAV is indicated as the solution until the 3D differential fix has finished acquisition. SBAS (Satellite-Based Augmentation System) indicates INACTIVE. When acquisition is complete, the solution status indicates 3D DIFF NAV and SBAS indicates ACTIVE. • RAIM (Receiver Autonomous Integrity Monitoring) Prediction (RAIM Softkey is pressed) In most cases performing a RAIM prediction is not necessary. However, in some cases, the selected approach may be outside the SBAS coverage area and it may be necessary to perform a RAIM prediction for the intended approach. Receiver Autonomous Integrity Monitoring (RAIM) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (2.0 nautical miles for oceanic and enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is available nearly 100% of the time. The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival date and time. 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 35
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INDEX AUDIO PANEL & CNS EIS FLIGHT
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