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All A. VOR mode The COMM./VOR-ILS/GPS transceiver is tuned to the frequency displayed in the VOR/LOC window of the display. The VOR signal is received by the antenna and transmitted to the COMM./VOR-ILS/GPS transceiver via A59 VOR signal separator (if installed). The COMM./VOR-ILS/GPS transceiver converts the VOR signals into continuous signals to control the vertical pointer, the "TO-FR" indicator and the NAV warning flag. The transceiver processes the audio identification signal from the VOR ground station and sends it to A50 audio control panel. B. ILS mode When a LOC frequency is selected on the COMM./VOR-ILS/GPS transceiver, the GS receiver automatically tunes to the paired Glide Slope frequency. The LOC and GS signals are received by the VOR and GS antenna and then transmitted to the COMM./VOR-ILS/GPS transceiver via A59 VOR signal separator (if installed) and A60 GS signal separator (if installed) respectively. COMM./VOR-ILS/GPS transceiver converts the LOC and GS signals into continuous signals to actuate the vertical pointer, the horizontal pointer and the paired warning flags. C. Coupling to the autopilot system (option) The A82 flight computer of the autopilot receives the VOR, GPS navigation data or LOC and GS approach data. D. Coupling to the Distance Measuring Equipment (DME) (option) The COMM./VOR-ILS/GPS transceiver sends the frequency information necessary to tune the interrogator of the Distance Measuring Equipment. E. Coupling to the Radio Magnetic Indicator (option) The COMM./VOR-ILS/GPS transceiver sends to the RMI the information that are necessary to display the bearing of the VOR ground station. ANAN Validity : GNS 430 34-51 00 (DI) Page 8 NOV 01 TRANSPONDEUR ( 34 - 53 - 00 ) TRANSPONDER ECRAN MULTIFONCTION ( 34 - 62 - 00 ) MULTIFUNCTION DISPLAY DEBITMETRE TOTALISATEUR ( 73 - 30 - 00 ) FUEL FLOW TOTALIZER SEPARATEUR DE SIGNAUX GS GS SIGNAL SEPARATOR SEPARATEUR DE SIGNAUX VOR VOR SIGNAL SEPARATOR NAV 1 installation — Schematic |
