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GLOBAL POSITIONING SYSTEM (GPS) DESCRIPTION AND OPERATION 1. GENERAL The GPS is a satellite-based radionavigation system which enables an aircraft to be located anywhere (tridimensional positioning : latitude, longitude and altitude). The system consists of : - the A78 GPS receiver, - the E48 GPS antenna, - the configuration module (if installed), Interfaced-with-HSI version - the A92 relay box, - the A93 relay box. The system uses the horizontal situation indicator (HSI) of the heading reference system - refer to 34-21-00. All The system also uses annunciators/switches or indicator lights of M6 advisory panel - refer to 31-50-00. The GPS receiver receives information from the following equipment : - the fuel flow system (option) - refer to 73-30-00, - the encoding altimeter (option) - refer to 34-11-00. The GPS sends information to the following equipment : - the A50 audio control panel - refer to 23-11-00, - the M63 multifunction display (option) - refer to 34-62-00, - the VHF NAV/COMM. (KX 155A or KX 165A) transceiver of NAV1 installation or NAV2 installation (option) -refer to 34-51-00 or 34-52-00. The system is electrically supplied by "BUS 3" bar. 2. LOCATION (Figure 1) COMPONENT QTY AREA ACCESS DOOR REFERENCE A78 GPS receiver 1 251C / 34-50-00 E48 GPS antenna 1 240 / 34-57-02 A92 relay box (option) 1 250 / 34-57-05 A93 relay box (option) 1 250 / 34-57-05 Configuration module (if installed) 1 250 / 34-57-00 APAP 3. DESCRIPTION |