|
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
In ILS operation (landing aid), the system allows a continuous guidance in azimuth (LOC) and in elevation (GLIDE). The optional system consists of : - the A52 VHF NAV / COMM transceiver, - the M74 Course Deviation Indicator (CDI). The system uses the VOR and GS antennas and the VOR and GS signal separators. All these components are described in NAV 1 installation - refer to 34-51-00. For the description of the communication portion of the VHF NAV / COMM transceiver, refer to 23-13-00. The system sends signals to : - the A50 Audio Control Box - refer to 23-11-00, the A110 NAV converter of the EFIS system - refer to 34-28-00, the optional Distance Measuring Equipment (DME) system - refer to 34-55-00. The system is electrically supplied by "BUS 3" bus bar via the CB88 "COM NAV 2" circuit breaker. 2. LOCATION (Figure 2) COMPONENT QTY AREA ACCESS DOOR REFERENCE A52 VHF NAV / COMM Transceiver 1 251 C / 34-50-00 M74 Course Deviation Indicator (CDI) 1 251 L / 34-52-00 Circuit breaker : - CB88 "COM NAV 2" 1 232L / WM ANTENNE GS GS ANTENNA SEPARATEUR DE SIGNAUX GS GS SIGNAL SEPARATOR ANTENNE Von VOR ANTENNA SEPARATEUR DE SIGNAUX VOR VOR SIGNAL SEPARATOR CONVERTISSEUR NAV NAV CONVERTER NAV 2 ARINC 429 SYSTEME EFIS EFIS SYSTEM VERS NAV 1 VERS NAV 1 TO NAV 1 TO NAV 1 EMETTEUR / RECEPTEUR VHF - NAV / COMM VHF - NAV / COMM TRANSCEIVER SIGNAUX VOR / LOC ET GS VOR / LOC AND GS SIGNALS DRAPEAUX VOR / LOC ET GS VOR / LOC AND GS FLAGS SYSTEME EFIS EFIS SYSTEM ( 34 - 28 - 00 ) INDICATEUR ECART DE ROUTE COURSE DEVIATION INDICATOR |
