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AlAl Validity : KX 165 with EFIS 34-52-00 (EA) Page 4 FEB 00 TRANSPONDER DESCRIPTION AND OPERATION 1. GENERAL (Figures 1, 1A, 1B and 1C) The transponder allows the operational air traffic service to identify the aircraft. The optional system consists of : - an A56 transponder, - an E36 antenna, - a conversion kit (28 volts only). The transponder can receive altitude information from the optional encoding altimeter or altitude encoder refer to 34-11-00. A desensitization line connects the transponder to the optional DME installation - refer to 34-55-00. 14-volt aircraft The transponder is electrically supplied by "BUS 1" or "BUS 2" or "BUS 3" bar(s) via the "ATC" circuit breaker. 28-volt aircraft The transponder is electrically supplied by "BUS 1" and / or "BUS 2" bar(s) via the "XPDR" circuit breaker. 2. LOCATION (Figure 2) COMPONENT QTY AREA ACCESS DOOR REFERENCE A56 transponder 1 251C / 34-50-00 E36 antenna 1 210 215 34-53-03 E012 conversion kit 1 250 211R 34-53-00 Circuit breakers : - "XPDR" 1 230 232L WM - "ATC" 1 230 232L WM 3. OPERATION NOTE : For equipment operation and maintenance, refer to the supplier's Maintenance Manual. Transponder - Electrical schematic Transponder - Electrical schematic |
