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┃ Lli,~ A320                     ┃                        ┃SEQ 200 I ┃J REV 28  ┃
┃      A~7-~'M" A321             ┃CONTROLS AND INDICATORS ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                        ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━━┻━━━━━┛
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                              ┃1.24.20     P 2       ┃
┃                                ┃                              ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃I     CONTROLSCANDCINDICATORS ┃SEQ 200 1 ┃I REV 23  ┃
┃ aw aw ,, ~% A319               ┃                              ┃          ┃          ┃
┃ Lli,~ A320                     ┃                              ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                              ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                              ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
     BAT 1 (2) pb sw
Controls the operation of the corresponding battery charge limiter.
Auto     The battery charge limiter controls automatically the connection and the
            disconnection of the corresponding battery to the DC BAT BUS (3 PP) by
            closing and opening of the battery line contactor.
            - The batteries are connected to the DC BAT BUS in the following cases
               ~ APU starting (MASTER SW at ON and N < 95%).
OFF
FAULT It
Note: The connection is limited to 3 minutes when the emergency
       generator is running.
~ Battery voltage below 26.5 V (battery charge). The charging cycle ends
 when battery charge current goes below 4 amperes.
 - on ground, immediately
 - in flight, after a time delay of 30 minutes.
~ Loss of AC BUS 1 and 2 when below 100 knots (EMER GEN not
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(14)