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┃                                ┃                            ┃1.24.10     P 10      ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃I          ELECDESCRIPTION  ┃SEQ 001 1 ┃I REV 23  ┃
┃ aw aw ,, ~L,~ A319             ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
FAILURE OF AC BUS 1
The AC BUS 2 can supply the AC ESS BUS and the ESS TR can supply the DC ESS BUS,
both through the AC ESS FEED pushbutton switch.
The DC BUS 2 supplies the DC BUS 1 and DC BAT BUS automatically after 5 seconds.
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━┓
┃I  -~ A318                      ┃ELECTRICAL  ┃1.24.10     P 11  ┃
┃  .*,,.8, ,, ~L,~ A319          ┃            ┃                  ┃
┃ Lli,~ A320                     ┃            ┃                  ┃
┃                                ┃            ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃DESCRIPTION ┃SEQ 001 ┃BEV 23  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃            ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━┻━━━━┛
FAILURE OF ONE TR
The contactor of each TR opens automatically in case of
- overheat
- minimum current
The other TR automatically replaces the fautly one.
The ESS TR supplies the DC ESS BUS.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                            ┃1.24.10     P 12      ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(2)