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┃I  -~ A318                      ┃ELECTRICAL  ┃1.24.10     P 17  ┃
┃  .*,,.8, ,, ~L,~ A319          ┃            ┃                  ┃
┃ Lli,~ A320                     ┃            ┃                  ┃
┃                                ┃            ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃DESCRIPTION ┃SEQ 001 ┃REV 27  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃            ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━┻━━━━┛
SMOKE CONFIGURATION
In this configuration the main bus bars are shedded. The electrical distribution is the same
as it is in the emergency configuration (loss of main generators), except that the fuel
pumps are connected upstream of the GEN 1 line connector.
The procedure sheds about 75 % of electrical equipment. All equipment that remains
powered is supplied through C/Bs on the overhead panel (except for that which is supplied
by hot buses).
CCM ALL
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┃                                ┃                            ┃1.24.10     P 18      ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
┃I  -~ A318                      ┃I          ELECDESCRIPTION  ┃SEQ 001 1 ┃I REV 23  ┃
┃  .,,,.8, ,, ~L,~ A319          ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(9)