曝光台 注意防骗
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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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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(2)
