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┃ ┃ ┃1.24.10 P 8 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I ELECDESCRIPTION ┃SEQ 001 1 ┃I REV 23 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
On ground, when only ground services are required, external power can supply the AC and
DC GND/FLT BUSES directly without supplying the entire aircraft network.
Personnel select this configuration with the MAINT BUS switch in the forward entrance
area.
CCM ALL
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┃I ~-~ A318 ┃ELECTRICAL ┃1.24.10 P 9 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃DESCRIPTION ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━┻━━━━┛
ABNORMAL CONFIGURATIONS
FAILURE OF ONE ENGINE GENERATOR
The system automatically replaces the failed generator with
- the APU GEN if available, or
- the other engine generator (automatically shedding part of the galley load)
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
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本文链接地址:AIRBUS A320 Flight Crew Operating Manual3