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┃ A~7-~'M" A321 ┃DESCRIPTION ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━┻━━━━┛
GENERAL
GEN 1 and 2 when operating have priority over the APU generator and over external power.
External power has priority over the APU generator when the EXT PWR pushbutton switch
is ON.
The APU generator or external power can supply the entire network.
One engine generator can supply the entire network.
The generators cannot be connected in parallel.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.24.10 P 6 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I ~-~ A318 ┃I ELECDESCRIPTION ┃SEQ 001 1 ┃I REV 23 ┃
┃ aw aw ,, ~L,~ .4319 ┃ ┃ ┃ ┃
┃ Lii,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
NORMAL CONFIGURATION
IN FLIGHT
Each engine-driven generator supplies its associated AC BUS (1 and 2) via its generator
line contactor (GLC 1 and GLC 2).
AC BUS 1 normally supplies the AC ESS BUS via a contactor.
TR 1 normally supplies DC BUS 1, DC BAT BUS, and DC ESS BUS.
TR 2 normally supplies DC BUS 2.
The two batteries are connected to the DC BAT BUS if they need charging. When they are
fully charged the battery charge limiter disconnects them.
┏━━━━━━━━━━━━━━━━━━━━┓
┃/ELEC ┃
┃ IDG 1 ~Cl10 115 ~C IDG 2 ┃
┣━━━━━━━━━━━━━━━━━━━━┫
┃ I I ┃
┗━━━━━━━━━━━━━━━━━━━━┛
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━┓
┃I -~ A318 ┃ELECTRICAL ┃1.24.10 P 7 ┃
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本文鏈接地址：
AIRBUS A320 Flight Crew Operating Manual2(158)
