W DOC AIRBUS | AMM A320F

DC ESSENTIAL & NORMAL GENERATION SWITCHING - DESCRIPTION AND OPERATION


** ON A/C NOT FOR ALL
1. General
These circuits control the supply of DC normal busbars and DC essential busbars.
They enable:
  • their normal supply in normal flight configuration,
  • automatic transfer in some failure conditions.
** ON A/C NOT FOR ALL
2. Component Location
-------------------------------------------------------------------------------
FIN ! FUNCTIONAL DESIGNATION ! PANEL ! ZONE ! ACCESS ! ATA
! ! ! ! DOOR ! REF.
-------------------------------------------------------------------------------
20PC1 FUSE 120VU 212 24-35-00

FIN FUNCTIONAL
DESIGNATION
PANEL ZONE ACCESS
DOOR
ATA REF
** ON A/C ALL
1PC1 CNTOR-DC NORM BUS 1 SWITCHING 120VU 212 24-35-55
1PC2 CNTOR-DC NORM BUS 2 SWITCHING 120VU 212 24-35-55
4PC CNTOR-DC ESS BUS SUPPLY 106VU 125 24-35-55
** ON A/C NOT FOR ALL
20PC HOLDER-FUSE 120VU 212 24-35-00
** ON A/C NOT FOR ALL
3. Operation/Control and Indicating
A. DC NORM BUS SWITCHING Contactor Control (1PC1 and 1PC2)
Contactor 1PC1 is supplied in normal configuration and when a TR is lost.
Contactor 1PC2 is supplied when a TR is lost or in case of DC NORM BUS 1 SWITCHING contactor (1PC1) failure.
NOTE: There is an electric interlock between contactors 1PC2 and 4PC to inhibit coupling between busbar 2PP and essential busbar 4PP.
B. DC ESS BUS SPLY Contactor Control (4PC)
Contactor 4PC supplies DC ESS BUS 4PP via BAT BUS 3PP if normal DC busbars 1PP and 2PP are not coupled (electrical interlock between contactors 1PC2 and 4PC).
DC ESS BUS SPLY contactor (4PC) opens when a normal TR is lost (coupling of busbars 1PP and 2PP), in emergency conditions or when the DC NORM BUS 1 SWITCHING contactor (1PC1) is lost.
[Rev.10 from 2021] 2026.03.31 23:23:35 UTC