DOC AIRBUS | AMM A320FDC MAIN DISTRIBUTION - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. General
The main 28 VDC distribution network corresponds to busbars 1PP, 2PP, 3PP, 6PP and associated sub-busbars,
** ON A/C NOT FOR ALL The main 28 VDC distribution network corresponds to busbars 1PP, 2PP, 3PP, 6PP and associated sub-busbars,
2. Component Location
DC Main Distribution - Component Location ** ON A/C NOT FOR ALL
DC Main Distribution - Component Location ** ON A/C NOT FOR ALL
** ON A/C NOT FOR ALL DC Main Distribution - Component Location ** ON A/C NOT FOR ALL DC Main Distribution - Component Location ** ON A/C NOT FOR ALL | FIN | FUNCTIONAL DESIGNATION | PANEL | ZONE | ACCESS DOOR | ATA REF |
|---|---|---|---|---|---|
| ** ON A/C ALL | |||||
| 8PN | CNTOR-DC SVCE BUS NORM SPLY | 120VU | 212 | 24-61-55 | |
| 10PN | CONTACTOR | 120VU | 212 | 24-61-55 | |
3. Operation/Control and Indicating
Busbars 1PP, 3PP are supplied by TR1.
Busbars 2PP, 6PP are supplied by TR2.
In case of loss of supply, a warning is triggered on the ECAM system,
In case of loss of main busbars, the ELEC page is automatically displayed on the ECAM lower display unit:
Busbars 1PP, 3PP are supplied by TR1.
Busbars 2PP, 6PP are supplied by TR2.
NOTE: In case of loss of one main TR, both main busbars are supplied by the remaining main TR.
Busbar 6PP is supplied in flight and/or on ground. This busbar can be supplied, independently from the main network, by the ground power unit via TR2 in ground service configuration (Ref. 24-43-00, P. Block 1). In case of loss of supply, a warning is triggered on the ECAM system,
In case of loss of main busbars, the ELEC page is automatically displayed on the ECAM lower display unit: