W DOC AIRBUS | TSM A320F

Loss of the R Yellow Brake Pressure-Transducer Input of the SDAC 2


TASK 31-54-00-810-821-A
Loss of the R Yellow Brake Pressure-Transducer Input of the SDAC 2


1. Possible Causes
  • SDAC-2 [1WV2]
  • wiring
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 31-50-00-710-001
Ground Scanning of the Central Warning System
AWM 315470
AMM 31-55-34-000-001
Removal of the SDAC
AMM 31-55-34-400-001
Installation of the SDAC
3. Fault Confirmation
Subtask 31-54-00-865-060-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUL/G/Y BRK/PRESS/IND61GGC10
** ON A/C NOT FOR ALL
49VUABCU &/Y BRK/PRESS IND61GGC10
Subtask 31-54-00-710-078-A
B. Test
Do the ground scanning of the central warning systems AMM 31-50-00-710-001.
4. Fault Isolation
Subtask 31-54-00-810-070-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message SDAC2 : RH Y BRK PRESS XDCR 62GG:
   (1) If the fault continues:
  • do a check and repair the wiring from the SDAC 2 (1WV2) pins AB/13G, 13H to the first terminal block , AWM 315470.
Subtask 31-54-00-810-070-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message SDAC2 : RH Y BRK PRESS XDCR 100GG:
   (1) If the fault continues:
  • do a check and repair the wiring from the SDAC 2 (1WV2) pins AB/13G, 13H to the first terminal block , AWM 315470.
Subtask 31-54-00-710-079-A
B. Do the test given in Para. 3.B.
[Rev.8 from Aug 2018] 2026.04.04 04:30:24 UTC