W DOC AIRBUS | TSM A320F

Failure of the SDAC Detected by the CSAS


TASK 21-58-00-810-813-A
Failure of the SDAC Detected by the CSAS


1. Possible Causes
  • SDAC-1 [1WV1]
  • CSAS CONTROL UNIT [100HW]
  • wiring of the SDAC 1 DATA BUS
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 215301
AMM 21-58-00-710-001
Operational Test of the Conditioned Service Air System without Bleed Air
AMM 21-58-34-000-001
Removal of the CSAS Control Unit
AMM 21-58-34-400-001
Installation of the CSAS Control Unit
AMM 31-50-00-710-001
Ground Scanning of the Central Warning System
AMM 31-55-34-000-001
Removal of the SDAC
AMM 31-55-34-400-001
Installation of the SDAC
3. Fault Confirmation
Subtask 21-58-00-710-074-A ** ON A/C NOT FOR ALL
A. Do the operational test of the conditioned service air system without bleed air AMM 21-58-00-710-001.
4. Fault Isolation
Subtask 21-58-00-810-062-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message SDAC1(1WV1)/CSAS CTL UNIT(100HW):
   (1) If the test gives a different maintenance message, do the related trouble shooting procedure.
   (2) If the fault continues:
   (3) If the fault continues:
     (a) If the fault continues:
  • remove the SDAC 1 and the CSAS CONTROL UNIT
  • do a check and repair the wiring of the SDAC 1 DATA BUS : between pins AE/9B,9C of the SDAC 1 and pins AB/10HG,10J of the CSAS CONTROL UNIT ASM 215301
  • install the SDAC 1 and the CSAS CONTROL UNIT
Subtask 21-58-00-710-075-A ** ON A/C NOT FOR ALL
B. Do the test as given in the Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:24:50 UTC