W DOC AIRBUS | TSM A320F

APU AUTO SHUT DOWN - REVERSE FLOW, Bleed Flow Transducer Fault (APS 3200)


TASK 49-00-00-810-933-A
APU AUTO SHUT DOWN - REVERSE FLOW, Bleed Flow Transducer Fault (APS 3200)


1. Possible Causes
  • COMPRESSOR DISCHARGE-PRESSURE SNSR P24
  • aircraft wiring
  • ELECTRONIC CONTROL BOX [59KD]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ESPM 2052210
ESPM 2053210
ESPM 205321A
AMM 49-00-00-710-008
Operational Test of the APU
AMM 49-51-19-000-002
Removal of the Sensor - Compressor Discharge Pressure (APS 3200)
AMM 49-51-19-400-002
Installation of the Sensor - Compressor Discharge Pressure (APS 3200)
ASM 496102
AMM 49-61-34-000-002
Removal of the Electronic Control Box (ECB) (APS 3200)
AMM 49-61-34-400-002
Installation of the Electronic Control Box (ECB) (APS 3200)
3. Fault Confirmation
Subtask 49-00-00-710-302-B ** ON A/C NOT FOR ALL
A. Do the operational test of the APU AMM 49-00-00-710-008.
4. Fault Isolation
Subtask 49-00-00-810-240-B ** ON A/C NOT FOR ALL
A. If an APU auto shutdown occurs during the operational test of the APU and the APU SHUTDOWNS report gives the maintenance message

REVERSE FLOW - BLEED FLOW XDCR P24

NOTE: Do a check and make sure that the orifices and the lines which are connected to the compressor discharge pressure sensor are not clogged. Clean if necessary.
   (1) If the fault continues:
   (2) If the fault continues:
Subtask 49-00-00-710-303-B ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:34:26 UTC