W DOC AIRBUS | TSM A320F

APU AUTO SHUTDOWN - SENSOR FAILURE, EGT1 Sensor Fault and ECB internal Fault (131-9(A))


TASK 49-00-81-810-814-A
APU AUTO SHUTDOWN - SENSOR FAILURE, EGT1 Sensor Fault and ECB internal Fault (131-9(A))


1. Possible Causes
  • EGT1 SENSOR FAILURE AND ECB INTERNAL FAILURE
  • EGT THERMOCOUPLE RAKE 1
  • ELECTRONIC CONTROL BOX [59KD]
  • EGT THERMOCOUPLE RAKE (8057KM1)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 49-00-00-860-008
APU Start by External Power
AMM 49-61-34-000-003
Removal of the Electronic Control Box (ECB) (131-9(A))
AMM 49-61-34-400-003
Installation of the Electronic Control Box (ECB) (131-9(A))
AMM 49-72-15-000-002
Removal of the Thermocouples (131-9(A))
AMM 49-72-15-400-003
Installation of the Thermocouples (131-9(A))
3. Fault Confirmation
Subtask 49-00-81-710-114-A ** ON A/C NOT FOR ALL
A. Read-out of ECB Trouble-Shooting Data
   (1) Put the APU MASTER SW to the ON position.
   (2) Get access to the APU SHUTDOWN report.
   (3) Push the '>' adjacent to LRU DATA:
  • the MCDU menu shows
    EGT1 SENSOR FAILURE AND ECB INTERNAL FAILURE

   (4) Start the APU and apply Bleed Air for 20 seconds, minimum AMM 49-00-00-860-008.
4. Fault Isolation
Subtask 49-00-81-810-088-A ** ON A/C NOT FOR ALL
A. If an APU auto shutdown occurs during the APU operation and the APU SHUTDOWN report gives the maintenance message:

SENSOR FAIL
EGT TCPLE RAKE 1 + ECB (59KD)

associated with the Fault Code Number (FCN) 36

Subtask 49-00-81-810-088-B ** ON A/C NOT FOR ALL
A. If an APU auto shutdown occurs during the APU operation and the APU SHUTDOWN report gives the maintenance message:

SENSOR FAIL
EGT TCPLE RAKE (8057KM1) AND ECB (59KD)

associated with the Fault Code Number (FCN) 36

Subtask 49-00-81-710-115-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:34:32 UTC