W DOC AIRBUS | TSM A320F

Loss of the ADIRU input Data through the Channel B or disagree between Aircraft and Engine sensors on Engine 1


TASK 73-20-00-810-961-A
Loss of the ADIRU input Data through the Channel B or disagree between Aircraft and Engine sensors on Engine 1


1. Possible Causes
  • PS12 Sensing Line
  • T12 temperature sensor
  • ADIRU-1 (1PF1)
  • ADIRU-2 (1PF2)
  • ADIRU-3 (1PF3)
  • pitot or static probes
  • ECU [4000KS]
  • P0 inlet port
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 72-23-00-000-040
Removal of the PS12 Line
AMM 72-23-00-280-002
Inspection/Check of the PS12 line
AMM 72-23-00-400-040
Installation of the PS12 Line
AMM 73-21-40-000-001
Removal of the T12 Temperature Sensor
AMM 73-21-40-400-001
Installation of the T12 Temperature Sensor
AMM 73-21-50-000-042
Removal of the HJ9 Harness for SAC Engines
AMM 73-21-50-000-043
Removal of the HJ10 Harness for SAC Engines
AMM 73-21-50-210-001
Visual Inspection of the Wiring Harness
AMM 73-21-50-400-042
Installation of the HJ9 Harness for SAC Engines
AMM 73-21-50-400-043
Installation of the HJ10 Harness for SAC Engines
AMM 73-21-60-000-001
Removal of the Electronic Control Unit (ECU)
AMM 73-21-60-400-001
Installation of the Electronic Control Unit (ECU)
AMM 73-21-60-740-007
Correct Time Limited Faults (Non Asterisked) of the Engine Scheduled Maintenance Report
3. Fault Confirmation
Subtask 73-20-00-710-288-A ** ON A/C NOT FOR ALL
A. Not applicable
4. Fault Isolation
Subtask 73-20-00-810-243-A ** ON A/C NOT FOR ALL
A. The fault is triggered by the ECU if the ADIRU inputs data to the ECU (TAT, Total Pressure and Altitude) disagree with the engine sensor inputs ( PS12 Sensing Line , T12 temperature sensor , P0).
   (1) If the failure message PO/P12/T12, ADC, ECU* or PO/P12/T12, ADC, ECU is displayed and one or more failure message(s) linked to the ADIRU-1 (1PF1), ADIRU-2 (1PF2), ADIRU-3 (1PF3), pitot or static probes is (are) present:
  • do the trouble shooting procedures related to the ADC, pitot probes or static probes failure message.
Subtask 73-20-00-810-244-A ** ON A/C NOT FOR ALL
B. If the fault message PO/P12/T12, ADC, ECU* or PO/P12/T12, ADC, ECU is displayed and no failure message linked to the ADC, static probes or pitot probes is (are) present:
  • Check in the Schedule Maintenance Report (SMR) or in the Class 3 Report AMM 73-21-60-740-007 for presence of failure message(s): "ECU (P0 SENSOR)", "T12 SNSR, J9, ECU", "T12 SNSR, J10, ECU", "ECU (PS12 SENSOR)".
   (1) If a fault is present:
  • do the trouble shooting per applicable procedure.
   (2) If no fault is found:
  • make sure there P0 inlet port located on the Pressure plate of the ECU [4000KS] is open and free from obstruction.
     (a) If damage is found:
  • clean the P0 inlet port ,
     (b) If nothing is found:
       1 if damage is found:
       2 if nothing is found, continues the troubleshooting as follows:
   (3) disconnect the J9 and J10 harnesses from the ECU (4000KS), and visually examine the ECU receptacles and the harnesses connectors for damaged pins or contamination AMM 73-21-50-210-001:
     (a) If damage is found:
  • clean or repair damaged parts as required.
     (b) If nothing is found:
       1 If the fault continues:
         a If the fault continues:
Subtask 73-20-00-710-289-A ** ON A/C NOT FOR ALL
C. No test is required for fault repair confirmation.
  • No additionnal maintenance action is required if the fault is not confirmed,
  • Repeat the fault isolation process if the fault continues.
[Rev.8 from Aug 2018] 2026.04.04 04:41:27 UTC