W DOC AIRBUS | TSM A320F

Downstream Pressure Transducer Disagree on Channels A and B

TASK 30-21-00-810-826-A
Downstream Pressure Transducer Disagree on Channels A and B

1. Possible Causes
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
PLIERS - JAWED, SOFT
 B. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 71-00-00-810-835-A
Component and Harness Intermittent Troubleshooting Procedure for Guidance Troubleshooting Intermittent Faults
AMM 30-21-23-000-801
Removal of the Nacelle Anti-Ice Fan-Pressure-Transducer
AMM 30-21-23-400-801
Installation of the Nacelle Anti-Ice Fan-Pressure-Transducer
AMM 71-13-00-010-802
Opening of the Fan Cowl Doors
AMM 71-13-00-410-802
Closing of the Fan Cowl Doors
AWM 715134
AMM 73-21-00-710-806
Test No.7 - EEC Operation Test (Self Test)
AMM 73-21-01-000-801
Removal of the Electronic Engine Control (EEC)
AMM 73-21-01-400-801
Installation of the Electronic Engine Control (EEC)
AMM 73-21-63-000-802
Removal of the Electronic Engine Control (EEC) Wiring Harness (W03)
AMM 73-21-63-400-802
Installation of the Electronic Engine Control (EEC) Wiring Harness (W03)
AMM 73-21-64-000-802
Removal of the Electronic Engine Control (EEC) Wiring Harness (W04)
AMM 73-21-64-400-802
Installation of the Electronic Engine Control (EEC) Wiring Harness (W04)
3. Fault Confirmation
Subtask 30-21-00-730-063-A ** ON A/C NOT FOR ALL
A. Test
Do the EEC system test AMM 73-21-00-710-806.
   (1) If the maintenance message does not come into view again, do the component and harness intermittent for guidance troubleshooting intermittent faults (Ref. TSM TASK 71-00-00-810-835).
     (a) If you find no fault, send the engine back to service. Monitor the engine to make sure that the maintenance message does not come into view again.
   (2) If the maintenance message comes into view again (hard fault) for channels A and B, go to the Para. Fault Isolation.
4. Fault Isolation
WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS WARNING, INJURY CAN OCCUR.
CAUTION: MAKE SURE YOU REMOVE ELECTRICAL POWER FROM THE EEC BEFORE YOU REMOVE THE ELECTRICAL CONNECTORS. IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE EEC CAN OCCUR.
Subtask 30-21-00-810-075-A ** ON A/C NOT FOR ALL
A. If there is confirmation of the fault:
   (1) Open the fan cowl doors AMM 71-13-00-010-802.
   (2) Make sure that electrical connector P17 of the W04 harness is correctly engaged in the receptacle of the NAI fan pressure-transducer.
     (a) If it is not correctly engaged, engage it.
  • Do the test given in Para. 3.
   (3) If the fault continues, or if electrical connector P17 is correctly engaged use PLIERS - JAWED, SOFT to disconnect electrical connector P17 from the receptacle of the NAI fan pressure-transducer:
  • Examine electrical connector P17 of the W04 harness for bent pins, contamination, corrosion or signs of damage.
     (a) If you find damage on electrical connector P17:
       1 Replace the W04 HARNESS [4088KS] AMM 73-21-64-000-802 and AMM 73-21-64-400-802.
       2 Do the test given in Para. 3.
     (b) If you find no damage on electrical connector P17 or the fault continues, use PLIERS - JAWED, SOFT to disconnect electrical connectors P14 from the EEC.
  • Do a continuity check of the W03 harness AWM 715134 between:
    . Pin P14/q of the EEC and pin P106/11 of 4100VC
    . Pin P14/BB of the EEC and pin P106/12 of 4100VC
    . Pin P14/p of the EEC and pin P106/25 of 4100VC
    . Pin P14/T of the EEC and pin P106/26 of 4100VC.
       1 If there is no continuity:
       2 If there is no continuity:
  • Do a continuity check of the W04 harness AWM 715134 between:
    . Pin J106/11 of 4100VC and P17/9 of the NAI fan pressure-transducer
    . Pin J106/12 of 4100VC and P17/8 of the NAI fan pressure-transducer
    . Pin J106/25 of 4100VC and P17/7 of the NAI fan pressure-transducer
    . Pin J106/26 of 4100VC and P17/6 of the NAI fan pressure-transducer.
         a If there is no continuity:
         b If there is continuity:
Use PLIERS - JAWED, SOFT to disconnect electrical connectors P13 from the EEC.
  • Do a continuity check of W04 harness AWM 715134 between:
    . Pin P13/q of the EEC and pin P17/12 of the NAI fan pressure-transducer
    . Pin P13/BB of the EEC and pin P17/4 of the NAI fan pressure-transducer
    . Pin P13/p of the EEC and pin P17/3 of the NAI fan pressure-transducer
    . Pin P13/T of the EEC and pin P17/11 of the NAI fan pressure-transducer.
    If there is no continuity:
  • Replace the W04 HARNESS [4088KS] AMM 73-21-64-000-802 and AMM 73-21-64-400-802.
  • Do the test given in Para. 3.
If there is continuity:
  • Examine the receptacle of the NAI fan pressure-transducer for bent pins, contamination or corrosion or signs of damage.
    * If you find damage on the receptacle:
  • Replace PRESS XDCR-ENGINE AIR INTAKE ANTI ICE, 2 [4003DN] AMM 30-21-23-000-801 and AMM 30-21-23-400-801.
  • Do the test given in Para. 3.
    * If you find no damage on the receptacle:
  • Do a resistance check on the NAI fan pressure-transducer AWM 715134 between:
    . Pin J17/3 and pin J17/12 of the NAI fan pressure-transducer
    . Pin J17/4 and pin J17/11 of the NAI fan pressure-transducer
    . Pin J17/6 and pin J17/7 of the NAI fan pressure-transducer
    . Pin J17/8 and pin J17/9 of the NAI fan pressure-transducer.
    ** If the resistance is more than 12.5 kohm:
    ** Replace PRESS XDCR-ENGINE AIR INTAKE ANTI ICE, 2 [4003DN] AMM 30-21-23-000-801 and AMM 30-21-23-400-801.
    ** Do the test given in Para. 3.
    *** If the resistance is less than 12.5 kohm:
    *** Replace the [4000KS] AMM 73-21-01-000-801 and AMM 73-21-01-400-801.
    *** Do the test given in Para. 3.
5. Close-up
Subtask 30-21-00-942-067-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Make sure that the work area is clean and clear of tools and other items.
     (a) Close the fan cowl doors AMM 71-13-00-410-802.
[Rev.8 from Aug 2018] 2026.04.04 04:29:33 UTC
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