W DOC AIRBUS | TSM A320F

Failure of the Bleed Bias System on Engine 2


TASK 75-30-00-810-830-B
Failure of the Bleed Bias System on Engine 2


1. Possible Causes
  • bleed bias venturi
  • bleed bias transducer
  • ECU [4000KS]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
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 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
AMM 75-34-10-000-001
Removal of the Bleed Bias Transducer
AMM 75-34-10-400-001
Installation of the Bleed Bias Transducer
AMM 75-34-20-000-001
Removal of the Bleed Bias Venturi
AMM 75-34-20-400-001
Installation of the Bleed Bias Venturi
3. Fault Confirmation
Subtask 75-30-00-710-118-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the operational test of the FADEC 2A on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 75-30-00-810-084-A ** ON A/C NOT FOR ALL
A. If the CLASS 3 FAULTS page gives the maintenance message CWB3, WB3 SENS, J15:
  • do a check for leakage or blockage of the pressure tubes between the bleed bias transducer and the bleed bias venturi.
   (1) If the fault continues:
   (2) If the fault continues:
   (3) If the fault continues:
Subtask 75-30-00-810-084-B ** ON A/C NOT FOR ALL
A. If the CLASS 3 FAULTS page gives the maintenance message VTURI, BLD SNSR, ECU:
  • do a check for leakage or blockage of the pressure tubes between the bleed bias transducer and the bleed bias venturi.
   (1) If the fault continues:
   (2) If the fault continues:
   (3) If the fault continues:
Subtask 75-30-00-710-119-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:37:09 UTC