W DOC AIRBUS | TSM A320F

Drift of the Engine 2 Bleed Regulated Pressure Transducer


TASK 36-11-00-810-954-A
Drift of the Engine 2 Bleed Regulated Pressure Transducer


1. Possible Causes
  • wiring
  • C/B-AIR BLEED/ENG 2/MONG [2HA2]
  • XDCR-BLEED REGULATED PRESS, ENG 2 [8HA2]
  • BMC-2 [1HA2]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 24-00-00-810-803-A
Circuit Breaker Tripped and/or C/B TRIPPED Warning
ASM 361102
AMM 36-11-16-000-001
Removal of the Bleed Regulated Pressure-Transducer
AMM 36-11-16-400-001
Installation of the Bleed Regulated Pressure-Transducer
AMM 36-11-34-000-001
Removal of the BMC
AMM 36-11-34-400-001
Installation of the BMC
3. Fault Confirmation
Subtask 36-11-00-740-063-A ** ON A/C NOT FOR ALL
A. Test
   (1) Not applicable.
4. Fault Isolation
Subtask 36-11-00-865-069-A ** ON A/C NOT FOR ALL
A. Table of the circuit breakers used in this procedure:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/MONG2HA2Z22
Subtask 36-11-00-810-248-A ** ON A/C NOT FOR ALL
B. If the fault symptom is identified by the maintenance message:
DRIFT REG-PRESS XDCR 8HA2
  • Do a check of the status of the AIR BLEED/ENG 2/MONG circuit breaker (2HA2).
   (1) If the circuit breaker is closed:
  • Do a check for 28VDC at pin A/1 of the bleed regulated pressure transducer (8HA2) ASM 361102.
     (a) If there is no 28VDC:
  • Do a check for ground at pin A/2 of the bleed regulated pressure transducer (8HA2) ASM 361102.
       1 If there is no ground:
  • Repair the wiring between pin A/2 of the bleed regulated pressure transducer (8HA2) and the ground ASM 361102.
       2 If there is a ground:
  • Do a check of the wiring between pin A/1 of the bleed regulated pressure transducer (8HA2) and the circuit breaker (2HA2) ASM 361102.
         a If there is no continuity:
  • Repair the wiring .
         b If there is continuity:
       3 If the fault continues:
  • Make sure that there is a 0 psig output signal (0.9VDC) at the BMC2 (1HA2) connector between pins AA/11B and AA/12B.
         a If there is no 0.9VDC:
       4 If the fault continues:
  • Do a check and repair the wiring between pins A/3 and A/4 of the bleed regulated pressure transducer (8HA2) and pins AA/12B and AA/11B of the BMC2 (1HA2) ASM 361102.
     (b) If there is 28VDC:
   (2) If the circuit breaker is open:
     (a) If the fault continues:
  • Replace the C/B-AIR BLEED/ENG 2/MONG [2HA2] .
     (b) If the circuit breaker stays closed and the fault continues:
Subtask 36-11-00-740-064-A ** ON A/C NOT FOR ALL
C. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:33:51 UTC