W DOC AIRBUS | TSM A320F

Loss of the Power Supply of the Bleed Pressure-Regulator Valve of the Engine 2


TASK 36-11-00-810-854-A
Loss of the Power Supply of the Bleed Pressure-Regulator Valve of the Engine 2


1. Possible Causes
  • BMC-2 [1HA2]
  • wiring between the BMC2 pin AB/1B and the ground terminal
  • wiring between the BMC2 pin AA/8A and the circuit breaker (3HA2)
  • C/B-AIR BLEED/ENG 2/CTL [3HA2]
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 36-11-34-000-001
Removal of the BMC
AMM 36-11-34-400-001
Installation of the BMC
3. Fault Confirmation
Subtask 36-11-00-710-152-A ** ON A/C NOT FOR ALL
A. Not applicable.
4. Fault Isolation
Subtask 36-11-00-865-058-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/CTL3HA2Z23
Subtask 36-11-00-810-102-B ** ON A/C NOT FOR ALL
B. If the fault symptom is identified by the maintenance message CHECK PRESS REG-V PWR SPLY:
  • Do a check of the status of the circuit breaker (3HA2).
   (1) If the circuit breaker (3HA2) is closed:
  • Do a check for 28VDC at pin AA/8A of the BMC2 (1HA2) ASM 361102.
     (a) If there is 28VDC:
     (b) If there is no 28VDC:
  • Do a check for ground at pin AB/1B of the BMC2 (1HA2).
       1 If there is no ground:
  • Repair the wiring between the BMC2 pin AB/1B and the ground terminal .
       2 If there is ground:
  • Do a check of the wiring between the BMC2 pin AA/8A and the circuit breaker (3HA2).
         a If there is no continuity:
  • Repair the above wiring.
         b If there is continuity:
  • Replace the circuit breaker (3HA2).
   (2) If the circuit breaker (3HA2) is open:
     (a) If the fault continues:
  • Replace the C/B-AIR BLEED/ENG 2/CTL [3HA2] .
     (b) If the circuit breaker stays closed and the fault continues:
  • Replace the BMC-2 [1HA2] .
Subtask 36-11-00-710-153-A ** ON A/C NOT FOR ALL
C. Do the operational test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:33:45 UTC