W DOC AIRBUS | TSM A320F

Bleed Valve of Engine 2 Failed in Open or Close Position


TASK 36-11-00-810-981-A
Bleed Valve of Engine 2 Failed in Open or Close Position


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 361102
AMM 36-11-52-000-802
Removal of the Bleed Pressure-Regulator Valve
AMM 36-11-52-400-802
Installation of the Bleed Pressure-Regulator Valve
AMM 36-11-52-720-811
Functional Test of the Pressure Regulator Valve with the Test Set P/N 98D36109001000
3. Fault Confirmation
Subtask 36-11-00-710-448-A ** ON A/C NOT FOR ALL
A. Test
   (1) Not applicable.
4. Fault Isolation
Subtask 36-11-00-810-385-A ** ON A/C NOT FOR ALL
A. If the fault is identified by the maintenance message PRESS REG-V (4001HA2):
   (1) Do a functional test of the PRV bleed valve AMM 36-11-52-720-811.
     (a) If the test is not OK:
     (b) If the test is OK:
  • Continue the trouble shooting procedure.
Subtask 36-11-00-810-352-A ** ON A/C NOT FOR ALL
B. If the fault continues:
   (1) Do a check of the wiring between the Bleed Valve (4001HA2) pin A/1 and A/2 to BMC2 (1HA2) pin AB/14C and AA/14B ASM 361102.
   (2) If the wiring is damaged:
  • Repair or replace the wiring .
Subtask 36-11-00-810-353-A ** ON A/C NOT FOR ALL
C. If the fault continues:
   (1) Do a check of the wiring between the Bleed Valve (4001HA2) A/1 and A/2 to BMC1 (1HA1) pin AB/15C and AB/15B ASM 361102.
   (2) If the wiring is damaged:
  • Repair or replace the wiring .
Subtask 36-11-00-710-449-A ** ON A/C NOT FOR ALL
D. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:33:52 UTC