W DOC AIRBUS | TSM A320F

The Bleed Pressure-Regulator Valve of the Engine 1 is Shown Open Amber on the Lower ECAM DU


TASK 36-11-00-810-902-A
The Bleed Pressure-Regulator Valve of the Engine 1 is Shown Open Amber on the Lower ECAM DU


1. Possible Causes
  • VALVE-BLEED PRESS REG [4001HA]
  • SOLENOID-BLEED PRESS REG V CTL, ENG 1 [10HA1]
  • XDCR-BLEED TRANSFER PRESS, ENG 1 [7HA1]
  • wiring
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 36-11-00-740-001
BITE Test of the BMC 1(2)
ASM 361101
AMM 36-11-15-000-001
Removal of the Bleed Transferred Pressure-Transducer
AMM 36-11-15-400-001
Installation of the Bleed Transferred Pressure-Transducer
AMM 36-11-52-000-040
Removal of the Bleed Pressure-Regulator Valve
AMM 36-11-52-000-042
Removal of the Bleed Pressure Regulator Valve
AMM 36-11-52-400-040
Installation of the Bleed Pressure-Regulator Valve
AMM 36-11-52-400-042
Installation of the Bleed Pressure Regulator Valve
AMM 36-11-55-000-001
Removal of the Bleed-Pressure-Regulator Valve Control-Solenoid
AMM 36-11-55-400-001
Installation of the Bleed-Pressure-Regulator Valve Control-Solenoid
3. Fault Confirmation
Subtask 36-11-00-710-250-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the BMC1 AMM 36-11-00-740-001.
4. Fault Isolation
Subtask 36-11-00-810-152-A ** ON A/C NOT FOR ALL
A. If the test gives a maintenance message:
  • Do the trouble shooting procedure related to the maintenance message.
   (1) If there is no maintenance message:
     (a) If the fault continues:
       1 If the fault continues:
         a If the fault continues:
  • do a check and repair the wiring :
    . from the FULLY CLOSED signal of the BMC1 (1HA1) to the bleed pressure-regulator valve (4001HA)
    . from pin A/3 of the bleed pressure-regulator valve (4001HA) to the first terminal block ASM 361101.
Subtask 36-11-00-810-152-C ** ON A/C NOT FOR ALL
A. If the test gives a maintenance message:
  • Do the trouble shooting procedure related to the maintenance message.
   (1) If there is no maintenance message:
     (a) If the fault continues:
       1 If the fault continues:
         a If the fault continues:
  • Do a check and repair the wiring :
    . From pin AA/2B of the BMC1 (1HA1) to pin A/5 of the bleed pressure-regulator valve (4001HA)
    . From pin A/3 of the bleed pressure-regulator valve (4001HA) to the first terminal block ASM 361101.
Subtask 36-11-00-710-251-A ** ON A/C NOT FOR ALL
B. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:33:49 UTC