W DOC AIRBUS | TSM A320F

The HP Bleed Valve of the Engine 2 is Shown Closed Amber on the Lower ECAM DU

TASK 36-11-00-810-909-A
The HP Bleed Valve of the Engine 2 is Shown Closed Amber on the Lower ECAM DU

1. Possible Causes
  • VALVE-HP BLEED [4000HA]
  • sense line between the bleed pressure-regulator valve (4001HA) and the control solenoid (10HA2)
  • VALVE-BLEED PRESS REG [4001HA]
  • wiring
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 36-11-00-720-007
Functional Test of the Sense Lines Connected to the Bleed Pressure-Regulator Valve with the Bleed Test Set P/N 98D36003000000
AMM 36-11-00-740-001
BITE Test of the BMC 1(2)
ASM 361102
AMM 36-11-49-000-029
Removal of the Pneumatic Sense Lines in the Pylon
AMM 36-11-49-000-042
Removal of the Pylon Interface Duct
AMM 36-11-49-400-029
Installation of the Pneumatic Sense Lines in the Pylon
AMM 36-11-49-400-042
Installation of the Pylon Interface Duct
AMM 36-11-51-000-040
Removal of the High Pressure Bleed Valve
AMM 36-11-51-000-042
Removal of the High Pressure Bleed Valve
AMM 36-11-51-400-040
Installation of the High Pressure Bleed Valve
AMM 36-11-51-400-042
Installation of the High Pressure Bleed Valve
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
3. Fault Confirmation
Subtask 36-11-00-710-264-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the BMC2 AMM 36-11-00-740-001.
4. Fault Isolation
Subtask 36-11-00-810-159-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:
  • do the functional test of the upstream sense line between the bleed pressure-regulator valve (4001HA) and the control solenoid (10HA2) AMM 36-11-00-720-007.
       1 If the pressure decreases to 0 psig in less than 20 seconds:
       2 If the pressure drop is not high:
         a If the fault continues:
  • do a check and repair the wiring :
    . from the FULLY CLOSED signal of the BMC2 (1HA2) to the bleed pressure-regulator valve (4001HA)
    . from pin A/5 of the bleed pressure-regulator valve (4001HA) to the first terminal block ASM 361102.
Subtask 36-11-00-810-159-D ** 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:
  • Do the functional test of the upstream sense line between the bleed pressure-regulator valve (4001HA) and the control solenoid (10HA2) AMM 36-11-00-720-007.
       1 If the pressure decreases to 0 psig in less than 20 seconds:
       2 If the pressure decreases by a small value.
         a If the fault continues:
  • Do a check and repair the wiring :
    . From pin AA/2B of the BMC2 (1HA2) to pin A/5 of the bleed pressure-regulator valve (4001HA)
    . From pin A/5 of the bleed pressure-regulator valve (4001HA) to the first terminal block ASM 361102.
Subtask 36-11-00-710-265-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
"WTRUIB" 2025