W DOC AIRBUS | TSM A320F

Low Bleed Pressure of the Engine 1 in Descent/Taxi


TASK 36-11-00-810-875-A
Low Bleed Pressure of the Engine 1 in Descent/Taxi


1. Possible Causes
  • VALVE-HP BLEED [4000HA]
  • sense line between the bleed-pressure regulator-valve control-solenoid (10HA1) and the bleed pressure-regulator valve (4001HA)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 36-11-00-740-001
BITE Test of the BMC 1(2)
AMM 36-11-49-000-026
Removal of the Sense Line between the Bleed Pressure-Regulator Valve (PRV) and the Pylon Interface
AMM 36-11-49-400-026
Installation of the Sense Line between the Bleed Pressure-Regulator Valve (PRV) and the Pylon Interface
AMM 36-11-51-000-042
Removal of the High Pressure Bleed Valve
AMM 36-11-51-400-042
Installation of the High Pressure Bleed Valve
3. Fault Confirmation
Subtask 36-11-00-710-197-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 36-11-00-810-125-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:
CAUTION: USE TWO WRENCHES DURING DISCONNECTION OF THE SENSE LINE, ONE TO MAINTAIN THE FIXED NUT AND THE SECOND ONE TO LOOSEN/TIGHTEN THE SENSE LINE COUPLING.
CAUTION: BE CAREFUL WITH THE SEMI-FLEXIBLE SENSE LINE. DEFORMATION OF THE RIGID PART OR LARGE DEFORMATION OF THE FLEXIBLE PART CAN QUICKLY CAUSE LEAKAGE.
     (a) If the fault continues:
Subtask 36-11-00-710-198-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 04:33:47 UTC