W DOC AIRBUS | TSM A320F

Low Bleed Pressure of the Engine 1 in Descent/Taxi


TASK 36-11-00-810-A29-A
Low Bleed Pressure of the Engine 1 in Descent/Taxi


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 36-11-00-740-802
BITE Test of the Engine Bleed Air System (EBAS) (System Test)
AMM 36-11-51-000-802
Removal of the HP Bleed Valve
AMM 36-11-51-400-802
Installation of the HP Bleed Valve
AMM 36-11-51-720-804
Functional Test of the HP Bleed Valve with the Test Set P/N 98D36109001000
3. Fault Confirmation
Subtask 36-11-00-710-486-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the EBAS AMM 36-11-00-740-802.
4. Fault Isolation
Subtask 36-11-00-810-483-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) Do the functional test of the HPV AMM 36-11-51-720-804.
       1 If the test is not OK:
Subtask 36-11-00-710-487-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 04:33:57 UTC