W DOC AIRBUS | TSM A320F

Failure of the HPV of Engine 2 in the Open Position


TASK 36-11-00-810-976-A
Failure of the HPV of Engine 2 in the Open Position


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 36-11-49-000-823
Removal of the Environmental Control System (ECS) Sense Lines
AMM 36-11-49-400-823
Installation of the Environmental Control System (ECS) Sense Lines
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
AMM 36-22-00-790-802
Leak Check on all the Bleed Air Ducts and Packs Components
3. Fault Confirmation
Subtask 36-11-00-710-440-A ** ON A/C NOT FOR ALL
A. Not applicable
4. Fault Isolation
Subtask 36-11-00-810-341-A ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the maintenance message HP BLEED-V (4000HA2)/SENSE LINE:
   (1) Turn the manual shaft of the HPV to OPEN.
   (2) Let the manual shaft go back to closed position.
     (a) If the valve does not go back to the closed position:
     (b) If the valve go back to the closed position:
       1 If the test is not OK:
       2 If the test is OK:
  • Continue the trouble shooting procedure.
Subtask 36-11-00-810-342-A ** ON A/C NOT FOR ALL
B. If the fault continues:
   (1) Replace the sense line of the HPV AMM 36-11-49-000-823 AMM 36-11-49-400-823.
   (2) Do a leak check of the sense line of the HPV AMM 36-22-00-790-802.
Subtask 36-11-00-710-441-A ** ON A/C NOT FOR ALL
C. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:33:52 UTC