W DOC AIRBUS | TSM A320F

Air Leak in the Right Wing with the APU in Operation


TASK 36-22-00-810-883-A
Air Leak in the Right Wing with the APU in Operation


1. Possible Causes
  • ducts
  • seals
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 21-52-00-200-010
Hot-Air Leak-Check in the Air Conditioning Bay
AMM 24-41-00-861-002
Energize the Aircraft Electrical Circuits from the External Power
AMM 24-41-00-862-002
De-energize the Aircraft Electrical Circuits Supplied from the External Power
AMM 31-60-00-860-001
EIS Start Procedure
AMM 31-60-00-860-002
EIS Stop Procedure
AMM 36-11-48-000-004
Removal of the Bleed Air Ducts
AMM 36-11-48-400-004
Installation of the Bleed Air Ducts
AMM 36-22-00-790-802
Leak Check on all the Bleed Air Ducts and Packs Components
AMM 49-00-00-860-008
APU Start by External Power
AMM 49-00-00-860-009
APU Shutdown by External Power (131-9(A))
3. Fault Confirmation
Subtask 36-22-00-860-064-A ** ON A/C NOT FOR ALL
A. Job Set-up
   (1) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
   (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
Subtask 36-22-00-860-067-B ** ON A/C NOT FOR ALL
B. Test
   (1) Start the APU AMM 49-00-00-860-008.
   (2) On AIR COND panel 30VU, push the APU BLEED pushbutton switch (5HV) (the ON legend comes on).
4. Fault Isolation
Subtask 36-22-00-810-154-A ** ON A/C NOT FOR ALL
A. On the upper ECAM DU, if the AIR R WING LEAK warning comes into view:
  • do a leak test on the bleed air ducts between wing anti ice valves and wing fuselage connections AMM 36-22-00-790-802.
   (1) If there are leaks:
   (2) If there is no leak:
     (a) If there are cracks or damage on the ducts:
     (b) If there are leaks on the seals:
  • replace the defective seals .
5. Close-up
Subtask 36-22-00-860-068-B ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) On the AIR COND panel 30VU, release the APU BLEED pushbutton switch (5HV) (the ON legend goes off).
   (2) Stop the APU AMM 49-00-00-860-009.
Subtask 36-22-00-860-065-A ** ON A/C NOT FOR ALL
B. Put the aircraft back to its initial configuration.
   (1) Do the EIS stop procedure
AMM 31-60-00-860-002.
   (2) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
[Rev.8 from Aug 2018] 2026.04.04 04:34:11 UTC