W DOC AIRBUS | TSM A320F

Air Separation Module (ASM) 1YM Performance Degraded Fault


TASK 47-11-00-810-806-A
Air Separation Module (ASM) 1YM Performance Degraded Fault


1. Possible Causes
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
BRUSH - BRISTLED, SMALL
 B. Referenced Information
REFERENCE
DESIGNATION
AMM 47-10-43-920-001
Air Separator Module Replacement
AMM 47-31-34-740-001
BITE Test of the IGGS with Bleed Air
AMM 47-41-15-000-001
Removal of the Oxygen Sensor
AMM 47-41-15-400-002
Installation of the Oxygen Sensor
3. Fault Confirmation
Subtask 47-11-00-740-060-B ** ON A/C NOT FOR ALL
A. Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
Subtask 47-11-00-810-055-B ** ON A/C NOT FOR ALL
A. Procedure
NOTE: Do the two subsequent steps at the same time. Two persons are necessary to do these steps.
   (1) Do the BITE test of the IGGS with bleed air AMM 47-31-34-740-001.
   (2) Examine all the ducts and connections between the ASM and the oxygen sensor for signs of air leakage.
   (3) If there are no leaks:
     (a) Remove the O2 sensor duct AMM 47-41-15-000-001 and examine its inner surface for signs of contamination.
     (b) If there is contamination:
  • Clean the contamination with a BRUSH - BRISTLED, SMALL or similar.
     (c) If there is no contamination:
     (d) Install the O2 sensor duct AMM 47-41-15-400-002.
   (4) If there are leaks:
     (a) Replace the defective connections, refer to the CMM 471141 (V92003).
NOTE: Before installation, clean the inner surface of the O2 sensor duct with a BRUSH - BRISTLED, SMALL or similar.
NOTE: Do the two subsequent steps at the same time. Two persons are necessary to do these steps.
     (b) Do the BITE test of the IGGS with bleed air AMM 47-31-34-740-001.
     (c) Examine the 02 sensor duct and its connections for signs of air leakage.
     (d) If there are leaks do again the previous step (2).
Subtask 47-11-00-740-061-B ** ON A/C NOT FOR ALL
B. Do the BITE test of the IGGS with bleed air AMM 47-31-34-740-001.
NOTE: After the subsequent flight make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:34:22 UTC