W DOC AIRBUS | TSM A320F

Outflow Valve Fault (05), (11), (24), (25), (26), (29), (60)


TASK 21-31-00-810-807-A
Outflow Valve Fault (05), (11), (24), (25), (26), (29), (60)


1. Possible Causes
  • VALVE-OUTFLOW (10HL), AUTO MOTOR 1
  • OUTFLOW VALVE [10HL]
  • VALVE-OUTFLOW (10HL), FEEDBACK ASSEMBLY
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 21-31-00-710-002
Operational Test of the Pressure Control and Monitoring
AMM 21-31-51-000-001
Removal of the Outflow Valve (From Inside)
AMM 21-31-51-000-003
Removal of the Outflow Valve (10HL) - Auto Motor 10HL-3 (10HL-4)
AMM 21-31-51-000-005
Removal of the Outflow Valve - Feedback Assembly 10HL-6
AMM 21-31-51-000-006
Removal of the Outflow Valve (From Outside)
AMM 21-31-51-400-001
Installation of the Outflow Valve (From Inside)
AMM 21-31-51-400-003
Installation of the Outflow Valve (10HL) - Auto Motor 10HL-3 (10HL-4)
AMM 21-31-51-400-005
Installation of the Outflow Valve - Feedback Assembly 10HL-6
AMM 21-31-51-400-006
Installation of the Outflow Valve (From Outside)
3. Fault Confirmation
Subtask 21-31-00-710-056-A
A. Test
   (1) Do the operational test of the pressure control and monitoring system AMM 21-31-00-710-002.
4. Fault Isolation
Subtask 21-31-00-810-061-A
A. If one of the reports, LAST LEG REPORT, PREVIOUS LEG REPORT, CLASS 3 FAULTS and/or the test gives one of the maintenance messages which follow,
  • OUTFLOW VALVE (05),
  • OUTFLOW VALVE (11),
  • OUTFLOW VALVE (24),
  • OUTFLOW VALVE BLOCKED (29) or,
  • OUTFLOW VALVE (60):
  • replace the VALVE-OUTFLOW (10HL), AUTO MOTOR 1 AMM 21-31-51-000-003 and AMM 21-31-51-400-003.
   (1) If the fault continues:
Subtask 21-31-00-810-109-A
B. Test Result
NOTE: This procedure is only applicable for Outflow Valve Part Numbers 9023-15703 and previous.
   (1) If the test gives the maintenance message,
OUTFLOW VALVE (25), or
OUTFLOW VALVE (26):
Subtask 21-31-00-810-110-A
C. Test Result
NOTE: This procedure is only applicable for Outflow Valve Part Number 20790-01AA and onwards.
   (1) If the test gives the maintenance message,
OUTFLOW VALVE (25), or
OUTFLOW VALVE (26):
Subtask 21-31-00-710-065-A
D. Do the test as given in the Para. 3.A.
5. Close-up
Subtask 21-31-00-860-056-A
A. Put the aircraft back to its initial configuration.
[Rev.8 from Aug 2018] 2026.04.04 04:24:41 UTC