W DOC AIRBUS | TSM A320F

Failure of the Dual Flow and Shut Off Valve 6YA


TASK 47-11-00-810-803-A
Failure of the Dual Flow and Shut Off Valve 6YA


1. Possible Causes
  • VALVE-NEA FLOW CTL, IGGS [6YA]
  • wiring from IGGS CTL UNIT (1YA) pin A/14 to DUAL FLOW SOV (6YA) pin A/9
  • wiring from IGGS CTL UNIT (1YA) pin A/38 to DUAL FLOW SOV (6YA) pin A/8
  • wiring from IGGS CTL UNIT (1YA) pin A/82 to DUAL FLOW SOV (6YA) pin A/2
  • wiring from IGGS CTL UNIT (1YA) pin A/23 to DUAL FLOW SOV (6YA) pin A/12
  • wiring from IGGS CTL UNIT (1YA) pin A/50 to DUAL FLOW SOV (6YA) pin A/11
  • wiring from IGGS CTL UNIT (1YA) pin A/60 to DUAL FLOW SOV (6YA) pin A/5
  • wiring from ground to DUAL FLOW SOV (6YA) pin A/1
  • wiring from ground to DUAL FLOW SOV (6YA) pin A/4
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 471101
AMM 47-21-43-000-001
Removal of the Dual-Flow and Shut-off Valve
AMM 47-21-43-400-001
Installation of the Dual-Flow and Shut-off Valve
AMM 47-31-34-740-001
BITE Test of the IGGS with Bleed Air
3. Fault Confirmation
Subtask 47-11-00-740-054-A ** ON A/C NOT FOR ALL
A. Do the BITE test of the IGGS with bleed air AMM 47-31-34-740-001.
4. Fault Isolation
Subtask 47-11-00-810-052-A ** ON A/C NOT FOR ALL
A. Procedure
   (1) Replace the VALVE-NEA FLOW CTL, IGGS [6YA] AMM 47-21-43-000-001 and AMM 47-21-43-400-001.
   (2) Do the test given in para. 3.
   (3) It the fault continues:
     (a) Do a check and repair the:
  • wiring from IGGS CTL UNIT (1YA) pin A/14 to DUAL FLOW SOV (6YA) pin A/9
  • wiring from IGGS CTL UNIT (1YA) pin A/38 to DUAL FLOW SOV (6YA) pin A/8
  • wiring from IGGS CTL UNIT (1YA) pin A/82 to DUAL FLOW SOV (6YA) pin A/2
  • wiring from IGGS CTL UNIT (1YA) pin A/23 to DUAL FLOW SOV (6YA) pin A/12
  • wiring from IGGS CTL UNIT (1YA) pin A/50 to DUAL FLOW SOV (6YA) pin A/11
  • wiring from IGGS CTL UNIT (1YA) pin A/60 to DUAL FLOW SOV (6YA) pin A/5
  • wiring from ground to DUAL FLOW SOV (6YA) pin A/1
  • wiring from ground to DUAL FLOW SOV (6YA) pin A/4 ASM 471101.
Subtask 47-11-00-740-055-A ** ON A/C NOT FOR ALL
B. Do the test given in para. 3.
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