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
A. Referenced Information
3. Fault Confirmation
Subtask 47-11-00-740-054-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 47-11-00-810-052-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:34:22 UTC
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
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 |
Subtask 47-11-00-740-054-A ** ON A/C NOT FOR ALL 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:
Subtask 47-11-00-740-055-A ** ON A/C NOT FOR ALL (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.
B. Do the test given in para. 3.
NOTE: After the subsequent flight make sure that the fault does not continue.