Engine-driven pump (EDP) does not stop when YELLOW ENG 2 PUMP P/BSW is OFF
TASK 29-13-00-810-821-A
Engine-driven pump (EDP) does not stop when YELLOW ENG 2 PUMP P/BSW is OFF
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 29-13-00-710-072-A
Subtask 29-13-00-810-077-A ** ON A/C NOT FOR ALL
Subtask 29-13-00-942-051-A
[Rev.8 from Aug 2018]
2026.04.04 04:29:27 UTC
Engine-driven pump (EDP) does not stop when YELLOW ENG 2 PUMP P/BSW is OFF
1. Possible Causes
- CONNECTOR [3030-GD--A]
- PUMP VARIABLE DTS [3030GD]
P/BSW 3703GD - engine pump solenoid-valve
- C/B-HYDRAULIC/Y HYD/PUMP ENG2/CTL [3701GD]
- SDAC
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 29-13-00-710-002 | Operational Test of the Yellow Hydraulic System |
| ASM 291301 | |
| AMM 29-13-51-000-011 | Removal of the Solenoid-Valve of Engine Pump |
| AMM 29-13-51-000-802 | Removal of the Solenoid-Valve of Engine Pump |
| AMM 29-13-51-400-011 | Installation of the Solenoid-Valve of Engine Pump |
| AMM 29-13-51-400-802 | Installation of the Solenoid-Valve of Engine Pump |
Subtask 29-13-00-710-072-A
A. Do the operational test of the Yellow hydraulic system AMM 29-13-00-710-002.
(1) If the hydraulic pressure during the test of the Yellow hydraulic system does not decrease to 0 psi (0.0 bar), go to Para. 4.A.
4. Fault Isolation(1) If the hydraulic pressure during the test of the Yellow hydraulic system does not decrease to 0 psi (0.0 bar), go to Para. 4.A.
Subtask 29-13-00-810-077-A ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
(1) Do a check of the EDP:
(a) Disconnect the electrical connector CONNECTOR [3030-GD--A] from the PUMP VARIABLE DTS [3030GD] .
(b) Make sure that theP/BSW 3703GD is released.
(c) On the electrical connector CONNECTOR [3030-GD--A] do a check for +28VDC at pin 3.
(d) Connect the electrical connector CONNECTOR [3030-GD--A] to the PUMP VARIABLE DTS [3030GD] .
(e) If there is +28VDC and the EDP P/N is 887673 or 3031863-001:
1 Replace the engine pump solenoid-valve AMM 29-13-51-000-802 and AMM 29-13-51-400-802.
2 Do the test given in Para. 3.
(f) If the fault continues:
1 Replace the PUMP VARIABLE DTS [3030GD] .
2 Do the test given in Para. 3.
(2) If the fault continues:
(a) Remove theP/BSW 3703GD .
(b) On the rack, do a check for +28VDC at pin AA/C3.
(c) Install theP/BSW 3703GD .
(d) If there is +28VDC:
1 Replace theP/BSW 3703GD .
2 Do the test given in Para. 3.
(3) If the fault continues:
(a) Do a check of the aircraft wiring between:
Subtask 29-13-00-810-077-B ** ON A/C NOT FOR ALL (1) Do a check of the EDP:
(a) Disconnect the electrical connector CONNECTOR [3030-GD--A] from the PUMP VARIABLE DTS [3030GD] .
(b) Make sure that the
(c) On the electrical connector CONNECTOR [3030-GD--A] do a check for +28VDC at pin 3.
(d) Connect the electrical connector CONNECTOR [3030-GD--A] to the PUMP VARIABLE DTS [3030GD] .
(e) If there is +28VDC and the EDP P/N is 887673 or 3031863-001:
1 Replace the engine pump solenoid-valve AMM 29-13-51-000-802 and AMM 29-13-51-400-802.
2 Do the test given in Para. 3.
(f) If the fault continues:
1 Replace the PUMP VARIABLE DTS [3030GD] .
2 Do the test given in Para. 3.
(2) If the fault continues:
(a) Remove the
(b) On the rack, do a check for +28VDC at pin AA/C3.
(c) Install the
(d) If there is +28VDC:
1 Replace the
2 Do the test given in Para. 3.
(3) If the fault continues:
(a) Do a check of the aircraft wiring between:
- The PUMP VARIABLE DTS [3030GD] and the
P/BSW 3703GD - The
P/BSW 3703GD and the C/B-HYDRAULIC/Y HYD/PUMP ENG2/CTL [3701GD] - The PUMP VARIABLE DTS [3030GD] and the SDAC
A. If the test confirms the fault:
(1) Do a check of the EDP:
(a) Disconnect the electrical connector CONNECTOR [3030-GD--A] from the PUMP VARIABLE DTS [3030GD] .
(b) Make sure that theP/BSW 3703GD is released.
(c) On the electrical connector CONNECTOR [3030-GD--A] do a check for +28VDC at pin 3.
(d) Connect the electrical connector CONNECTOR [3030-GD--A] to the PUMP VARIABLE DTS [3030GD] .
(e) If there is +28VDC and the EDP P/N is 887673 or 3031863-001:
1 Replace the engine pump solenoid-valve AMM 29-13-51-000-011 and AMM 29-13-51-400-011.
2 Do the test given in Para. 3.
(f) If the fault continues:
1 Replace the PUMP VARIABLE DTS [3030GD] .
2 Do the test given in Para. 3.
(2) If the fault continues:
(a) Remove theP/BSW 3703GD .
(b) On the rack, do a check for +28VDC at pin AA/C3.
(c) Install theP/BSW 3703GD .
(d) If there is +28VDC:
1 Replace theP/BSW 3703GD .
2 Do the test given in Para. 3.
(3) If the fault continues:
(a) Do a check of the aircraft wiring between:
5. Close-up(1) Do a check of the EDP:
(a) Disconnect the electrical connector CONNECTOR [3030-GD--A] from the PUMP VARIABLE DTS [3030GD] .
(b) Make sure that the
(c) On the electrical connector CONNECTOR [3030-GD--A] do a check for +28VDC at pin 3.
(d) Connect the electrical connector CONNECTOR [3030-GD--A] to the PUMP VARIABLE DTS [3030GD] .
(e) If there is +28VDC and the EDP P/N is 887673 or 3031863-001:
1 Replace the engine pump solenoid-valve AMM 29-13-51-000-011 and AMM 29-13-51-400-011.
2 Do the test given in Para. 3.
(f) If the fault continues:
1 Replace the PUMP VARIABLE DTS [3030GD] .
2 Do the test given in Para. 3.
(2) If the fault continues:
(a) Remove the
(b) On the rack, do a check for +28VDC at pin AA/C3.
(c) Install the
(d) If there is +28VDC:
1 Replace the
2 Do the test given in Para. 3.
(3) If the fault continues:
(a) Do a check of the aircraft wiring between:
- The PUMP VARIABLE DTS [3030GD] and the
P/BSW 3703GD - The
P/BSW 3703GD and the C/B-HYDRAULIC/Y HYD/PUMP ENG2/CTL [3701GD] - The PUMP VARIABLE DTS [3030GD] and the SDAC
Subtask 29-13-00-942-051-A
A. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.
(1) Make sure that the work area is clean and clear of tools and other items.