Operational Check of APU Low Pressure Fuel Valve for evidence of internal Leakage with left Wing Tank Pump on
TASK 28-29-00-710-002-A
Operational Check of APU Low Pressure Fuel Valve for evidence of internal Leakage with left Wing Tank Pump on
Refer to the MPD TASK: 282900-02
OPERATIONAL CHECK OF APU LP FUEL VALVE FOR EVIDENCE OF INTERNAL LEAKAGE WITH LEFT WING TANK PUMP ON
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 28-29-00-860-052-A
Subtask 28-29-00-710-052-A ** ON A/C NOT FOR ALL
Subtask 28-29-00-860-053-A
[Rev.10 from 2021]
2026.04.02 06:18:02 UTC
Operational Check of APU Low Pressure Fuel Valve for evidence of internal Leakage with left Wing Tank Pump on
WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
1. Reason for the JobRefer to the MPD TASK: 282900-02
OPERATIONAL CHECK OF APU LP FUEL VALVE FOR EVIDENCE OF INTERNAL LEAKAGE WITH LEFT WING TANK PUMP ON
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT) |
| No specific | AR | CONTAINER 5 L (1.32 USGAL) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| 98A28007570000 | 1 | ADAPTER - VENT AND DRAIN VALVE, APU |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 315AL |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 28-29-41-000-001-A | Removal of the APU Fuel Low-Pressure Valve |
| TASK 28-29-41-400-001-A | Installation of the APU Fuel Low-Pressure-Valve |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
Subtask 28-29-00-860-052-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) On the FUEL overhead panel 40VU, make sure that all L TK PUMPS and R TK PUMPS pushbutton switches are released (the OFF legends are on).
(4) On the APU section of the overhead panel 25VU, make sure that the APU MASTER SW pushbutton switch is in the off position (the ON legend is off).
Subtask 28-29-00-865-054-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) On the FUEL overhead panel 40VU, make sure that all L TK PUMPS and R TK PUMPS pushbutton switches are released (the OFF legends are on).
(4) On the APU section of the overhead panel 25VU, make sure that the APU MASTER SW pushbutton switch is in the off position (the ON legend is off).
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 28-29-00-865-056-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 121VU | APU/FUEL/LP VALVE/CTL | 1QF | M40 |
| 121VU | APU/FUEL/LP VALVE/SPLY | 2QF | M39 |
C. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 28-29-00-010-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 121VU | FUEL/L WING TK/PUMP1 SPLY | 1QA | N23 |
| 121VU | FUEL/PUMPS/1/L CTL AND R IND | 3QA | R23 |
D. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT) below the APU compartment.
(2) Open the APU access door 315AL.
(3) Remove the blanking plug (2) from the vent and drain valve (1).
(4) Install the 98A28007570000 ADAPTER - VENT AND DRAIN VALVE, APU (3) on the vent and drain valve (1).
(5) Put a CONTAINER 5 L (1.32 USGAL) below the APU vent and drain valve to collect the unwanted fuel.
4. Procedure(1) Put the ACCESS PLATFORM 3M (10 FT) below the APU compartment.
(2) Open the APU access door 315AL.
(3) Remove the blanking plug (2) from the vent and drain valve (1).
(4) Install the 98A28007570000 ADAPTER - VENT AND DRAIN VALVE, APU (3) on the vent and drain valve (1).
(5) Put a CONTAINER 5 L (1.32 USGAL) below the APU vent and drain valve to collect the unwanted fuel.
Subtask 28-29-00-710-052-A ** ON A/C NOT FOR ALL
A. Check of the APU LP Fuel Valve for evidence of internal Leakage with the left Wing Tank Pump on
Subtask 28-29-00-710-052-B ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the ECAM control panel:
| On the lower ECAM display unit:
|
2.On the FUEL overhead panel 40VU:
| On the FUEL overhead panel 40VU:
NOTE: If the FAULT legend in the L TK PUMPS 1 pushbutton switch comes on, then the pump does not operate. |
| | At the APU vent and drain valve:
NOTE: No flow of fuel is permitted. That shows that the APU fuel LP valve has no internal leakage. If fuel comes out of the vent and drain valve replace the APU fuel LP valve (Ref. AMM TASK 28-29-41-000-001) and (Ref. AMM TASK 28-29-41-400-001). |
3.On the FUEL overhead panel 40VU:
| On the FUEL overhead panel 40VU:
|
A. Check of the APU LP Fuel Valve for evidence of internal Leakage with the left Wing Tank Pump on
5. Close-up| ACTION | RESULT |
|---|---|
1.On the ECAM control panel:
| On the system display unit:
|
2.On the FUEL overhead panel 40VU:
| On the FUEL overhead panel 40VU:
NOTE: If the FAULT legend in the L TK PUMPS 1 pushbutton switch comes on, then the pump does not operate. |
| | At the APU vent and drain valve:
NOTE: No flow of fuel is permitted. That shows that the APU fuel LP valve has no internal leakage. If fuel comes out of the vent and drain valve replace the APU fuel LP valve (Ref. AMM TASK 28-29-41-000-001) and (Ref. AMM TASK 28-29-41-400-001). |
3.On the FUEL overhead panel 40VU:
| On the FUEL overhead panel 40VU:
|
Subtask 28-29-00-860-053-A
A. Put the aircraft back to its initial configuration.
(1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(2) De-energize the aircraft electrical circuits. (Ref. AMM TASK 24-41-00-862-002)
Subtask 28-29-00-410-050-A (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(2) De-energize the aircraft electrical circuits. (Ref. AMM TASK 24-41-00-862-002)
B. Close Access
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2) Remove the 98A28007570000 ADAPTER - VENT AND DRAIN VALVE, APU (3) from the vent and drain valve (1).
(3) Install the blanking plug (2) on the vent and drain valve (1).
(4) Make sure that the work area is clean and clear of tools and other items.
(5) Close the APU access door 315AL.
(6) Remove the access platform(s).
(7) Put the system back to the serviceable condition.
Subtask 28-29-00-865-055-A (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2) Remove the 98A28007570000 ADAPTER - VENT AND DRAIN VALVE, APU (3) from the vent and drain valve (1).
(3) Install the blanking plug (2) on the vent and drain valve (1).
(4) Make sure that the work area is clean and clear of tools and other items.
(5) Close the APU access door 315AL.
(6) Remove the access platform(s).
(7) Put the system back to the serviceable condition.
Adapter for Vent and Drain Valve