Operational Test of the APU-Fuel Low-Pressure Circuit ((131-9(A))
TASK 49-31-00-710-003-A
Operational Test of the APU-Fuel Low-Pressure Circuit ((131-9(A))
Self explanatory
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 49-31-00-860-056-A ** ON A/C NOT FOR ALL
Subtask 49-31-00-710-057-A ** ON A/C NOT FOR ALL
Subtask 49-31-00-410-058-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 07:33:35 UTC
Operational Test of the APU-Fuel Low-Pressure Circuit ((131-9(A))
ZONE: 210
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | STEPLADDER 2.0 M (6.6 FT) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 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 31-60-00-860-001-A | EIS Start Procedure |
| TASK 32-12-00-010-001-A | Open the Main Gear Doors for Access |
| TASK 32-12-00-410-001-A | Close the Main Gear Doors after Access |
| TASK 49-00-00-860-008-A | APU Start by External Power |
| TASK 49-00-00-860-008-A-01 | APU Start by Batteries |
| TASK 49-00-00-860-009-A | APU Shutdown by External Power (131-9(A)) |
| TASK 49-00-00-860-009-A-01 | APU Shutdown by Batteries (131-9(A)) |
Subtask 49-31-00-860-056-A ** ON A/C NOT FOR ALL
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 the R TK PUMPS pushbutton switches are released (the OFF legends are on).
Subtask 49-31-00-865-063-A ** ON A/C NOT FOR ALL (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 the R TK PUMPS pushbutton switches are released (the OFF legends are on).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 49-31-00-010-058-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FUEL/X FEED/VALVE/MOT1 | 2QE | A12 |
| 49VU | APU/FUEL/BLOW OFF/PUMP | 2QC | B14 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/FUEL/BLOW OFF/CTL | 1QC | K39 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
| 121VU | APU/FUEL/LP VALVE/CTL | 1QF | M40 |
| 121VU | APU/FUEL/LP VALVE/SPLY | 2QF | M39 |
| 121VU | APU/FUEL/PUMP/CTL | 3QC | M38 |
| 121VU | FUEL/X FEED/VALVE/MOT2 | 1QE | M24 |
| 121VU | FUEL/L WING TK/PUMP2 SPLY | 7QA | N26 |
| 121VU | FUEL/L WING TK/PUMP1 SPLY | 1QA | N23 |
| 121VU | FUEL/R WING TK/PUMP2 SPLY | 8QA | Q26 |
| 121VU | FUEL/R WING TK/PUMP1 SPLY | 2QA | Q23 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/FUEL/BLOW OFF/CTL | 1QC | P38 |
C. Get Access
(1) Open the LH main landing-gear (MLG) door (Ref. AMM TASK 32-12-00-010-001).
(2) Put the STEPLADDER 2.0 M (6.6 FT) in position at the LH MLG door.
4. Procedure(1) Open the LH main landing-gear (MLG) door (Ref. AMM TASK 32-12-00-010-001).
(2) Put the STEPLADDER 2.0 M (6.6 FT) in position at the LH MLG door.
Subtask 49-31-00-710-057-A ** ON A/C NOT FOR ALL
A. Operational Test of the APU Fuel Low Pressure Circuit
5. Close-upNOTE: You can feel with your hand when the APU fuel pump operates.
| 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:
|
| 3.Start and operate the APU (Ref. AMM TASK 49-00-00-860-008). NOTE: Operate the APU with no electric and/or pneumatic load. | At the APU fuel pump 4QC on the FR42/ZONE 140:
|
4.On the FUEL overhead panel 40VU:
| On the FUEL overhead panel 40VU:
|
| | At the APU fuel pump 4QC on the FR42/ZONE 140:
|
5.On the circuit breaker panel 49VU:
| At the APU fuel pump 4QC on the FR42/ZONE 140:
|
| | On the lower ECAM display unit:
NOTE: It is possible, that an APU AUTO SHUTDOWN occurs. |
| 6.Do the APU shutdown (Ref. AMM TASK 49-00-00-860-009). | On the lower ECAM display unit:
NOTE: The ECB (59KD) stores the fault message LOW FUEL PRESSURE CHECK APU FUEL SUPPLY (class 2). |
7.On the circuit breaker panel 49VU:
| |
8.On the APU section of the overhead panel 25VU:
| On the APU section of the overhead panel 25VU:
|
| | At the APU fuel pump 4QC on the FR42/ZONE 140:
|
9.On the APU section of the overhead panel 25VU:
| On the APU section of the overhead panel 25VU:
|
| | At the APU fuel pump 4QC on the FR42/ZONE 140:
|
Subtask 49-31-00-410-058-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the stepladder from the LH MLG door.
(3) Close the LH MLG door. (Ref. AMM TASK 32-12-00-410-001)
Subtask 49-31-00-860-057-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the stepladder from the LH MLG door.
(3) Close the LH MLG door. (Ref. AMM TASK 32-12-00-410-001)
B. 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).
(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).