APU No Load Operation (131-9(A))
TASK 49-00-00-860-809-A
APU No Load Operation (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 49-00-00-941-087-A ** ON A/C NOT FOR ALL
Subtask 49-00-00-860-183-A ** ON A/C NOT FOR ALL
Subtask 49-00-00-860-184-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 01:25:47 UTC
APU No Load Operation (131-9(A))
WARNING:
MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN WITH A WARNING PLACARD ATTACHED TO IT.
THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT.
WARNING:
DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS WHEN YOU DO THE MAINTENANCE TASK(S).
WARNING:
WHILE THE APU OPERATES, DO NOT GO INTO THESE AREAS:
- THE AREA BEHIND THE APU EXHAUST DUCT: 25m (82ft.) REARWARD OF THE DUCT, MORE THAN 3m (10ft.) ABOVE THE GROUND, AND THE WIDTH OF THE HORIZONTAL STABILIZER
- THE AREA AROUND THE APU AIR-INTAKE: 2m (7ft) AROUND THE INTAKE
- THE AREA OF THE OIL-COOLER OUTLET.
CAUTION:
DO NOT START OR TRY TO START THE APU MORE THAN THREE TIMES, ONE AFTER THE OTHER. AFTER THE THIRD TIME, THERE MUST BE A MINIMUM OF ONE HOUR BEFORE YOU START OR TRY TO START THE APU AGAIN. THIS MAKES SURE THAT THE TEMPERATURE OF THE STARTER MOTOR DECREASES SUFFICIENTLY.
CAUTION:
DO NOT TRY TO START THE APU AGAIN DURING A REFUEL/DEFUEL PROCEDURE AFTER AN AUTOMATIC SHUTDOWN OR FAILED APU START. IF YOU DO, THERE IS A RISK OF INJURY AND/OR DAMAGE.
CAUTION:
OBEY THE SAFETY PRECAUTIONS.
CAUTION:
DO NOT USE THE APU DURING FLUID DE-ICING OPERATIONS. DE-ICING FLUID CAN CONTAMINATE THE INSIDE OF THE APU.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 811 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 23-44-00-860-001-A | Operation of the Service Interphone System |
| TASK 24-42-00-861-001-A | Energize the Ground Service Network from the External Power |
| TASK 24-42-00-862-001-A | De-energize the Ground Service Network Supplied from the External Power |
| TASK 26-22-00-710-001-A | Operational Test of the APU Fire-Extinguishing Loop/Squib |
| TASK 29-00-00-864-001-A | Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action |
| TASK 31-32-00-860-001-A | Procedure to Get Access to the SYSTEM REPORT/TEST Menu Page |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 49-00-00-710-009-A | Self-Test of the ECB |
| TASK 52-41-00-010-002-A | Open the Avionics Compartment Doors for Access |
| TASK 52-41-00-410-001-A | Close the APU Doors after Access |
| TASK 52-41-00-410-002-A | Close the Avionics Compartment Doors after Access |
Subtask 49-00-00-941-087-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) Make sure that the danger areas are clear of persons and/or equipment.
(2) Make sure that APU access doors 315AL and 316AR are closed (Ref. AMM TASK 52-41-00-410-001).
(3) If an emergency or a malfunction occurs during operation of the APU, do the emergency shutdown procedure immediately. You can start the emergency shutdown from:
Subtask 49-00-00-860-182-A ** ON A/C NOT FOR ALL (1) Make sure that the danger areas are clear of persons and/or equipment.
(2) Make sure that APU access doors 315AL and 316AR are closed (Ref. AMM TASK 52-41-00-410-001).
(3) If an emergency or a malfunction occurs during operation of the APU, do the emergency shutdown procedure immediately. You can start the emergency shutdown from:
- The APU FIRE PUSH pushbutton switch on the panel 20VU.
- The APU SHUT OFF pushbutton switch on the panel 108VU.
NOTE: Do the emergency shutdown immediately if fire, smoke, unusual noise, fuel or oil leakage occurs.
B. Aircraft Maintenance Configuration
(1) Open the access door 811 (Ref. AMM TASK 52-41-00-010-002).
(2) Put the WARNING NOTICE(S) in position on the opened access door 811 which tells persons not to close the door.
(3) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
(a) On the ELEC section on the panel 35VU:
(5) Depressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-00-00-864-001).
(6) Make a service interphone connection from the cockpit to the APU compartment area (Ref. AMM TASK 23-44-00-860-001).
(7) On the AIR COND section of the panel 30VU:
(Ref. AMM TASK 31-60-00-860-001).
(a) On the ECAM control panel, push the APU pushbutton switch (on the lower ECAM DU, the APU page comes on).
(10) Make sure that the APU fire and overheat detection system and the APU fire extinguishing system are operational (Ref. AMM TASK 26-22-00-710-001).
(11) Remove the APU air intake and exhaust blanking plugs.
(12) If not required during operation of the APU, remove the ground support equipment, the special and standard tools and all other items.
(13) Do the ECB self test (Ref. AMM TASK 49-00-00-710-009).
(14) Get access to the APU menu page in SYSTEM REPORT/TEST (Ref. AMM TASK 31-32-00-860-001).
(a) Push the line key adjacent to the GND SCANNING indication.
Subtask 49-00-00-865-183-A ** ON A/C NOT FOR ALL (1) Open the access door 811 (Ref. AMM TASK 52-41-00-010-002).
(2) Put the WARNING NOTICE(S) in position on the opened access door 811 which tells persons not to close the door.
(3) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
(a) On the ELEC section on the panel 35VU:
- Make sure that the BAT 1 and BAT 2 pushbutton switches are in the auto position (the ON and FAULT legends are OFF).
(5) Depressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-00-00-864-001).
(6) Make a service interphone connection from the cockpit to the APU compartment area (Ref. AMM TASK 23-44-00-860-001).
(7) On the AIR COND section of the panel 30VU:
- Make sure that the APU BLEED pushbutton switch is in the OFF position (the ON and FAULT legends are off).
- Make sure that the X BLEED selector switch is in the AUTO position.
- Make sure that both ENG MASTER control switches are in the OFF position.
(Ref. AMM TASK 31-60-00-860-001).
(a) On the ECAM control panel, push the APU pushbutton switch (on the lower ECAM DU, the APU page comes on).
(10) Make sure that the APU fire and overheat detection system and the APU fire extinguishing system are operational (Ref. AMM TASK 26-22-00-710-001).
(11) Remove the APU air intake and exhaust blanking plugs.
(12) If not required during operation of the APU, remove the ground support equipment, the special and standard tools and all other items.
(13) Do the ECB self test (Ref. AMM TASK 49-00-00-710-009).
(14) Get access to the APU menu page in SYSTEM REPORT/TEST (Ref. AMM TASK 31-32-00-860-001).
(a) Push the line key adjacent to the GND SCANNING indication.
- Keep the GND SCANNING active during the APU no load operation.
C. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 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/FIRE AND OVHT/DET/LOOP B | 2WG | L44 |
| 121VU | APU/FIRE AND OVHT/DET/LOOP A | 1WG | L43 |
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
| 121VU | APU/FIRE/EXTIG/SQUIB/B | 2WF | L39 |
| 121VU | APU/FIRE/EXTIG/SQUIB/A | 1WF | L38 |
| 121VU | APU/FIRE/LP VALVE/NORM | 4WF | M42 |
| 121VU | APU/FIRE/LP VALVE/STBY | 3WF | M41 |
| 121VU | APU/FUEL/LP VALVE/CTL | 1QF | M40 |
| 121VU | APU/FUEL/LP VALVE/SPLY | 2QF | M39 |
| 121VU | APU/FUEL/PUMP/CTL | 3QC | M38 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/FUEL/BLOW OFF/CTL | 1QC | P38 |
Subtask 49-00-00-860-183-A ** ON A/C NOT FOR ALL
A. APU No Load Operation
(1) On the GND SCANNING menu page make sure that no faults have occurred during the APU no load operation.
Subtask 49-00-00-860-183-B ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On panel 35VU:
| On panel 35 VU:
NOTE: If the battery voltage is less than 25.5V, a battery charging-cycle of approximately 20 minutes is required. |
2.On panel 11VU:
| On ECAM panel display:
|
3.On panel 25VU:
| On panel 25VU:
NOTE: The MASTER SW FAULT legend could come on if the Battery Charge Limiter does a power-up test after A/C power loss. Wait 45 seconds, recycle the APU MASTER SW then continue with the start sequence. |
4.On panel 25VU:
| On panel 25VU:
|
5.On the lower ECAM display:
| On the lower ECAM display:
|
|
|
| On panel 25VU:
|
| 6.Operate the APU at Ready to Load (RTL) condition. | On the lower ECAM display:
|
7.On panel 25VU:
| On panel 25VU:
|
| | On the lower ECAM display:
NOTE: You must wait 2 minutes after the AVAIL legend goes off before you select BAT 1 and BAT 2 to the OFF position. This gives sufficient time for the air intake to fully close. |
A. APU No Load Operation
(1) On the GND SCANNING menu page make sure that no faults have occurred during the APU no load operation.
5. Close-up| ACTION | RESULT |
|---|---|
1.On panel 35VU:
| On panel 35 VU:
NOTE: If the battery voltage is less than 25.5V, a battery charging-cycle of approximately 20 minutes is required. |
2.On panel 11VU:
| On ECAM panel display:
|
3.On panel 25VU:
| On panel 25VU:
NOTE: The MASTER SW FAULT legend could come on if the Battery Charge Limiter does a power-up test after A/C power loss. Wait 45 seconds, recycle the APU MASTER SW then continue with the start sequence. |
4.On panel 25VU:
| On panel 25VU:
|
5.On the lower ECAM display:
| On the lower ECAM display:
|
|
|
| On panel 25VU:
|
| 6.Operate the APU at Ready to Load (RTL) condition. | On the lower ECAM display:
|
7.On panel 25VU:
| On panel 25VU:
|
| | On the lower ECAM display:
NOTE: You must wait 2 minutes after the AVAIL legend goes off before you select BAT 1 and BAT 2 to the OFF position. This gives sufficient time for the air intake to fully close. |
Subtask 49-00-00-860-184-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) On the MCDU 1(2):
(3) De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
(4) Make sure that the work area is clean and clear of tools and other items.
(5) Remove the WARNING NOTICE(S).
(6) Close the access door 811 (Ref. AMM TASK 52-41-00-410-002).
(7) Put the aircraft back to its initial configuration.
(1) On the MCDU 1(2):
- Push the line key adjacent to the RETURN indication until the MCDU MENU page comes on.
- Set the BRT knob to off.
(3) De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
(4) Make sure that the work area is clean and clear of tools and other items.
(5) Remove the WARNING NOTICE(S).
(6) Close the access door 811 (Ref. AMM TASK 52-41-00-410-002).
(7) Put the aircraft back to its initial configuration.