Operational Test of Emergency Shutdown System (with APU SHUT OFF Switch 1KL) (131-9(A))
TASK 49-62-00-710-007-A
Operational Test of Emergency Shutdown System (with APU SHUT OFF Switch 1KL) (131-9(A))
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information
3. Job Set-up
Subtask 49-62-00-865-056-A ** ON A/C NOT FOR ALL
Subtask 49-62-00-710-058-A ** ON A/C NOT FOR ALL
Subtask 49-62-00-860-055-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 08:26:32 UTC
Operational Test of Emergency Shutdown System (with APU SHUT OFF Switch 1KL) (131-9(A))
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information
| 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 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 49-62-00-865-056-A ** ON A/C NOT FOR ALL
A. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 49-62-00-860-054-A ** ON A/C NOT FOR ALL | 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 |
B. 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).
4. Procedure(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).
Subtask 49-62-00-710-058-A ** ON A/C NOT FOR ALL
A. Operational Test of the Emergency Shutdown System
5. Close-up| ACTION | RESULT |
|---|---|
1.In the INT LT section of the overhead panel 25VU:
| In the cockpit:
|
2.In the INT LT section of the overhead panel 25VU:
| In the cockpit:
|
3.On the overhead panel 25VU:
| On the overhead panel 25VU:
|
4.On the ECAM control panel:
| On the ECAM lower display unit:
|
| | On the FUEL page of the ECAM lower display unit:
|
5.On the external power control panel 108VU:
| On the ECAM upper display unit:
|
| | On the glareshield panels 130VU and 131VU:
|
| | On the overhead panel 25VU:
|
| | On the FUEL page of the ECAM lower display unit:
|
6.On the overhead panel 25VU:
| On the overhead panel 25VU:
|
| | On the ECAM upper display unit:
|
7.On the glareshield panel 130VU or 131VU:
| On the glareshield panels 130VU and 131VU:
|
8.On the overhead panel 25VU:
| On the ECAM upper display unit:
|
9.On the overhead panel 25VU:
| On the overhead panel 25VU:
|
| | On the FUEL page of the ECAM lower display unit:
|
10.On the overhead panel 25VU:
| On the overhead panel 25VU:
|
Subtask 49-62-00-860-055-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).