Operational Test of the APU Fire-Extinguishing Loop/Squib
TASK 26-22-00-710-001-A
Operational Test of the APU Fire-Extinguishing Loop/Squib
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 26-22-00-860-050-A
Subtask 26-22-00-875-050-A ** ON A/C NOT FOR ALL
Subtask 26-22-00-860-051-A
[Rev.10 from 2021]
2026.03.31 23:45:29 UTC
Operational Test of the APU Fire-Extinguishing Loop/Squib
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| 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 |
| TASK 33-14-00-710-001-A | Operational Check of the Light Test System |
Subtask 26-22-00-860-050-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) Do the operational test of the annunciator light test system in the cockpit (Ref. AMM TASK 33-14-00-710-001).
Subtask 26-22-00-865-053-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) Do the operational test of the annunciator light test system in the cockpit (Ref. AMM TASK 33-14-00-710-001).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 121VU | APU/FIRE AND OVHT/DET/LOOP B | 2WG | L44 |
| 121VU | APU/FIRE AND OVHT/DET/LOOP A | 1WG | L43 |
| 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 |
Subtask 26-22-00-875-050-A ** ON A/C NOT FOR ALL
A. Open, safety and tag this(these) circuit breaker(s):
Subtask 26-22-00-710-052-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/AUTO/EXTIG/GND/TEST | 30WF | L40 |
B. Operational Test of the APU Fire-Extinguishing Loop/Squib
Subtask 26-22-00-710-052-B ** ON A/C NOT FOR ALL - Make sure that circuit breaker APU AUTO EXTIG GND TEST 30WF (L40) on panel 121VU is open.
NOTE: You can open circuit breaker APU AUTO EXTIG GND TEST 30WF (L40) to prevent an unwanted automatic fire-extinguisher discharge during the test.
| ACTION | RESULT |
|---|---|
WARNING:
DO NOT PUSH THE APU FIRE/TEST PUSHBUTTON SWITCH FOR MORE THAN 3 SECONDS. IF YOU PUSH IT FOR MORE THAN 3 SECONDS, THERE IS A RISK THAT IT WILL CAUSE THE DISCHARGE OF THE APU FIRE-EXTINGUISHER BOTTLE. 1.On APU FIRE panel 20VU:
| On APU FIRE panel 20VU:
|
| | On glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
2.On APU FIRE panel 20VU:
| On APU FIRE panel 20VU:
|
| | On glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
B. Operational Test of the APU Fire-Extinguishing Loop/Squib
Subtask 26-22-00-875-051-A ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
WARNING:
DO NOT PUSH THE APU FIRE/TEST PUSHBUTTON SWITCH FOR MORE THAN 3 SECONDS. IF YOU PUSH IT FOR MORE THAN 3 SECONDS, THERE IS A RISK THAT IT WILL CAUSE THE DISCHARGE OF THE APU FIRE-EXTINGUISHER BOTTLE. 1.On APU FIRE panel 20VU:
| On APU FIRE panel 20VU:
|
| | On glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
2.On APU FIRE panel 20VU:
| On APU FIRE panel 20VU:
|
| | On glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
5. Close-up| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/AUTO/EXTIG/GND/TEST | 30WF | L40 |
Subtask 26-22-00-860-051-A
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).