Operational Test of the APU Bleed Air Supply and Crossbleed Systems
TASK 36-12-00-710-001-A
Operational Test of the APU Bleed Air Supply and Crossbleed Systems
1. Reason for the Job
To check the correct operation of the crossbleed valve indicating circuit.
2. Job Set-up Information
A. Referenced Information
3. Job Set-up
Subtask 36-12-00-865-050-A
Subtask 36-12-00-710-050-A
Subtask 36-12-00-860-050-B ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 08:09:15 UTC
Operational Test of the APU Bleed Air Supply and Crossbleed Systems
1. Reason for the Job
To check the correct operation of the crossbleed valve indicating circuit.
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 |
| TASK 49-00-00-860-005-A | APU Start by External Power |
| TASK 49-00-00-860-005-A-01 | APU Start by Batteries |
| TASK 49-00-00-860-006-A | APU Shutdown by External Power |
| TASK 49-00-00-860-006-A-01 | APU Shutdown by Batteries |
| 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 36-12-00-865-050-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 36-12-00-860-051-B ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR BLEED/ENG 1/CTL | 3HA1 | D12 |
| 49VU | AIR BLEED/ENG 1/MONG | 2HA1 | D11 |
| ** ON A/C ALL | |||
| 49VU | AIR BLEED/X FEED/VALVE/BAT | 2HV | D13 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR BLEED/ENG 2/MONG | 3HA2 | D12 |
| 49VU | AIR BLEED/ENG 1/CTL | 2HA1 | D11 |
| ** ON A/C ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR BLEED/ENG 2/CTL | 3HA2 | Z23 |
| 122VU | AIR BLEED/ENG 2/MONG | 2HA2 | Z22 |
| ** ON A/C ALL | |||
| 122VU | AIR BLEED/X FEED VALVE/NORM | 1HV | Z20 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR BLEED/ENG 1/MONG | 3HA1 | Z23 |
| 122VU | AIR BLEED/ENG 2/CTL | 2HA2 | Z22 |
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).
(3) On AIR COND panel 30VU, make sure that the OFF legends on the PACK 1 and PACK 2 pushbutton switches are on.
(4) Start the APU (Ref. AMM TASK 49-00-00-860-005).
Subtask 36-12-00-860-051-C ** 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 AIR COND panel 30VU, make sure that the OFF legends on the PACK 1 and PACK 2 pushbutton switches are on.
(4) Start the APU (Ref. AMM TASK 49-00-00-860-005).
NOTE: After the APU starts, Airbus recommends you to wait for a minimum of 3 minutes for the warm up period, before you select the APU BLEED.
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).
(3) On AIR COND panel 30VU, make sure that the OFF legends on the PACK 1 and PACK 2 pushbutton switches are on.
(4) Start the APU (Ref. AMM TASK 49-00-00-860-008).
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).
(3) On AIR COND panel 30VU, make sure that the OFF legends on the PACK 1 and PACK 2 pushbutton switches are on.
(4) Start the APU (Ref. AMM TASK 49-00-00-860-008).
NOTE: After the APU starts, Airbus recommends you to wait for a minimum of 3 minutes of warm up period before you select the APU BLEED.
Subtask 36-12-00-710-050-A
A. Operational Test of the APU Bleed Air Supply and Crossbleed System
(1) Reset of the Message on the Status Page
(b) Put the X-BLEED selector switch in the OPEN position (with the crossbleed valve in closed postion) and keep it there until the message X-BLEED MAN CTL goes out of view.
(c) Close the circuit breaker AIR/BLEED/X FEED/VALVE BAT/(2HV).
5. Close-up| ACTION | RESULT |
|---|---|
1.On the AIR COND overhead control panel 30VU:
| |
2.On the circuit breaker panel 122VU:
| |
| 3.On the AIR COND overhead control panel 30VU: | On the AIR COND overhead control panel 30VU: |
|
|
| | The APU supplies bleed air after 5 s. |
| | A single chime is heard after approximately 20 s. |
| | On the LH (131VU) and RH (130VU) glareshield:
|
| | On the upper ECAM display unit:
|
| | On the BLEED page of the lower ECAM display unit:
|
4.On the circuit breaker panel 122VU:
| On the LH (131VU) and RH (130VU) glareshield:
|
| | The crossbleed valve opens after approximately 5 s. |
| | On the upper ECAM display unit:
|
| | On the lower ECAM display unit:
|
| 5.On the ECAM control panel (ECP) 11VU: | On the ECAM control panel (ECP) 11VU: |
|
|
| | On the BLEED page the lower ECAM display unit:
|
| 6.On the AIR COND overhead control panel 30VU: | On the AIR COND overhead control panel 30VU: |
|
|
| | The APU bleed valve and the crossbleed valve close. |
| | On the BLEED page of the lower ECAM display unit:
|
| 7.On the ECAM control panel (ECP) 11VU: | On the ECAM control panel (ECP) 11VU: |
|
|
| | On the lower ECAM display unit:
|
NOTE: During the test the message X-BLEED MAN CTL comes into view on the STS page. Reset the FWC 1 and FWC 2 or do the subsequent procedure.
(a) Pull the circuit breaker AIR/BLEED/X FEED/VALVE/BAT (2HV). (b) Put the X-BLEED selector switch in the OPEN position (with the crossbleed valve in closed postion) and keep it there until the message X-BLEED MAN CTL goes out of view.
(c) Close the circuit breaker AIR/BLEED/X FEED/VALVE BAT/(2HV).
Subtask 36-12-00-860-050-B ** ON A/C NOT FOR ALL
A. Put the aircraft back to the serviceable condition.
(1) Shut down the APU (Ref. AMM TASK 49-00-00-860-006).
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 36-12-00-860-050-C ** ON A/C NOT FOR ALL (1) Shut down the APU (Ref. AMM TASK 49-00-00-860-006).
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
A. Put the aircraft back to the serviceable condition.
(1) Shut down the APU (Ref. AMM TASK 49-00-00-860-009).
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(1) Shut down the APU (Ref. AMM TASK 49-00-00-860-009).
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).