Operational Test of the Pressure Control and Monitoring
TASK 21-31-00-710-002-A
Operational Test of the Pressure Control and Monitoring
Refer to the MPD TASK: 213100-01
OPERATIONAL CHECK OF SYSTEM VIA MCDU
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 21-31-00-865-052-A
Subtask 21-31-00-710-052-B
5. Close-up
Subtask 21-31-00-860-054-A
[Rev.10 from 2021]
2026.03.31 23:04:30 UTC
Operational Test of the Pressure Control and Monitoring
WARNING:
MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE.
HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
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.
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 213100-01
OPERATIONAL CHECK OF SYSTEM VIA MCDU
2. Job Set-up Information
A. Work Zones and Access Panels
| 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 31-32-00-860-002-A | Procedure to Get Access to the SYSTEM REPORT/TEST/AIR COND Page |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TASK 34-10-00-860-002-A | ADIRS Start Procedure |
| TASK 34-10-00-860-005-A | ADIRS Stop Procedure |
Subtask 21-31-00-865-052-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 21-31-00-860-053-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | AIR COND/CAB/PRESS/CTL1 | 1HL | D09 |
| 122VU | AIR COND/CAB PRESS/CTL/MAN | 3HL | Y23 |
| 122VU | AIR COND/CAB PRESS/CTL/2 | 2HL | Y22 |
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 the ECAM control panel push the PRESS pushbutton switch, the CAB PRESS page comes into view on the lower ECAM display unit.
(4) On one MCDU get the SYSTEM REPORT/TEST AIR COND menu page (Ref. AMM TASK 31-32-00-860-002).
(5) On the AIR COND panel 30VU, make sure that:
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 the ECAM control panel push the PRESS pushbutton switch, the CAB PRESS page comes into view on the lower ECAM display unit.
(4) On one MCDU get the SYSTEM REPORT/TEST AIR COND menu page (Ref. AMM TASK 31-32-00-860-002).
(5) On the AIR COND panel 30VU, make sure that:
- the PACK 1 and the PACK 2 pushbutton switches are in the off position (the OFF legends are on).
- the RAM AIR pushbutton switch is in the off position (the ON legend is off).
- the MODE SEL pushbutton switch is in the AUTO configuration (with the FAULT and MAN legends off).
- the LDG ELEV selector is in the AUTO position.
- the DITCHING pushbutton switch is in the AUTO configuration (with the ON legend off).
Subtask 21-31-00-710-052-B
WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE OUTFLOW VALVES ARE CLEAR. MOVEMENT OF THE OUTFLOW VALVES CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
A. Operational Test of the Pressure Control and Monitoring | ACTION | RESULT |
|---|---|
1.On the MCDU SYSTEM REPORT/TEST AIR COND menu page:
| On the MCDU:
NOTE: If the CAB PRESS CONT 1 page does not show do a reset of CPC1 and CPC2 two times: For the reset of the CPCs the subsequent circuit breakers must be opened for at least 10 seconds: - for the CPC 1, the circuit breaker 1HL which is installed on the circuit breaker panel 49VU, - for the CPC 2, the circuit breaker 2HL which is installed on the circuit breaker panel 122VU. |
2.On the MCDU CAB PRESS CONT 1 menu page:
| On the MCDU:
|
3.On the CABIN PRESS panel 25VU:
| On the ECAM upper display unit:
|
| | On the ECAM lower display unit:
|
4.On the MCDU CAB PRESS CONT 1 TEST/CALIBRATION menu page:
| On the MCDU:
NOTE: In case of interruption by a power-supply transient the test may be aborted. If TEST OK or TEST FAIL is not confirmed, the test should be repeated. |
NOTE: Do the test again for CPC 2.
Subtask 21-31-00-860-054-A
A. Aircraft Maintenance Configuration
(1) On the CABIN PRESS panel 25VU, set the LDG ELEV selector to AUTO.
(2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(4) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) On the CABIN PRESS panel 25VU, set the LDG ELEV selector to AUTO.
(2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(4) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).