Verification Test of the Automatic Cabin-Pressure Control-Systems
TASK 21-31-00-040-002-A
Verification Test of the Automatic Cabin-Pressure Control-Systems
MMEL 21-31-02A
MANUAL CABIN PRESSURE CONTROL SYSTEM (MAN V/S CTL SELECTOR, OUTFLOW VALVE MAN CHANNEL)
2. Job Set-up Information
A. Referenced Information
3. Job Set-up
Subtask 21-31-00-865-062-A
Subtask 21-31-00-710-065-B
(1) Make sure that both automatic pressure control systems are operative.
(2) Put a tag in the cockpit to tell the flight crew that the manual pressure control system is inoperative.
(3) Make an entry in the aircraft technical logbook.
5. Close-up
Subtask 21-31-00-860-064-A
[Rev.10 from 2021]
2026.04.02 06:11:13 UTC
Verification Test of the Automatic Cabin-Pressure Control-Systems
Task Summary
1. Reason for the Job| Access | Test | Specific Tools | Mhr | E/T | Nb Men |
|---|---|---|---|---|---|
| NO | NO | NO | 0.5 | 0.5 | 1 |
MMEL 21-31-02A
MANUAL CABIN PRESSURE CONTROL SYSTEM (MAN V/S CTL SELECTOR, OUTFLOW VALVE MAN CHANNEL)
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 31-32-00-860-002-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 21-31-00-865-062-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 21-31-00-860-063-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 21-31-00-710-065-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:
|
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, the CAB PRESS CONT 1 TEST/CALIBRATION menu page shows: IN PROGRESS (20...90S) comes on, then the message TEST OKAY RESET LFES - > AUTO comes on. NOTE: Do the test again for CPC 2. |
(2) Put a tag in the cockpit to tell the flight crew that the manual pressure control system is inoperative.
(3) Make an entry in the aircraft technical logbook.
Subtask 21-31-00-860-064-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).