Operational Check of all Pressure Sensing Channels for Rapid Decompression
TASK 52-51-00-720-002-A
Operational Check of all Pressure Sensing Channels for Rapid Decompression
Refer to the MPD TASK: 525111-02
OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS FOR RAPID DECOMPRESSION.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 52-51-00-860-066-A
Subtask 52-51-00-720-052-A
Subtask 52-51-00-860-067-A
[Rev.10 from 2021]
2026.04.02 06:28:23 UTC
Operational Check of all Pressure Sensing Channels for Rapid Decompression
ZONE: 220
1. Reason for the JobRefer to the MPD TASK: 525111-02
OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS FOR RAPID DECOMPRESSION.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | DECOMPRESSION TEST SIMULATOR |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 220 | FWD CAB UTILITY AREAS |
| 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) |
Subtask 52-51-00-860-066-A
A. Aircraft Maintenance Configuration
(1) Make sure that the cockpit door is closed.
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 52-51-00-865-060-A (1) Make sure that the cockpit door is closed.
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 122VU | DOORS/PAX/MONG | 1MQ | T13 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | DOORS CKPT LOCK | 1MQ | T13 |
| 122VU | COCKPIT DOOR LOCK SYSTEM | 1MQ | T13 |
Subtask 52-51-00-720-052-A
A. Functional Test of the Decompression Event
(1) Do the test to make sure that the pressure sensors in the control unit 24MQ operate correctly.
5. Close-up(1) Do the test to make sure that the pressure sensors in the control unit 24MQ operate correctly.
NOTE: In this test a rapid decompression of the cabin pressure is simulated with the DECOMPRESSION TEST SIMULATOR (referred to as vacuum pump).
AIRBUS recommends the use of P/N AR 4728-1 (manufacturer ADAMS RITE AEROSPACE) or the equivalent standard.
AIRBUS recommends the use of P/N AR 4728-1 (manufacturer ADAMS RITE AEROSPACE) or the equivalent standard.
| ACTION | RESULT |
|---|---|
| 1.On the CKPT DOOR CONT Panel 20VU: | On the CKPT DOOR CONT panel 20VU: |
| On the Cockpit Door:
|
|
|
| On the Cockpit Door:
|
|
|
Subtask 52-51-00-860-067-A
A. Put the aircraft back to the serviceable condition.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).