Functional Check of Low Pressure Switch
TASK 35-12-00-710-001-A
Functional Check of Low Pressure Switch
Refer to the MPD TASK: 351351-01
FUNCTIONAL CHECK OF LOW PRESSURE SWITCH
To do a check of the low-pressure oxygen-supply solenoid-valve (in closing mode) and the low pressure indicator.
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 35-12-00-860-050-A ** ON A/C NOT FOR ALL
Subtask 35-12-00-710-050-C ** ON A/C NOT FOR ALL
Subtask 35-12-00-860-051-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 01:04:07 UTC
Functional Check of Low Pressure Switch
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 351351-01
FUNCTIONAL CHECK OF LOW PRESSURE SWITCH
To do a check of the low-pressure oxygen-supply solenoid-valve (in closing mode) and the low pressure indicator.
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 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TSM 35-10-00-810-801 | Loss of the Oxygen Pressure Indication on the DOOR/OXY Page |
| TSM 35-10-00-810-811 | Crew Oxygen Pressure Indication with Amber Pressure Value and Amber Half Box on the DOOR/OXY Page |
| TSM 35-10-00-810-820 | REGUL LO PR Indication with no Oxygen Pressure Value on the DOOR/OXY Page |
| TSM 35-10-00-810-828 | Loss of the REGUL LO PR Indication |
Subtask 35-12-00-860-050-A ** ON A/C NOT FOR ALL
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).
Subtask 35-12-00-865-050-A ** 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).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | OXYGEN/CREW/OXY/SPLY | 1HT | HA01 |
Subtask 35-12-00-710-050-C ** ON A/C NOT FOR ALL
A. Functional Check
(1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure (Ref. AMM TASK 35-10-00-810-801).
(3) Do the test that follows:
Subtask 35-12-00-710-050-G ** ON A/C NOT FOR ALL (1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
NOTE: If the DOOR/OXY page is not shown, the aircraft system is unserviceable.
(a) If the DOOR/OXY page is not shown:- On the center pedestal, on the ECAM control panel, push the DOOR key (the DOOR/OXY page comes into view).
NOTE: If the pressure is less than 1500 psi (103.42 bar), an amber half-box (advisory) is shown only for information.
(a) If the HP oxygen pressure is less than 400 psi (27.58 bar), do not do the test that follows but do the troubleshooting procedure (Ref. AMM D/O 35-10-00-81).(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure (Ref. AMM TASK 35-10-00-810-801).
(3) Do the test that follows:
| ACTION | RESULT |
|---|---|
1.On panel 21VU:
| On the DOOR/OXY page:
|
2.On panel 21VU:
| On the DOOR/OXY page:
|
3.In the cockpit, on one of the oxygen-mask stowage boxes:
| On the DOOR/OXY page:
|
4.On panel 21VU:
| On the DOOR/OXY page:
|
5.On panel 21VU:
|
|
A. Functional Check
(1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
(a) If the DOOR/OXY page is not shown, the aircraft system is unserviceable.
(b) If the DOOR/OXY page is not shown:
(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure TSM 35-10-00-810-801 or TSM 35-10-00-810-820.
(3) Do the test that follows:
Subtask 35-12-00-710-050-H ** ON A/C NOT FOR ALL (1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
(a) If the DOOR/OXY page is not shown, the aircraft system is unserviceable.
(b) If the DOOR/OXY page is not shown:
- On the center pedestal, on the lower ECAM DU, push the DOOR key (the DOOR/OXY page comes into view).
NOTE: If the pressure is less than 1500 psi (103.42 bar), an amber half-box (advisory) is shown only for information.
(a) If the HP oxygen pressure is less than 400 psi (27.58 bar), do not do the test that follows but do the troubleshooting procedure TSM 35-10-00-810-811. (b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure TSM 35-10-00-810-801 or TSM 35-10-00-810-820.
(3) Do the test that follows:
| ACTION | RESULT |
|---|---|
1.On the OXYGEN section of overhead control and indicating panel 21VU:
| The OFF legend goes off. On the DOOR/OXY page:
|
2.On the OXYGEN section of overhead control and indicating panel 21VU:
| The OFF legend comes on. On the DOOR/OXY page:
|
3.In the cockpit, on one of the oxygen-mask stowage boxes:
| On the DOOR/OXY page:
If the REGUL LO PR indication does not come into view on the DOOR/OXY page and/or if the volume of the sound of the oxygen flow does not stop:
|
4.On the OXYGEN section of overhead control and indicating panel 21VU:
| The OFF legend goes off. On the DOOR/OXY page:
|
5.On the OXYGEN section of overhead control and indicating panel 21VU:
| The OFF legend comes on. |
A. Functional Check
(1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure (Ref. AMM TASK 35-10-00-810-801).
(3) Do the test that follows:
Subtask 35-12-00-710-050-I ** ON A/C NOT FOR ALL (1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
NOTE: If the DOOR/OXY page is not shown, the aircraft system is unserviceable.
(a) If the DOOR/OXY page is not shown:- On the center pedestal, on the ECAM control panel, push the DOOR key (the DOOR/OXY page comes into view).
NOTE: If the pressure in one or two oxygen cylinder(s) is less than 800 psi (55.16 bar), an amber half-box (advisory) is shown only for information.
(a) If the HP oxygen pressure is less than 200 psi (13.79 bar), do not do the test that follows but do the troubleshooting procedure (Ref. AMM D/O 35-10-00-81).(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure (Ref. AMM TASK 35-10-00-810-801).
(3) Do the test that follows:
| ACTION | RESULT |
|---|---|
1.In the cockpit, on the OXYGEN section of overhead control and indicating panel 21VU:
| On the DOOR/OXY page:
|
2.In the cockpit, on the OXYGEN section of overhead control and indicating panel 21VU:
| On the DOOR/OXY page:
|
3.In the cockpit, on one of the oxygen-mask stowage boxes:
When the flow rate indicator is black and you do not hear the sound of the oxygen flow:
| On the DOOR/OXY page:
|
4.In the cockpit, on the OXYGEN section of overhead control and indicating panel 21VU:
| On the DOOR/OXY page:
|
5.In the cockpit, on the OXYGEN section of overhead control and indicating panel 21VU:
| On the DOOR/OXY page:
|
6.In the cockpit, on one of the oxygen-mask stowage boxes:
When the flow rate indicator is black and you do not hear the sound of the oxygen flow:
| On the DOOR/OXY page:
|
7.In the cockpit, on the OXYGEN section of overhead control and indicating panel 21VU:
| On the DOOR/OXY page:
|
8.In the cockpit, on the OXYGEN section of overhead control and indicating panel 21VU:
| On the DOOR/OXY page:
|
9.In the cockpit, on the captain and first-officer oxygen-mask stowage-boxes:
| On the DOOR/OXY page:
|
10.In the cockpit, on the OXYGEN section of the overhead control and indicating panel 21VU:
| On the DOOR/OXY page:
|
11.In the cockpit, on the OXYGEN section of overhead control and indicating panel 21VU:
|
|
A. Functional Check
(1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure (Ref. AMM TASK 35-10-00-810-801).
(3) Do the test that follows:
Subtask 35-12-00-710-050-J ** ON A/C NOT FOR ALL (1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
NOTE: If the DOOR/OXY page is not shown, the aircraft system is unserviceable.
(a) If the DOOR/OXY page is not shown:- On the center pedestal, on the ECAM control panel, push the DOOR key (the DOOR/OXY page comes into view).
NOTE: If the pressure is less than 1000 psi (68.95 bar), an amber half-box (advisory) is shown only for information.
(a) If the HP oxygen pressure is less than 400 psi (27.58 bar), do not do the test that follows but do the troubleshooting procedure (Ref. AMM D/O 35-10-00-81).(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure (Ref. AMM TASK 35-10-00-810-801).
(3) Do the test that follows:
| ACTION | RESULT |
|---|---|
1.On the OXYGEN section of overhead control and indicating panel 21VU:
| On the OXYGEN/CREW SUPPLY pushbutton switch:
|
2.On the OXYGEN section of overhead control and indicating panel 21VU:
| On the OXYGEN/CREW SUPPLY pushbutton switch:
|
3.In the cockpit, on one of the oxygen-mask stowage boxes:
| On the DOOR/OXY page:
|
4.On the OXYGEN section of overhead control and indicating panel 21VU:
| On the OXYGEN/CREW SUPPLY pushbutton switch:
|
5.On the OXYGEN section of overhead control and indicating panel 21VU:
| On the OXYGEN/CREW SUPPLY pushbutton switch:
|
A. Functional Check
(1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure (Ref. AMM TASK 35-10-00-810-801).
(3) Do the test that follows:
5. Close-up(1) On the center pedestal, on the lower ECAM display unit, the DOOR/OXY page is shown automatically:
NOTE: If the DOOR/OXY page is not shown, the aircraft system is unserviceable.
(a) If the DOOR/OXY page is not shown:- On the center pedestal, on the ECAM control panel, push the DOOR key (the DOOR/OXY page comes into view).
NOTE: If the pressure is less than 1000 psi (68.95 bar), an amber half-box (advisory) is shown only for information.
(a) If the HP oxygen pressure is less than 400 psi (27.58 bar), do not do the test that follows but do the troubleshooting procedure (Ref. AMM D/O 35-10-00-81).(b) If the HP oxygen pressure is not available, do not do the test that follows (the amber crosses show that the oxygen pressure information is not available: XXXXPSI) but do the troubleshooting procedure (Ref. AMM TASK 35-10-00-810-801).
(3) Do the test that follows:
| ACTION | RESULT |
|---|---|
1.On panel 21VU:
| On the DOOR/OXY page:
|
2.On panel 21VU:
| On the DOOR/OXY page:
|
3.In the cockpit, on one of the oxygen-mask stowage boxes:
| On the DOOR/OXY page:
|
4.On panel 21VU:
| On the DOOR/OXY page:
|
5.On panel 21VU:
|
|
Subtask 35-12-00-860-051-A ** ON A/C NOT FOR ALL
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).