Operational Test of the Automatic Function of the Cabin Signs in Case of Excessive Altitude
TASK 23-73-00-710-804-A
Operational Test of the Automatic Function of the Cabin Signs in Case of Excessive Altitude
Self explanatory
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 23-73-00-860-220-A ** ON A/C NOT FOR ALL
Subtask 23-73-00-710-357-A ** ON A/C NOT FOR ALL
Subtask 23-73-00-710-357-B ** ON A/C NOT FOR ALL
5. Close-up
Subtask 23-73-00-865-270-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:12:28 UTC
Operational Test of the Automatic Function of the Cabin Signs in Case of Excessive Altitude
ZONE: 200
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 200 | UPPER HALF FUSELAGE |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 23-73-00-860-003-A | Cabin Zones Programming |
| TASK 23-73-00-861-001-A | Energize the Cabin Intercommunication Data System (CIDS) |
| 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 |
Subtask 23-73-00-860-220-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) Make sure that the Cabin Intercommunication Data System (CIDS) is energized (Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) On the ECAM control panel push the PRESS pushbutton switch, the CAB PRESS page comes into view on the lower ECAM display unit.
(5) On AIR COND panel 30VU, make sure that:
(8) Make sure that the A/C is not in a NON SMOKER configuration and a NO SMOKING area is not programmed, if applicable (Ref. AMM TASK 23-73-00-860-003).
Subtask 23-73-00-865-268-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized (Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) On the ECAM control panel push the PRESS pushbutton switch, the CAB PRESS page comes into view on the lower ECAM display unit.
(5) On 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 position (the FAULT and MAN legends are off).
- The LDG ELEV selector is in the AUTO position.
- The DITCHING pushbutton switch is in the AUTO position (the ON legend is off).
(8) Make sure that the A/C is not in a NON SMOKER configuration and a NO SMOKING area is not programmed, if applicable (Ref. AMM TASK 23-73-00-860-003).
NOTE: The Non Smoker Section (NSS) signs come on together with the No Smoking (NS) signs.
(9) Make sure that there are no persons near the Outflow Valve (OFV) before you start this test. B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 23-73-00-865-269-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| 49VU | AIR COND/CAB/PRESS/CTL1 | 1HL | D09 |
| 49VU | FWS/FWC1/SPLY | 3WW | F01 |
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | EIS/FWC2/SPLY | 2WW | Q07 |
| 122VU | AIR COND/CAB PRESS/CTL/MAN | 3HL | Y23 |
| 122VU | AIR COND/CAB PRESS/CTL/2 | 2HL | Y22 |
C. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | RPCU | 4HL | X23 |
Subtask 23-73-00-710-357-A ** ON A/C NOT FOR ALL
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. Do the Test of the Automatic Function of the Cabin Signs in Case of Excessive Cabin Altitude NOTE: The No Mobile signs in the cabin stay permanently on.
| ACTION | RESULT |
|---|---|
1.On CABIN PRESS panel 25VU:
| On the ECAM upper display unit:
|
| | On the ECAM lower display unit:
NOTE: The actual manual altitude indication depends on the LDG ELEV selector position. |
2.On CABIN PRESS panel 25VU:
| On CABIN PRESS panel 25VU:
NOTE: The accuracy of the cabin altitude indication in MAN mode is +/- 1100 ft. |
| | On the ECAM lower display unit:
|
| | In the cabin:
NOTE: The FSB signs operation is related to the Cabin Assignment Module (CAM) configuration.
NOTE: The NS signs operation is related to the CAM configuration. In the cabin and in the lavatories:
NOTE: You can hear the emergency announcement only if it is recorded on the Prerecorded Announcement and Boarding Music (PRAM).
NOTE: You can hear a LO chime only if no emergency announcement is recorded on PRAM. In the lavatories:
NOTE: The ECAM message "NO SMOKING" comes into view only if NS signs are installed.
|
3.On CABIN PRESS panel 25VU:
| On CABIN PRESS panel 25VU:
|
| | On the ECAM lower display unit:
|
4.On CABIN PRESS panel 25VU:
| On the ECAM upper display unit:
|
| | On the ECAM lower display unit:
|
| | In the cabin:
NOTE: The ECAM message "NO SMOKING" goes out of view only if NS signs are installed.
|
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.
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. Do the Test of the Automatic Function of the Cabin Signs in Case of Excessive Cabin Altitude NOTE: The No Mobile signs in the cabin stay permanently on.
| ACTION | RESULT |
|---|---|
1.On CABIN PRESS panel 25VU:
| On the ECAM upper display unit:
|
| | On the ECAM lower display unit:
NOTE: The actual manual altitude indication depends on the LDG ELEV selector position. |
2.On CABIN PRESS panel 25VU:
| On CABIN PRESS panel 25VU:
NOTE: The accuracy of the cabin altitude indication in MAN mode is +/- 1100 ft. |
| | On the ECAM lower display unit:
|
| | In the cabin:
NOTE: The FSB signs operation is related to the Cabin Assignment Module (CAM) configuration.
NOTE: The NS signs operation is related to the CAM configuration. In the cabin and in the lavatories:
|
3.On CABIN PRESS panel 25VU:
| On CABIN PRESS panel 25VU:
|
| | On the ECAM lower display unit:
|
4.On CABIN PRESS panel 25VU:
| On the ECAM upper display unit:
|
| | On the ECAM lower display unit:
|
| | In the cabin:
|
Subtask 23-73-00-865-270-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 23-73-00-860-221-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | RPCU | 4HL | X23 |
B. Aircraft Maintenance 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).