Disagree between the DOOR/OXY Page Indication and the Locked Position of the R Forward Passenger/Crew Door
TASK 52-11-00-810-803-A
Disagree between the DOOR/OXY Page Indication and the Locked Position of the R Forward Passenger/Crew Door
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 52-11-00-860-058-A
Subtask 52-11-00-810-064-A
Subtask 52-11-00-860-059-A
[Rev.8 from Aug 2018]
2026.04.04 04:34:43 UTC
Disagree between the DOOR/OXY Page Indication and the Locked Position of the R Forward Passenger/Crew Door
1. Possible Causes
- IND LT-SLIDE ARMED, FWD R DOOR [1WN2]
- RELAY-PWR SPLY SWITCHOVER [12WN]
- PROX SW-HANDLE, R FWD PAX/CREW DOOR [13WV2]
- PROX SW-HOOK, R FWD PAX/CREW DOOR [11WV2]
- wiring
- SDAC-1 [1WV1]
- SDAC-2 [1WV2]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 24-41-00-861-002 | Energize the Aircraft Electrical Circuits from the External Power |
| AMM 24-41-00-862-002 | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| ASM 315402 | |
| ASM 315405 | |
| AMM 31-55-34-000-001 | Removal of the SDAC |
| AMM 31-55-34-400-001 | Installation of the SDAC |
| AMM 31-60-00-860-001 | EIS Start Procedure |
| AMM 52-71-00-820-001 | Adjustment of the Proximity Switches of the Locking Hook of the Pax/Crew Doors with the CHECKING TOOL-DOOR |
| AMM 52-71-00-820-002 | Adjustment of the Proximity Switches of the Passenger/Crew Doors with the CHECKING TOOL-DOORS |
| AMM 52-71-11-000-001 | Removal of the Proximity Switches of the Passenger/Crew Doors |
| AMM 52-71-11-400-001 | Installation of the Proximity Switches of the Passenger/Crew Door |
| ASM 527301 | |
| AWM 527303 | |
| AMM 52-73-21-000-001 | Removal of the SLIDE ARMED Indicator-Light of the FWD Passenger/Crew Door |
| AMM 52-73-21-400-001 | Installation of the SLIDE ARMED Indicator-Light of the FWD Passenger/Crew Door |
Subtask 52-11-00-860-058-A
A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
Subtask 52-11-00-865-052-A (1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 52-11-00-710-058-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 121VU | EIS/SLIDES/ARM AND WARN/GND | 13WN | P10 |
C. Test
(1) Make sure that the right forward passenger/crew door is fully closed and the indicator plate shows LOCKED.
(2) On the ECAM control panel:
4. Fault Isolation(1) Make sure that the right forward passenger/crew door is fully closed and the indicator plate shows LOCKED.
(2) On the ECAM control panel:
- push the DOOR key to get the DOOR/OXY page.
- make sure that the CABIN indication comes into view amber.
Subtask 52-11-00-810-064-A
A. On the Door/Oxy page, if the CABIN indication comes into view amber:
Subtask 52-11-00-710-061-A - do a check for 6VDC between pins A and D of the handle proximity switch (13WV2) ASM 315405.
- replace the IND LT-SLIDE ARMED, FWD R DOOR [1WN2] AMM 52-73-21-000-001 and AMM 52-73-21-400-001.
- replace the RELAY-PWR SPLY SWITCHOVER [12WN] ASM 527301.
- repair the wiring as necessary.
- disconnect the connector of the handle proximity switch (13WV2)
- install the jumper wire between pins B and C of the connector (13WV2-A) ASM 315405
- do the test given in Para. 3.C.
- remove the jumper wire between pins B and C of the connector (13WV2-A)
- connect the connector of the handle proximity switch (13WV2)
- adjust the handle proximity switch (13WV2) with the door checking tool AMM 52-71-00-820-002 or with the ECAM system AMM 52-71-00-820-002.
- replace the PROX SW-HANDLE, R FWD PAX/CREW DOOR [13WV2] AMM 52-71-11-000-001 and AMM 52-71-11-400-001.
- remove the jumper wire between pins B and C of the connector (13WV2-A)
- connect the connector of the handle proximity switch (13WV2)
- do a check for 28VDC between pins A and D of the hook proximity switch (11WV2) ASM 315405.
- repair the wiring as necessary.
- disconnect the connector of the hook proximity switch (11WV2)
- install the jumper wire between pins B and C of connector (11WV2-A) ASM 315405
- do the test given in Para. 3.C.
- remove the jumper wire between pins B and C of the connector (11WV2-A)
- connect the connector of the hook proximity switch (11WV2)
- adjust the hook proximity switch (11WV2) with the door checking tool AMM 52-71-00-820-001 or with the ECAM system AMM 52-71-00-820-001.
* On the Door/Oxy page, if the CABIN indication comes into view amber: - replace the PROX SW-HOOK, R FWD PAX/CREW DOOR [11WV2] AMM 52-71-11-000-001 and AMM 52-71-11-400-001.
- remove the jumper wire between pins B and C of the connector (11WV2-A)
- connect the connector of the hook proximity switch (11WV2)
- disconnect the plug of the indicator light (1WN2)
- install the jumper wire between pins F and G of the plug 2874VC AWM 527303
- do the test given in Para. 3.C.
* On the Door/Oxy page, if the CABIN indication comes into view green: - remove the jumper wire between pins F and G of the plug 2874VC
- replace the IND LT-SLIDE ARMED, FWD R DOOR [1WN2] AMM 52-73-21-000-001 and AMM 52-73-21-400-001.
* On the Door/Oxy page, if the CABIN indication comes into view amber: - remove the jumper wire between pins F and G of the plug 2874VC
- connect the plug 2874VC to the indicator light (1WN2)
- do a check for a ground signal at pin C of the handle proximity switch (13WV2) ASM 315405.
** If there is no ground signal: - repair the wiring from the pin C of the handle proximity switch (13WV2) to the ground terminal ASM 315405.
** If there is a ground signal: - do a check of the wiring between:
*** the handle proximity switch (13WV2) pin B and the indicator light (1WN2) pin F,
*** the indicator light (1WN2) pin G and the hook proximity switch (11WV2) pin C,
*** the hook proximity switch (11WV2) pin B and the SDAC-1(2) pin AD/11G ASM 315402 and ASM 315405. - repair the wiring as necessary.
- replace the SDAC-1 [1WV1] AMM 31-55-34-000-001 and AMM 31-55-34-400-001.
- replace the SDAC-2 [1WV2] AMM 31-55-34-000-001 and AMM 31-55-34-400-001.
B. Test
(1) On the ECAM control panel:
5. Close-up(1) On the ECAM control panel:
- push the door key to get the DOOR/OXY page.
- make sure that the CABIN indication comes into view green.
Subtask 52-11-00-860-059-A
A. Put the aircraft back to its initial configuration.
(1) On the ECAM control panel, set the LOWER DISPLAY and the UPPER DISPLAY potentiometers to OFF.
(2) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
(1) On the ECAM control panel, set the LOWER DISPLAY and the UPPER DISPLAY potentiometers to OFF.
(2) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.