No SLIDE Indication on the DOOR/OXY Page when the L Aft Escape Slide Handle is in the SLIDE ARMED Position
TASK 52-13-00-810-806-A
No SLIDE Indication on the DOOR/OXY Page when the L Aft Escape Slide Handle is in the SLIDE ARMED Position
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 52-13-00-860-064-A
Subtask 52-13-00-810-067-A
Subtask 52-13-00-860-065-A
[Rev.8 from Aug 2018]
2026.04.04 04:34:46 UTC
No SLIDE Indication on the DOOR/OXY Page when the L Aft Escape Slide Handle is in the SLIDE ARMED Position
1. Possible Causes
- IND LT-SLIDE ARMED, AFT L DOOR [3WN1]
- IND LT-SLIDE ARMED, L EMER EXIT [2WN1]
- IND LT-SLIDE ARMED, FWD L DOOR [1WN1]
- RELAY-PWR SPLY SWITCHOVER [12WN]
wiring from the connector (7WN1-A) to the indicator light (3WN1) wiring from the indicator light (3WN1) to the SDAC-1(2) (1WV1(2)) wiring from the connector (7WN1-A) pin A/C to the ground terminal wiring from the indicator light (3WN1) to the indicator light (2WN1) wiring from the indicator light (2WN1) to the indicator light (1WN2) wiring from the indicator light (1WN1) to the relay (12WN) wiring from the relay (12WN) to the circuit breaker (13WN) wiring from the relay (12WN) to the circuit breaker (15WN) - PROX SW-HANDLE, L AFT ESC SLIDE [7WN1]
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 |
| AMM 31-60-00-860-001 | EIS Start Procedure |
| AMM 52-71-00-820-002 | Adjustment of the Proximity Switches of the Passenger/Crew Doors with the CHECKING TOOL-DOORS |
| ASM 527301 | |
| AMM 52-73-11-000-002 | Removal of the Proximity Switches of the Aft Passenger/Crew Doors |
| AMM 52-73-11-400-002 | Installation of the Proximity Switches of the Aft Passenger/Crew Doors |
| AMM 52-73-21-000-001 | Removal of the SLIDE ARMED Indicator-Light of the FWD Passenger/Crew Door |
| AMM 52-73-21-000-002 | Removal of the SLIDE ARMED Indicator-Light of the Aft Passenger/Crew Door |
| AMM 52-73-21-000-003 | Removal of the SLIDE ARMED Indicator-Light of the Emergency Exit |
| AMM 52-73-21-400-001 | Installation of the SLIDE ARMED Indicator-Light of the FWD Passenger/Crew Door |
| AMM 52-73-21-400-002 | Installation of the SLIDE ARMED Indicator-Light of the Aft Passenger/Crew Door |
| AMM 52-73-21-400-003 | Installation of the SLIDE ARMED Indicator-Light of the Emergency Exit |
Subtask 52-13-00-860-064-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 52-13-00-865-055-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 52-13-00-710-064-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 121VU | EIS/SLIDES/ARM AND WARN/GND | 13WN | P10 |
C. Test
(1) On the ECAM control panel:
4. Fault Isolation(1) On the ECAM control panel:
- push the DOOR key to get the DOOR/OXY page.
Subtask 52-13-00-810-067-A
A. If the test confirms the fault:
Subtask 52-13-00-710-065-A - disconnect the connector of the handle proximity switch (7WN1)
- install the jumper wire between the pins B and C of the connector (7WN1-A) ASM 527301
- do the test given in Para 3.B.
- replace the IND LT-SLIDE ARMED, AFT L DOOR [3WN1] AMM 52-73-21-000-002 and AMM 52-73-21-400-002.
- replace the IND LT-SLIDE ARMED, L EMER EXIT [2WN1] AMM 52-73-21-000-003 and AMM 52-73-21-400-003.
- replace the IND LT-SLIDE ARMED, FWD L DOOR [1WN1] AMM 52-73-21-000-001 and AMM 52-73-21-400-001
- replace the RELAY-PWR SPLY SWITCHOVER [12WN] ASM 527301.
- do a check for a ground signal at pin A/C of the proximity switch (7WN1) ASM 527301.
- do a check and repair the
wiring from the connector (7WN1-A) to the indicator light (3WN1) pin A/B to pin H ASM 527301 - do a check and repair the
wiring from the indicator light (3WN1) to the SDAC-1(2) (1WV1(2)) pin K to pin AA (AD)/12B(12H) ASM 527301.
- repair the
wiring from the connector (7WN1-A) pin A/C to the ground terminal ASM 527301.
- do a check and repair the
wiring from the indicator light (3WN1) to the indicator light (2WN1) pin A to pin B ASM 527301 and ASM 527301. - do a check and repair the
wiring from the indicator light (2WN1) to the indicator light (1WN2) pin A to pin B ASM 527301. - do a check and repair the
wiring from the indicator light (1WN1) to the relay (12WN) pin A to pin A/B2 ASM 527301. - do a check and repair the
wiring from the relay (12WN) to the circuit breaker (13WN) pin A/B3 to pin 2 ASM 527301. - do a check and repair the
wiring from the relay (12WN) to the circuit breaker (15WN) pin A/B1 to pin 2 ASM 527301.
- remove the jumper wire between the pins B and C of the connector (7WN1-A)
- connect the connector of the handle proximity switch (7WN1)
- adjust the handle proximity switch (7WN1) with the doors checking tool AMM 52-71-00-820-002 or with the ECAM system AMM 52-71-00-820-002.
- replace the PROX SW-HANDLE, L AFT ESC SLIDE [7WN1] AMM 52-73-11-000-002 and AMM 52-73-11-400-002.
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.
Subtask 52-13-00-860-065-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.