W DOC AIRBUS | TSM A320F

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
  • 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]
2. Job Set-up Information
 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
3. Fault Confirmation
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
B. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
Subtask 52-13-00-710-064-A
C. Test
   (1) On the ECAM control panel:
  • push the DOOR key to get the DOOR/OXY page.
   (2) Make sure that the SLIDE indication is not shown on the DOOR/OXY page when the L aft escape-slide handle is in the SLIDE ARMED position.
4. Fault Isolation
Subtask 52-13-00-810-067-A
A. If the test confirms the fault:
  • 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.
   (1) If the test confirms the fault:
     (a) If the fault continues:
     (b) If the fault continues:
     (c) If the fault continues:
     (d) If the fault continues:
  • do a check for a ground signal at pin A/C of the proximity switch (7WN1) ASM 527301.
       1 If there is a ground signal:
  • 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.
       2 If there is no ground signal:
  • repair the wiring from the connector (7WN1-A) pin A/C to the ground terminal ASM 527301.
     (e) If the fault continues:
  • 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.
   (2) If the test does not confirm the fault:
  • 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.
     (a) If the fault continues:
Subtask 52-13-00-710-065-A
B. Test
   (1) On the ECAM control panel:
  • push the DOOR key to get the DOOR/OXY page.
   (2) Make sure that the SLIDE indication is shown on the DOOR/OXY page when the L aft escape-slide handle is in the SLIDE ARMED position.
5. Close-up
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.
[Rev.8 from Aug 2018] 2026.04.04 04:34:46 UTC