(b) If there is a ground signal:

 - do a check and repair the wiring from the connector (17WV2-A) to the indicator light (3WN2) pin B to pin F (Ref. ASM 31-54/05) and (Ref. ASM 52-73/01).

 (2) If the test does not confirm the fault:

 - remove the jumper wire between the pins B and C of the connector (17WV2-A)

 - connect the connector of the handle proximity switch (17WV2)

 - adjust the handle proximity switch (17WV2) with the doors checking tool (Ref. AMM TASK 52-71-00-820-002) or with the ECAM system (Ref. AMM TASK 52-71-00-820-002).

 (a) If the fault continues:
 - replace the PROX SW-HANDLE, R AFT PAX/CREW DOOR (17WV2) (Ref. AMM TASK 52-71-11-000-001) and (Ref. AMM TASK 52-71-11-400-001).
 B. Test
 (1) Make sure that the SLIDE ARMED indicator light of the R aft passenger/crew door is off when the door is locked with the handle of the escape slide in the ARMED position.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞52-13-00∞∞∞∞∞∞∞∞∞∞Page 230
 Nov 01/03R CES

 5. Close-up
________
 A. Put the aircraft back to its initial configuration.
 (1) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞52-13-00∞∞∞∞∞∞∞∞∞∞Page 231
 Nov 01/03R
 CES

 TASK 52-13-00-810-808

 SLIDE ARMED Indicator Light On with the L Aft Passenger/Crew Door in the Locked Position and the Handle of the Escape Slide in the ARMED Position
 1. Possible Causes_______________
 - PROX SW-HANDLE, L AFT PAX/CREW DOOR (17WV1)

 - wiring from the pin C of the connector (17WV1-A) to the terminal block

 - wiring from the connector (17WV1-A) to the indicator light (3WN1)

 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 52-71-00-820-002  Adjustment of the Proximity Switches (4WN1, 4WN2, 7WN1, 7WN2, 13WV1, 13WV2, 17WV1, 17WV2) of the Passenger/Crew Doors with the CHECKING TOOL-DOORS
 AMM 52-71-00-820-002  Adjustment of the Proximity Switches (4WN1, 4WN2, 7WN1, 7WN2, 13WV1, 13WV2, 17WV1, 17WV2) of the Passenger/Crew Doors with the ECAM DU.
 AMM 52-71-11-000-001  Removal of the Proximity Switches of the Passenger/Crew Doors (11WV1,11WV2,13WV1,13WV2,15WV1,15WV2,17WV1,17WV2)
 AMM 52-71-11-400-001  Installation of the Proximity Switches of the Passenger/Crew Door (11WV1,11WV2,13WV1,13WV2,15WV1,15WV2,17WV1,17WV2)
 ASM 31-54/05
 ASM 52-73/01
 3. Fault Confirmation__________________
 A. Job Set-up
 (1) Aircraft Maintenance Configuration
 (a) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞52-13-00∞∞∞∞∞∞∞∞∞∞Page 232
 Nov 01/03R
 CES  B. Make sure that this(these) circuit breaker(s) is(are) closed:

 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10
 C. Test
 (1) Make sure that the SLIDE ARMED indicator light of the L aft passenger/crew door is on when the door is locked with the handle of the escape slide in the ARMED position.
 4. Fault Isolation
_______________
 A. If the test confirms the fault:
 - disconnect the connector of the handle proximity switch (17WV1)

 - install the jumper wire between the pins B and C of the connector (17WV1-A) (Ref. ASM 31-54/05)

 - do the test given in Para 3.B.

 (1) If the test confirms the fault:

 - do a check for a ground signal at pin C of the handle proximity switch (17WV1) (Ref. ASM 31-54/05).
 (a) If there is no ground signal:
　
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