- install the jumper wire between the pins B and C of the handle proximity switch (13WV1) (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 (13WV1) (Ref. ASM 31-54/05).
 (a) If there is no ground signal:

 - repair the wiring from the pin C of the handle proximity switch (13WV1) to the terminal block.

 (b) If there is a ground signal:

 - do a check and repair the wiring from the handle proximity switch (13WV1) to the indicator light (1WN1) 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 handle proximity switch (13WV1)

 - connect the connector of the handle proximity switch (13WV1)

 - adjust the handle proximity switch (13WV1) 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, L FWD PAX/CREW DOOR (13WV1) (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 L. forward 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 ∞∞52-11-00∞∞∞∞∞∞∞∞∞∞Page 229
 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 ∞∞52-11-00∞∞∞∞∞∞∞∞∞∞Page 230
 Nov 01/03R
 CES

 TASK 52-11-00-810-809

 The SLIDE ARMED indicator light of the forward right passenger/crew door is
 inoperative in flight
 1. Possible Causes
_______________
 - IND LT-SLIDE ARMED, FWD R DOOR (1WN2)

 - wiring from the proximity switch (13WV2) to the indicator light (1WN2)

 - wiring from the proximity switch (13WV2) pin C to the ground

 - RELAY-PWR SPLY SWITCHOVER (12WN)

 - wiring from the relay (12WN) to the indicator light (1WN2)

 - C/B-EIS/SLIDES/ARM AND WARN/FLT (15WN)

 - wiring from the circuit breaker (15WN) to the relay (12WN)

 - wiring from the circuit breaker (15WN) to the indicator light (1WN2)

 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
R AMM 25-62-44-000-002 Removal of the Escape-Slide Pack-Assembly
R AMM 25-62-44-400-001 Installation of the Escape-Slide Pack-Assembly AMM 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew Door AMM 52-10-00-860-002 Special Precautions after Work on the Passenger/Crew Door AMM 52-73-21-000-001 Removal of the SLIDE ARMED Indicator-Light (1WN1, 1WN2) of the FWD Passenger/Crew Door AMM 52-73-21-400-001 Installation of the SLIDE ARMED Indicator-Light (1WN1, 1WN2) of the FWD Passenger/Crew Door ASM 31-54/05 ASM 52-73/01
 3. Fault Confirmation
__________________
 A. Aircraft Maintenance Configuration
 (1) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).

 (2) Disarm the percussion system of the door damper and emergency operation cylinder (Ref. AMM TASK 52-10-00-860-001).

 (3) Remove the escape slide or escape slide/raft pack assembbly (Ref. AMM TASK 25-62-44-000-002).

 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
 ------------------------------------------ACTION  ------------------RESULT -------------------
　
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