B. Make sure that this(these) circuit breaker(s) is(are) closed:

 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11 121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10
 C. Test
 (1) On the ECAM control panel:

 - push the DOOR key to get the DOOR/OXY page.

 (2) Make sure that the slide control handle for the LH FWD emergency exit is in the slide armed position.

 (3) Make sure that the SLIDE indication is not shown on the DOOR/OXY page.

 4. Fault Isolation
_______________
 A. If the test confirms the fault:
 - disconnect the connector A of the handle proximity switch (5WN1)

 - install the jumper wire at the connector A, between pins B and C of the handle proximity switch (5WN1) (Ref. ASM 52-73/01).

 - do the test given in Para 3.

 (1) If the test confirms the fault:
 - replace the IND LT-SLIDE ARMED, AFT L EMERGENCY EXIT (21WN1) (Ref. AMM TASK 52-73-21-000-003) and (Ref. AMM TASK 52-73-21-400-003).
 (a) If the fault continues:

 - replace the RELAY-PWR SPLY SWITCH OVER (12WN) (Ref. ASM 52-73/01).

 (b) If the fault continues:

 - do a check for a ground signal at connector A, pin C of the proximity switch (5WN1) (Ref. ASM 52-73/01).
 1 If there is a ground signal:
_
 - do a check and repair the aircraft wiring from the proximity switch (5WN1) to the SDAC 1(2) ((1WV1 (2)) (Ref. ASM 52-73/01) and (Ref. ASM 52-73/01).
 2 If there is no ground signal:
_
 - repair the aircraft wiring from the proximity switch (5WN1) connector A, pin C to the ground terminal (Ref. ASM 52-73/01).
 「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 : 301-399, ∞∞52-22-00∞∞∞∞∞∞∞∞∞∞Page 228
 May 01/04 CES (2) If the test does not confirm the fault:

 - remove the jumper wire of the connectors A between the pins B and C of the handle proximity switch (5WN1).

 - connect the connector A of the handle proximity switch (5WN1).

 - adjust the handle proximity switch (5WN1) with the door checking tool or with the ECAM system (Ref. AMM TASK 52-71-00-820-009).

 (a) If the fault continues:
 - replace the PROX SW-HANDLE, L FWD EMER EXIT ESC SLIDE (5WN1) (Ref. AMM TASK 52-73-11-000-003) and (Ref. AMM TASK 52-73-11-400-003).
 B. Do a test as given in Para. 3. to make sure that the operation is
 correct.

 5. Close-up
________
 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
 (Ref. AMM TASK 24-41-00-862-002).

 TASK 52-22-00-810-812

 No SLIDE Indication on the DOOR/OXY Page for the RH FWD Emergency Exit when the Slide Control handle is in the Slide Armed Position
 1. Possible Causes
_______________
 - IND LT-SLIDE ARMED, FWD R EMERGENCY EXIT (21WN2)

 - PROX SW-HANDLE, R FWD EMER EXIT ESC SLIDE (5WN2)

 - RELAY-PWR SPLY SWITCH OVER (12WN)

 - aircraft wiring

 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 52-71-00-820-009 Adjustment of the Proximity Switches (5WN1, 5WN2,

 6WN1, 6WN2) of the Emergency Exits AMM 52-73-11-000-003 Removal of the Proximity Switches (5WN1, 5WN2) of the FWD Emergency Exits AMM 52-73-11-400-003 Installation of the Proximity Switches (5WN1, 5WN2) of the FWD Emergency Exits AMM 52-73-21-000-003 Removal of the SLIDE ARMED Indicator-Light (2WN1, 2WN2) of the Emergency Exit AMM 52-73-21-400-003 Installation of the SLIDE ARMED Indicator-Light
 (2WN1, 2WN2) of the Emergency Exit
 ASM 52-73/01
 ASM 52-73/01

 3. Fault Confirmation
__________________
 A. Job Set-up
 (1) Aircraft Maintenance Configuration
 (a) Energize the aircraft electrical circuits
　
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