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

 (2) Make sure that the latch pin for the RH emergency exit is in the slide armed position.

 (3) Make sure that the SLIDE indication is shown on the DOOR/OXY page.

 NOTE : If this occurs, the trouble shooting procedure is
____
 satisfactory.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 151-199, 401-499, ∞∞52-21-00∞∞∞∞∞∞∞∞∞∞Page 225
 Aug 01/05 CESR **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,

 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).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞52-21-00∞∞∞∞∞∞∞∞∞∞Page 226
 201-299, 401-499, Aug 01/05 CES

 PASSENGER COMPARTMENT EMERGENCY EXIT ((DOORS)) - FAULT ISOLATION PROCEDURES
___________________________________________________________________________
 TASK 52-22-00-810-801
 Disagree between the DOOR/OXY page of the ECAM System and the locked LH FWD
 Emergency Exit Door
 1. Possible Causes
_______________
 - PROX SW-HOOK, L FWD EMER EXIT (59WV1)

 - SDAC-1 (1WV1)

 - SDAC-2 (1WV2)

 - EIS/SDAC1 AND 2/DOOR/DET/PAX (48WV)

 - IND LT-SLIDE ARMED, AFT L EMERGENCY EXIT (21WN1)

 - PROX SW-HANDLE FLAP, L FWD EMER EXIT (19WV1)

 - EIS/SLIDES/ARM AND WARN/GND (13WN)

 - 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 31-60-00-860-001 EIS Start Procedure
 AMM 52-22-00-410-001 Closing of the Emergency Exit Doors from the

 Passenger Compartment
 AMM 52-71-00-820-005  Adjustment of the Proximity Switches (59WV1,59WV2,61WV1,61WV2) of the Emergency Exits with the CHECKING TOOL-DOORS
 AMM 52-71-00-820-007  Adjustment of the Proximity Switches (19WV1, 19WV2, 21WV1,21WV2) of the Emergency Exit Doors with the CHECKING TOOL-DOORS
 AMM 52-71-13-000-003 Removal of the Proximity Switches 59WV1, 59WV2, 61WV1 and 61WV2 AMM 52-71-13-400-003 Installation of the Proximity Switches 59WV1, 59WV2, 61WV1 and 61WV2 AMM 52-73-22-000-003 Removal of the CABIN PRESSURE Warning Light Panel (19WN1,19WN2,20WN1,20WN2) of the Emergency Exit
 AMM 52-73-22-400-003  Installation of the CABIN PRESSURE Warning Light
 Panel of the Emergency Exit Door
 (19WN1,19WN2,20WN1,20WN2)

 ASM 31-54/05
 「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 201
 May 01/04 CES

 3. Fault Confirmation
__________________

 A. Aircraft Maintenance Configuration
 (1) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).

 (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).

 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 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
 C. Test
 (1) Make sure that the LH FWD emergency exit door is closed and locked (Ref. AMM TASK 52-22-00-410-001).

 (2) On the ECAM control panel:

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

 (3) On the DOOR/OXY page of the lower ECAM DU, look for possible fault indications.

 4. Fault Isolation
_______________
 A. If the test gives the amber EMER EXIT indication of the LH FWD emergency exit door:
 - do a check and adjust as necessary the PROX SW-HOOK, L FWD EMER EXIT (59WV1) (Ref. AMM TASK 52-71-00-820-005)
　
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