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R  - do a check and repair the wiring from the door frame 
R  proximity switch (36WV) to the SDAC-1(2) (1WV1(2)) pin B to 
R  pin AD/12F (Ref. ASM 31-54/05). 
R  (b) If the test does not confirm the fault: 
R  - remove the jumper wire between the pins B and C of the door 
R  frame proximity switch (36WV) 
R  - connect the connector of the door frame proximity switch (36WV) 
R  - adjust the door frame proximity switch (36WV) with the doors 
R  checking tool (Ref. AMM TASK 52-71-00-820-008) or with the ECAM 
R  system (Ref. AMM TASK 52-71-00-820-008). 
R  1_  If the fault continues:
R  - replace the PROX SW-FRAME, FWD AVIONICS COMPT DOOR (36WV) 
R  (Ref. AMM TASK 52-71-14-000-001) and (Ref. AMM TASK 52-71-
14-400-001). 
R  (3) If the fault continues: 
R  - replace the SDAC-1 (1WV1) (Ref. AMM TASK 31-55-34-000-001) and 
R  (Ref. AMM TASK 31-55-34-400-001).

 「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 ∞∞52-41-00∞∞∞∞∞∞∞∞∞∞Page 208
 Nov 01/03 CES

R R R R (4) If the fault continues: - replace the SDAC-2 (1WV2) (Ref. AMM TASK 31-55-34-000-001) and (Ref. AMM TASK 31-55-34-400-001). 
B. Test
 (1) On the ECAM control panel: - push the DOOR key to get the DOOR/OXY page.
 (2) Make sure that the FWD AVIONIC indication and the door symbol come into view green.
 5. Close-up________
 A. Put the aircraft back to its initial configuration.
 (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (Ref. AMM TASK 31-60-00-860-002)
 (2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).

 TASK 52-41-00-810-804

 Disagree between the ECAM System Display Page Indication and the Closed and Locked Position of the Aft Avionics-Compartment-Door
 1. Possible Causes
_______________
 - PROX SW-FRAME, AFT AVIONICS COMPT DOOR (40WV) R - SDAC-1 (1WV1) R - SDAC-2 (1WV2) R - wiring R
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-41-00-861-002
AMM 24-41-00-862-002
R AMM 31-55-34-000-001 R AMM 31-55-34-400-001
AMM 31-60-00-860-001 R AMM 52-71-00-820-008 R R R AMM 52-71-00-820-008 R R
AMM 52-71-14-000-001
AMM 52-71-14-400-001
ASM 31-54/05
 3. Fault Confirmation
__________________
 A. Job Set-UpEnergize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External Power Removal of the SDAC (1WV1,1WV2) Installation of the SDAC (1WV1,1WV2)EIS Start Procedure Adjustment of the Proximity Switches (23WV, 38WV, 40WV) of the Avionics Compartment Doors with the CHECKING TOOL-DOORS Adjustment of the Proximity Switches (23WV, 38WV, 40WV) of the Avionics Compartment Doors with the lower ECAM DURemoval of the Proximity Switches (23WV, 36WV, 38WV, 40WV) of the Avionics Compartment DoorsInstallation of the Proximity Switches (23WV, 36WV, 38WV, 40WV) of the Avionics Compartment Doors
 (1) Aircraft Maintenance Configuration
 (a) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).

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

 「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 ∞∞52-41-00∞∞∞∞∞∞∞∞∞∞Page 210
 Nov 01/03 CES

 B. Test

 (1) On the ECAM control panel:
 - push the DOOR key to get the DOOR/OXY page.
 (2) Make sure that the Aft AVIONIC indication and the door symbol come
 into view amber.
 4. Fault Isolation_______________ 
R  A. If the test confirms the fault: 
R  - do a check for 28VDC between pins A and D of door frame proximity 
R  switch (40WV) (Ref. ASM 31-54/05). 
R  (1) If there is no 28VDC: 
R  - repair the wiring as necessary. 
R  (2) If there is 28VDC: 
R  - disconnect the connector of the door frame proximity switch (40WV) 
R  - install the jumper wire between the pins B and C of the door frame 
　
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