R * On the Door/Oxy page, if the CABIN indication comes
R into view green:
- remove the jumper wire between pins F and G of the plug
2879VC
- replace the IND LT-SLIDE ARMED, AFT L DOOR (3WN1) (Ref.
AMM TASK 52-73-21-000-002) and (Ref. AMM TASK 52-73-21-
400-002).
R
R * On the Door/Oxy page, if the CABIN indication comes
R into view amber:
- remove the jumper wire between pins F and G of the plug
2879VC
- connect the plug 2879VC to the indicator light (3WN1)
- do a check for a ground signal at pin C of the handle
proximity switch (17WV1) (Ref. ASM 31-54/05).
R
R ** If there is no ground signal:
- repair the wiring from the pin C of the handle proximity
switch (17WV1) to the ground terminal (Ref. ASM 31-54/05)
R
R ** If there is a ground signal:
- do a check of the wiring between:
R *** the handle proximity switch (17WV1) pin B and the
R indicator light (3WN1) pin F,
R *** the indicator light (3WN1) pin G and the hook
R proximity switch (15WV1) pin C,
R *** the hook proximity switch (15WV1) pin B and the
R SDAC-1(2) pin AA/11B (Ref. ASM 31-54/02) and (Ref. ASM
R 31-54/05).
- repair the wiring as necessary.
R 3_ If the fault continues:
R - replace the SDAC-1 (1WV1) (Ref. AMM TASK 31-55-34-000-001)
R and (Ref. AMM TASK 31-55-34-400-001).
R 4_ If the fault continues:
R - replace the SDAC-2 (1WV2) (Ref. AMM TASK 31-55-34-000-001)
R 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) On the DOOR/OXY page:
- make sure that the CABIN indication comes into view green.
「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 213
Nov 01/03 CES
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).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞52-13-00∞∞∞∞∞∞∞∞∞∞Page 214
Nov 01/03R
CES
TASK 52-13-00-810-804
Disagree between the DOOR/OXY Page Indication and the Locked Position of the R Aft PAX/Crew Door
1. Possible Causes
_______________
R
- IND LT-SLIDE ARMED, AFT R DOOR (3WN2) R - IND LT-SLIDE ARMED, R EMER EXIT (2WN2) R - PROX SW-HANDLE, R AFT PAX/CREW DOOR (17WV2) R - PROX SW-HOOK, R AFT PAX/CREW DOOR (15WV2) R - SDAC-1 (1WV1) R - SDAC-2 (1WV2)
- wiring
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 52-71-00-820-001 R R R AMM 52-71-00-820-001 R R
AMM 52-71-00-820-002
AMM 52-71-00-820-002
AMM 52-71-11-000-001
AMM 52-71-11-400-001
R AMM 52-73-21-000-001 R Energize 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 (11WV1, 11WV2, 15WV1, 15WV2) of the Locking Hook of the Pax/Crew Doors with the CHECKING TOOL-DOOR Adjustment of the Proximity Switches (11WV1, 11WV2, 15WV1, 15WV2) of the Locking Hook of the Passenger/Crew Doors with the ECAM DUAdjustment of the Proximity Switches (4WN1, 4WN2, 7WN1, 7WN2, 13WV1, 13WV2, 17WV1, 17WV2) of the Passenger/Crew Doors with the CHECKING TOOL-DOORSAdjustment of the Proximity Switches (4WN1, 4WN2, 7WN1, 7WN2, 13WV1, 13WV2, 17WV1, 17WV2) of the Passenger/Crew Doors with the ECAM DU.Removal of the Proximity Switches of the Passenger/Crew Doors (11WV1,11WV2,13WV1,13WV2,15WV1,15WV2,17WV1,17WV2)Installation of the Proximity Switches of the Passenger/Crew Door (11WV1,11WV2,13WV1,13WV2,15WV1,15WV2,17WV1,17WV2) Removal of the SLIDE ARMED Indicator-Light (1WN1, 1WN2) of the FWD Passenger/Crew Door
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