ACCESS DOORS - FAULT ISOLATION PROCEDURES
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TASK 52-41-00-810-801
Disagree between the ECAM System Display Page Indication and the Closed and Locked Position of the Left Avionics-Compartment Door
1. Possible Causes
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- PROX SW-FRAME, L AVIONICS COMPT DOOR (23WV) R - SDAC-1 (1WV1) R - SDAC-2 (1WV2) R - wiring R
2. Job Set-up Information
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A. Referenced Information
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REFERENCE DESIGNATION
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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 AMM 31-60-00-860-002
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
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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 ProcedureEIS Stop 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).
「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 201
Nov 01/03 CES
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
B. Test
(1) On the ECAM control panel:
- push the DOOR key to get the DOOR/OXY page.
(2) Make sure that the L AVIONIC indication and the door symbol come into view amber.
4. Fault Isolation
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A. If the test confirms the fault: R - do a check for 28VDC between pins A and D of door frame proximity R switch (23WV) (Ref. ASM 31-54/05).
R (1) If there is no 28VDC:
R - repair the wiring as necessary.
R (2) If there is 28VDC:
- disconnect the connector of the door frame proximity switch (23WV)
- install the jumper wire between the pins B and C of the door frame proximity switch (23WV) (Ref. ASM 31-54/05)
- do the test given in Para 3.B. R
R (a) If the test confirms the fault:
- do a check for a ground signal at pin C of the door frame proximity switch (23WV) (Ref. ASM 31-54/05).
R
R 1_ If there is no ground signal:
R - repair the wiring from the pin C of the door frame proximity
R switch (23WV) to the ground terminal.
R
R 2_ If there is a ground signal:
R - do a check and repair the wiring from the door frame
R proximity switch (23WV) to the SDAC-1(2) (1WV1(2)) pin B to
R pin AD/11E (Ref. ASM 31-54/05).
R
R (b) If the test does not confirm the fault:
- remove the jumper wire between the pins B and C of the door
frame proximity switch (23WV)
- connect the connector of the door frame proximity switch (23WV)
- adjust the door frame proximity switch (23WV) with the doors
checking tool (Ref. AMM TASK 52-71-00-820-008) or with the ECAM
system (Ref. AMM TASK 52-71-00-820-008).
R
「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 202
Nov 01/03 CES
R 1_ If the fault continues: - replace the PROX SW-FRAME, L AVIONICS COMPT DOOR (23WV) (Ref. AMM TASK 52-71-14-000-001) and (Ref. AMM TASK 52-71-14-400-001).
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 艙門 DOORS(112)
