「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 ∞∞52-11-00∞∞∞∞∞∞∞∞∞∞Page 219
Nov 01/03R CES
3. Fault Confirmation
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A. Job Set-up
(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).
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
C. Test
(1) On the ECAM control panel:
- push the DOOR key to get the DOOR/OXY page.
(2) Make sure that the SLIDE indication is not shown on the DOOR/OXY page when the R forward escape-slide handle is in the SLIDE ARMED position.
4. Fault Isolation
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A. If the test confirms the fault:
- disconnect the connector A of the handle proximity switch (4WN2)
- install the jumper wire between the pins A/B, C of the handle proximity switch (4WN2) (Ref. ASM 52-73/01)
- do the test given in Para 3.B.
(1) If the test confirms the fault:
- replace the IND LT-SLIDE ARMED, FWD R DOOR (1WN2) (Ref. AMM TASK 52-73-21-000-002) and (Ref. AMM TASK 52-73-21-400-002).
(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 pin A/C of the proximity switch (4WN2) (Ref. ASM 52-73/01).
1 If there is a ground signal:
_
- do a check and repair the wiring from the proximity switch (4WN2) to the indicator light (1WN2) pin A/B to pin H (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 : ALL ∞∞52-11-00∞∞∞∞∞∞∞∞∞∞Page 220
Nov 01/03R CES
- do a check and repair the wiring from the indicator light (1WN2) to the SDAC - 1(2) (1WV1(2)) pin K to pin AA (AD)/12A,12G (Ref. ASM 52-73/01) and (Ref. ASM 52-73/01).
2 If there is no ground signal:
_
- repair the wiring from the proximity switch (4WN2) pin A/C to the ground terminal (Ref. ASM 52-73/01).
(c) If the fault continues:
- do a check and repair the wiring from the indicator light (1WN2) to the relay (12WN) pin A to pin A/A2 (Ref. ASM 52-73/01)
- do a check and repair the wiring from the relay (12WN) to the circuit breaker (13WN) pin A/B3 to pin 2 (Ref. ASM 52-73/01)
- do a check and repair the wiring from the relay (12WN) to the circuit breaker (15WN) pin A/B1 to pin 2 (Ref. ASM 52-73/01).
(2) If the test does not confirm the fault:
- remove the jumper wire between the pins A/B, C of the handle proximity switch (4WN2)
- connect the connector A of the handle proximity switch (4WN2)
- adjust the handle proximity switch (4WN2) with the door checking tool (Ref. AMM TASK 52-71-00-820-002) or with the ECAM system (Ref. AMM TASK 52-71-00-820-002).
(a) If the fault continues:
- replace the PROX SW-HANDLE, R FWD ESC SLIDE (4WN2) (Ref. AMM TASK 52-73-11-000-002) and (Ref. AMM TASK 52-73-11-400-002).
B. Test
(1) On the ECAM control panel:
- push the DOOR key to get the DOOR/OXY page.
(2) Make sure that the SLIDE indication is shown on the DOOR/OXY page when the R. forward escape-slide handle is in the SLIDE ARMED position.
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 ∞∞52-11-00∞∞∞∞∞∞∞∞∞∞Page 221 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 艙門 DOORS(30)
