- wiring from the connector (7WN2-A) pin A/C to the ground terminal
- wiring from the indicator light (3WN2) to the indicator light (2WN2)
- wiring from the indicator light (2WN2) to the indicator light (1WN2)
- wiring from the indicator light (1WN2) to the relay (12WN)
- wiring from the relay (12WN) to the circuit breaker (13WN)
- wiring from the relay (12WN) to the circuit breaker (15WN)
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 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power AMM 31-60-00-860-001 EIS Start Procedure AMM 52-71-00-820-002 Adjustment of the Proximity Switches (4WN1, 4WN2,
7WN1, 7WN2, 13WV1, 13WV2, 17WV1, 17WV2) of the Passenger/Crew Doors with the CHECKING TOOL-DOORS
AMM 52-71-00-820-002 Adjustment of the Proximity Switches (4WN1, 4WN2, 7WN1, 7WN2, 13WV1, 13WV2, 17WV1, 17WV2) of the Passenger/Crew Doors with the ECAM DU.
AMM 52-73-11-000-002 Removal of the Proximity Switches (7WN1, 7WN2) of the Aft Passenger/Crew Doors AMM 52-73-11-400-002 Installation of the Proximity Switches (7WN1, 7WN2) of the Aft Passenger/Crew Doors AMM 52-73-21-000-001 Removal of the SLIDE ARMED Indicator-Light (1WN1, 1WN2) of the FWD Passenger/Crew Door AMM 52-73-21-000-002 Removal of the SLIDE ARMED Indicator-Light (3WN1, 3WN2) of the Aft Passenger/Crew Door AMM 52-73-21-000-003 Removal of the SLIDE ARMED Indicator-Light (2WN1, 2WN2) of the Emergency Exit AMM 52-73-21-400-001 Installation of the SLIDE ARMED Indicator-Light (1WN1, 1WN2) of the FWD Passenger/Crew Door
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞52-13-00∞∞∞∞∞∞∞∞∞∞Page 221
Nov 01/03R CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 52-73-21-400-002 Installation of the SLIDE ARMED Indicator-Light (3WN1, 3WN2) of the Aft Passenger/Crew Door AMM 52-73-21-400-003 Installation of the SLIDE ARMED Indicator-Light
(2WN1, 2WN2) of the Emergency Exit ASM 52-73/01 ASM 52-73/01
3. Fault Confirmation
__________________
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 aft escape-slide handle is in the SLIDE ARMED position.
4. Fault Isolation
_______________
A. If the test confirms the fault:
- disconnect the connector of the handle proximity switch (7WN2)
- install the jumper wire between the pins B and C of the connector (7WN2-A) (Ref. ASM 52-73/01)
- do the test given in Para 3.B.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞52-13-00∞∞∞∞∞∞∞∞∞∞Page 222
Nov 01/03R
CES (1) If the test confirms the fault:
- replace the IND LT-SLIDE ARMED, AFT R DOOR (3WN2) (Ref. AMM TASK 52-73-21-000-002) and (Ref. AMM TASK 52-73-21-400-002).
(a) If the fault continues:
- replace the IND LT-SLIDE ARMED, R EMER EXIT (2WN2) (Ref. AMM TASK 52-73-21-000-003) and (Ref. AMM TASK 52-73-21-400-003).
(b) If the fault continues:
- replace the IND LT-SLIDE ARMED, FWD R DOOR (1WN2) (Ref. AMM TASK 52-73-21-000-001) and (Ref. AMM TASK 52-73-21-400-001)
(c) If the fault continues:
- replace the RELAY-PWR SPLY SWITCHOVER (12WN) (Ref. ASM 52-73/01).
(d) If the fault continues:
中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 舱门 DOORS(52)
