- repair the wiring from the pin C of the connector (17WV1-A) to the terminal block.
(b) If there is a ground signal:
- do a check and repair the wiring from the connector (17WV1-A) to the indicator light (3WN1) pin B to pin F (Ref. ASM 31-54/05) and (Ref. ASM 52-73/01).
(2) If the test does not confirm the fault:
- remove the jumper wire between the pins B and C of the connector (17WV1-A)
- connect the connector of the handle proximity switch (17WV1)
- adjust the handle proximity switch (17WV1) with the doors 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, L AFT PAX/CREW DOOR (17WV1) (Ref. AMM TASK 52-71-11-000-001) and (Ref. AMM TASK 52-71-11-400-001).
B. Test
(1) Make sure that the SLIDE ARMED indicator light of the L aft passenger/crew door is off when the door is locked with the handle of the escape slide in the ARMED position.
「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 233
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5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) 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 234
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CES
TASK 52-13-00-810-809
The SLIDE ARMED indicator light of the right aft passenger/crew door is
inoperative in flight
1. Possible Causes
_______________
- IND LT-SLIDE ARMED, AFT R DOOR (3WN2)
- IND LT-SLIDE ARMED, R EMER EXIT (2WN2)
- IND LT-SLIDE ARMED, FWD R DOOR (1WN2)
- wiring from the proximity switch (17WV2) to the indicator light (3WN2)
- wiring from the proximity switch (17WV2) pin C to the ground
- wiring from the indicator light (3WV2) to the indicator light (2WN2)
- wiring from the indicator light (2WN2) to the indicator light (1WN2)
- wiring from the indicator light (1WV2) to the relay (12WN)
- RELAY-PWR SPLY SWITCHOVER (12WN)
- wiring from the relay (12WN) to the circuit breaker (15WN)
- C/B-EIS/SLIDES/ARM AND WARN/FLT (15WN)
- wiring from the circuit breaker (15WN) to the indicator light (3WN2)
- circuit breaker 15WN
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 52732100000100 AMM 52732140000100 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 25-62-44-000-002 Escape-Slide Pack-Assembly - Removal AMM 25-62-44-400-001 Escape-Slide Pack-Assembly - Installation AMM 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
Door AMM 52-10-00-860-002 Special Precautions after Work on the Passenger/Crew Door AMM 52-73-21-000-001 Removal of the SLIDE ARMED Indicator-Light (1WN1, 1WN2) of the FWD Passenger/Crew Door AMM 52-73-21-400-001 Installation of the SLIDE ARMED Indicator-Light
(1WN1, 1WN2) of the FWD Passenger/Crew Door
ASM 31-54/05
ASM 52-73/01
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 ∞∞52-13-00∞∞∞∞∞∞∞∞∞∞Page 235
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3. Fault Confirmation
__________________
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Disarm the percussion system of the door damper and emergency operation cylinder (Ref. AMM TASK 52-10-00-860-001).
(3) Remove the escape slide or escape slide/raft pack assembbly (Ref. AMM TASK 25-62-44-000-002).
B. Make sure that this(these) circuit breaker(s) is(are) closed: -------------------------------------------------------------------------------
PANEL ------ DESIGNATION ------------------------------------ ------------------ IDENT. LOCATION-------------------
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