SLIDE ARMED Indicator Light On with the L Aft Passenger/Crew Door in the Locked Position and the Handle of the Escape Slide in the ARMED Position

TASK 52-13-00-810-808-A
SLIDE ARMED Indicator Light On with the L Aft Passenger/Crew Door in the Locked Position and the Handle of the Escape Slide in the ARMED Position

1. Possible Causes

wiring from the pin C of the connector (17WV1-A) to the terminal block
wiring from the connector (17WV1-A) to the indicator light (3WN1)
PROX SW-HANDLE, L AFT PAX/CREW DOOR [17WV1]

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
ASM 315405
AMM 52-71-00-820-002	Adjustment of the Proximity Switches of the Passenger/Crew Doors with the CHECKING TOOL-DOORS
AMM 52-71-11-000-001	Removal of the Proximity Switches of the Passenger/Crew Doors
AMM 52-71-11-400-001	Installation of the Proximity Switches of the Passenger/Crew Door
ASM 527301

3. Fault Confirmation
Subtask 52-13-00-860-068-A

A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.

Subtask 52-13-00-865-057-A

B. Make sure that this(these) circuit breaker(s) is(are) closed:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
121VU	EIS/SLIDES/ARM AND WARN/GND	13WN	P10

Subtask 52-13-00-710-068-A

C. Test
(1) Make sure that the SLIDE ARMED indicator light of the L aft passenger/crew door is on when the door is locked with the handle of the escape slide in the ARMED position.

4. Fault Isolation
Subtask 52-13-00-810-069-A

A. If the test confirms the fault:

disconnect the connector of the handle proximity switch (17WV1)
install the jumper wire between the pins B and C of the connector (17WV1-A) ASM 315405
do the test given in Para 3.B.

(1) If the test confirms the fault:

do a check for a ground signal at pin C of the handle proximity switch (17WV1) ASM 315405.

(a) If there is no ground signal:

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 ASM 315405 and ASM 527301.

(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 AMM 52-71-00-820-002 or with the ECAM system AMM 52-71-00-820-002.

(a) If the fault continues:

replace the PROX SW-HANDLE, L AFT PAX/CREW DOOR [17WV1] AMM 52-71-11-000-001 and AMM 52-71-11-400-001.

Subtask 52-13-00-710-069-A

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.

5. Close-up
Subtask 52-13-00-860-069-A

A. Put the aircraft back to its initial configuration.
(1) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.

[Rev.8 from Aug 2018] 2026.04.04 04:34:46 UTC