Operational Test of the Warning System Related to the Emergency Exit Doors

TASK 52-73-00-710-002-A
Operational Test of the Warning System Related to the Emergency Exit Doors

WARNING: DO NOT OPEN THE EMERGENCY EXITS.

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER

B. Referenced Information

REFERENCE	DESIGNATION
TASK 24-41-00-861-002-A	Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01	Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02	Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A	De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01	De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02	De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure
TASK 52-71-13-400-001-A	Installation of the Proximity Switches
Disarming of the Emergency Exit Doors

3. Job Set-up
Subtask 52-73-00-861-051-A ** ON A/C NOT FOR ALL

A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).

Subtask 52-73-00-860-056-A ** ON A/C NOT FOR ALL

B. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(2) On the ECAM control panel, push the DOOR key (the "DOOR/OXY" page comes into view).

Subtask 52-73-00-865-052-A ** ON A/C NOT FOR ALL

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

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	EIS/SLIDES/ARM AND WARN/FLT	15WN	P11
121VU	EIS/SLIDES/ARM AND WARN/GND	13WN	P10

Subtask 52-73-00-865-057-A ** ON A/C NOT FOR ALL

D. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	LIGHTING/EMER LT/CABIN	2WL	H06
49VU	LIGHTING/EMER LT/CABIN	1WL	H05
122VU	LIGHTING/CABIN/EMER/LT	3WL	V07

4. Procedure
Subtask 52-73-00-710-051-A ** ON A/C NOT FOR ALL

A. Operational Test of the Warning System Related to the Emergency Exit Doors

Disarming of the Emergency Exit Doors ** ON A/C NOT FOR ALL

(1) Do the tests that follow:

NOTE: If the task is for FAA MMEL 52-70-01, only the information related to the "SLIDE" indication on the ECAM "DOOR/OXY" page is applicable.

ACTION	RESULT
1.On the forward left hatch (forward left emergency-exit-door): Pull the cover flap (2) down. Remove the cover flap (2) from the hatch lining.	On the lower ECAM DU, on the "DOOR/OXY" page: The symbol of the forward left emergency-exit-door and the "EMER EXIT" message come into view in amber. SLIDE ARMED indicator light 2WN1 (3) comes on.
Turn the head of the latch pin (1) a quarter turn counterclockwise to retract the latch pin to the DISARMED position.	SLIDE ARMED indicator light 2WN1 (3) goes off.
	On the lower ECAM DU, on the "DOOR/OXY" page: The white "SLIDE" indication goes out of view.
2.On the aft left hatch (aft left emergency-exit-door): Pull the cover flap (2) down. Remove the cover flap (2) from the hatch lining.	SLIDE ARMED indicator light 2WN1 (3) comes on.
	On the lower ECAM DU, on the "DOOR/OXY" page: The symbol of the aft left emergency-exit-door comes into view in amber.
Turn the head of the latch pin (1) a quarter turn counterclockwise to retract the latch pin to the DISARMED position.	SLIDE ARMED indicator light 2WN1 (3) goes off.
3.On the forward left hatch (forward left emergency-exit-door): Push the latch pin (1) against the spring. Turn the head of the latch pin (1) a quarter turn clockwise to extend the latch pin in the ARMED position.	SLIDE ARMED indicator light 2WN1 (3) comes on.
Install the cover flap (2) on the hatch lining. Push the cover flap (2) against the hatch.	The symbol of the forward left emergency-exit-door becomes green. SLIDE ARMED indicator light 2WN1 (3) goes off.
4.On the aft left hatch (aft left emergency-exit-door): Push the latch pin (1) against the spring. Turn the head of the latch pin (1) a quarter turn clockwise to extend the latch pin in the ARMED position.	SLIDE ARMED indicator light 2WN1 (3) comes on.
	On the lower ECAM DU, on the "DOOR/OXY" page: The white "SLIDE" indication comes into view.
Install the cover flap (2) on the hatch lining. Push the cover flap (2) against the hatch.	SLIDE ARMED indicator light 2WN1 (3) goes off.
	On the lower ECAM DU, on the "DOOR/OXY" page: The symbol of the aft left emergency-exit-door becomes green. The "EMER EXIT" message goes out of view.

(2) Make sure that the clearance between the target and the related proximity switch is in the limits (Ref. AMM TASK 52-71-13-400-001).
(3) Do steps (1) and (2) for the right emergency-exit doors.

NOTE: The forward right hatch is on the forward right emergency-exit-door and the aft right hatch is on the aft right emergency-exit-door.

NOTE: The FIN of the SLIDE ARMED indicator light (3) on the right emergency-exit-door is 2WN2.

5. Close-up
Subtask 52-73-00-865-053-A ** ON A/C NOT FOR ALL

A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	LIGHTING/EMER LT/CABIN	2WL	H06
49VU	LIGHTING/EMER LT/CABIN	1WL	H05
122VU	LIGHTING/CABIN/EMER/LT	3WL	V07

Subtask 52-73-00-860-057-A ** ON A/C NOT FOR ALL

B. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).

Subtask 52-73-00-862-051-A ** ON A/C NOT FOR ALL

C. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.02 06:28:34 UTC