Operational Test of the Emergency Escape-Slide Release-System of the Passenger/Crew Doors

TASK 52-73-00-710-001-A
Operational Test of the Emergency Escape-Slide Release-System of the Passenger/Crew Doors

WARNING: DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE THAN 65 KNOTS.

WARNING: BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT:

THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.

IF YOU DO NOT OBEY THESE INSTRUCTIONS, THE DOOR CAN OPEN WITH FORCE OR THE ESCAPE SLIDE CAN DEPLOY SUDDENLY. THIS CAN CAUSE INJURY AND/OR DAMAGE.

WARNING: STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES. IF THE RED WARNING LIGHT FLASHES, REMAINING PRESSURE CAN CAUSE THE DOOR TO OPEN SUDDENLY AND CAN:

KILL OR CAUSE SERIOUS INJURY TO PERSONS
CAUSE DAMAGE TO THE AIRCRAFT.

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	ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
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 52-10-00-010-001-A	Opening of the Passenger/Crew Door
TASK 52-10-00-410-001-A	Closing of the Passenger/Crew Door
TASK 52-10-00-860-001-A	Special Precautions before Work on the Passenger/Crew Door
TASK 52-10-00-860-002-A	Special Precautions after Work on the Passenger/Crew Door

3. Job Set-up
Subtask 52-73-00-861-050-A

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

Subtask 52-73-00-010-053-A

B. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in front of forward passenger/crew door 831.
(2) Open the passenger/crew door (Ref. AMM TASK 52-10-00-010-001).
(3) Obey the special precautions before you start work on the door (Ref. AMM TASK 52-10-00-860-001).
(4) Close the door from the inner side of the aircraft (Ref. AMM TASK 52-10-00-410-001).

Subtask 52-73-00-860-055-A

C. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).

Subtask 52-73-00-865-050-A

D. 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/FLT	15WN	P11
121VU	EIS/SLIDES/ARM AND WARN/GND	13WN	P10
121VU	EIS/SDAC1 AND 2/DOOR/DET/PAX	48WV	P05

Subtask 52-73-00-865-056-A

E. 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
** ON A/C NOT FOR ALL
49VU	LIGHTING/EMER LT/CABIN	2WL	H04
49VU	LIGHTING/EMER LT/CABIN	1WL	H03
** ON A/C ALL
122VU	LIGHTING/CABIN/EMER/LT	3WL	V07

4. Procedure
Subtask 52-73-00-710-050-A

A. Test of the Emergency Escape-Slide Release-System

WARNING: DO NOT OPEN THE PASSENGER/CREW DOORS.

(1) Do the tests that follow:
(a) Do the tests in paragraphs 1 thru 5 for the forward passenger/crew door (831/841) and for the aft passenger/crew door (832/842).

NOTE: The SLIDE ARMED indicator light (1WN1/1WN2) is on at the forward passenger/crew door (831/841). The SLIDE ARMED indicator light (3WN1/3WN2) is on at the aft passenger/crew door (832/842).

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 lower ECAM DU: Open the "DOOR/OXY" page.	On the lower ECAM DU, on the "DOOR/OXY" page: The green symbol for the passenger/crew door comes into view.
2.On the emergency control-handle mechanism of the passenger/crew door: Remove the 98D52103500000 SAFETY PIN - SLIDE ARMING. Set the emergency control handle to the ARMED position.	On the lower ECAM DU, on the "DOOR/OXY" page: The white "SLIDE" message comes into view.
	On the passenger/crew door: The SLIDE ARMED indicator light is off.
3.On the passenger/crew door: Hold the door and pull the inner control handle of the door up until the visual indicator shows UNLOCKED.	On the lower ECAM DU, on the "DOOR/OXY" page: The "CABIN" message and the amber symbol for the passenger/crew door come into view. The white "SLIDE" message stays shown.
	On the passenger/crew door: The SLIDE ARMED indicator light comes on.
4.On the passenger/crew door: Push the inner control handle of the door down until the visual indicator shows LOCKED.	On the passenger/crew door: The SLIDE ARMED indicator light goes off.
	On the lower ECAM DU, on the "DOOR/OXY" page: The symbol for the passenger/crew door becomes green. The "CABIN" message goes out of view.
5.On the passenger/crew door: Set the emergency control handle to the DISARMED position. Install the 98D52103500000 SAFETY PIN - SLIDE ARMING.	On the lower ECAM DU, on the "DOOR/OXY" page: The white "SLIDE" message goes out of view.

5. Close-up
Subtask 52-73-00-865-051-A

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
** ON A/C NOT FOR ALL
49VU	LIGHTING/EMER LT/CABIN	2WL	H04
49VU	LIGHTING/EMER LT/CABIN	1WL	H03
** ON A/C ALL
122VU	LIGHTING/CABIN/EMER/LT	3WL	V07

Subtask 52-73-00-860-054-A

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

Subtask 52-73-00-410-053-A

C. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Obey the special precautions after you do the work on the door (Ref. AMM TASK 52-10-00-860-002).
(3) Close forward passenger/crew door 831 (Ref. AMM TASK 52-10-00-410-001).
(4) Remove the access platform(s).

Subtask 52-73-00-862-050-A

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

[Rev.10 from 2021] 2026.04.01 01:48:18 UTC