-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-22-00-860-004 52-73-00-710-002 52-71-00-991-018
FOR FIN 5WN1 25-23-47-000-012
25-23-47-400-012 FOR FIN 5WN2 25-23-47-000-013
25-23-47-400-013
FOR FIN 6WN1 25-23-47-000-013
25-23-47-400-013
FOR FIN 6WN2 25-23-47-000-013
25-23-47-400-013
3. Job Set-up
__________ Subtask 52-71-00-861-066
Special Precaution after Maintenance on the Door Damper and Emergency Operation CylinderOperational Test of the Warning System related to the Emergency ExitsFig. 517
Removal of the Door Linings of the LH FWD Emergency Exit Door, zone 231Installation of the Door Linings of the LH FWD Emergency Exit Door, zone 231
Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232.Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232.
Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232.Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232.
Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232.Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232.
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
1EFF : 301-399, 1 52-71-00Page A516 1 1 May 01/05R 1 1 1CES 1
Subtask 52-71-00-010-081
B. Get Access WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES.
_______ RESIDUAL PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT.
(1)
Put an access platform in position at the applicable emergency exit 833 or 834 or 843 or 844.
(2)
Open the applicable emergency exit 833 or 834 or 843 or 844, (Ref. TASK 52-22-00-010-002).
(3)
Obey the special precautions before you start work on the emergency exit (Ref. TASK 52-22-00-860-003).
(4)
Close the applicable emergency exit 833 or 834 from the inside (Ref. TASK 52-22-00-410-001).
Subtask 52-71-00-010-082
C. Removal of the Lining Panel
(1) Remove the lining panel:
FOR 5WN1
833CZ, (Ref. TASK 25-23-47-000-012).
FOR 5WN2
843CZ, (Ref. TASK 25-23-47-000-013).
FOR 6WN1
834CZ, (Ref. TASK 25-23-47-000-013).
FOR 6WN2
844CZ, (Ref. TASK 25-23-47-000-013).
(2) Remove the insulation blanket. Subtask 52-71-00-860-067
D. Aircraft Maintenance Configuration
(1)
Make sure that all the doors are closed.
(2)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001)
R 1EFF : 301-399, 1 52-71-00Page A517 1 1 May 01/05 1 1 1CES 1
(3) On the ECAM control panel, push the DOOR key: - on the lower ECAM DU the DOOR/OXY page comes into view.
4. Procedure
_________ Subtask 52-71-00-820-075
A. Adjustment of the Proximity Switch
(Ref. Fig. 517/TASK 52-71-00-991-018)
WARNING : DO NOT OPEN THE EMERGENCY EXIT DURING THE ADJUSTMENT.
_______
(1)
Remove the lockwire from the nut (4).
(2)
Loosen the nut (4).
(3)
Turn the target (3) until the symbol of the door is green on the lower ECAM DU.
NOTE : The target (3) and the proximity switch (2) must not be in
____
contact.
(4)
Turn the target (2) in the opposite direction until the symbol is amber on the lower ECAM DU.
(5)
From this position, screw the target (2) by two turns to two turns and a half.
(6)
Tighten the nut (4).
(7) Safety the nut (4) with MISCELLANEOUS (Material No. 19-010). Subtask 52-71-00-710-067
B. Operational Test
(1) Do an operational test of the warning system related to the emergency exits (Ref. TASK 52-73-00-710-002).
5. Close-up
________ Subtask 52-71-00-860-068
A. Put the aircraft back to its initial configuration.
(1) Do an EIS Stop Procedure (Ref. TASK 31-60-00-860-002).
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