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ACTION RESULT
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R R R R R 2. On the FWD left passenger/crew door, pull the inner control handle of the door up until the visual indicator is in the UNLOCKED position. On the lower ECAM display unit, on theDOOR/OXY page: - the CABIN message and the symbol for the FWD left passenger/crew door come on view in amber. The SLIDE message stays on view in white.
On the FWD left passenger/crew door: - the SLIDE ARMED indicator light (1WN1) comes on.
R R 3. On the FWD left passenger/crew door: - put the emergency control in the DISARMED position. Install the SAFETY PIN - SLIDE ARMING (98D52103500000). - push the inner control handle of the door down until the visual indicator is in the LOCKED position. On the lower ECAM display unit, on theDOOR/OXY page: - the SLIDE message goes off.On the FWD left passenger/crew door:- the SLIDE ARMED indicator light(1WN1) goes off.- the symbol of the FWDleft passenger/crew door becomesgreen. The CABIN message goes off.
4. Do the tests in paragraphs 1 to 3 for the FWD right, rear left and rear right passenger/crew doors 832, 841, 842.
NOTE : The SLIDE ARMED indicator____ light (1WN2) is on at the FWD right door. The SLIDE ARMED indicator light (3WN1) is on at the aft left door. The SLIDE ARMED
indicator light (3WN2) is on at the aft right door.
5. Close-up________
Subtask 52-73-00-865-051
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1WL, 2WL, 3WL
B. Energize the aircraft electrical circuits
(1)
Do an EIS stop procedure (Ref. TASK 31-60-00-860-002) Subtask 52-73-00-410-053
C. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Obey the special precautions after work on the door. (Ref. TASK 52-10-00-860-002)
(3)
Close the FWD passenger/crew door 831 (Ref. TASK 52-10-00-410-001).
(4)
Remove the access platform(s). Subtask 52-73-00-862-050
D. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 52-73-00Page 505 1 1 May 01/04R 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-149, 201-299,
TASK 52-73-00-710-002
Operational Test of the Warning System related to the Emergency Exits
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
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REFERENCE QTY DESIGNATION
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No specific circuit breaker(s) safety clip(s)
B. Referenced Information
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REFERENCE DESIGNATION
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24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
52-73-00-991-001 Fig. 501
3. Job Set-up
__________
Subtask 52-73-00-861-051
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 52-73-00Page 506 1 1 May 01/05 1 1 1CES 1 Subtask 52-73-00-860-056
B. Aircraft Maintenance Configuration
(1)
Do an EIS start procedure (Ref. 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
C. Make sure that this(these) circuit breaker(s) is(are) closed: -------------------------------------------------------------------------------
PANEL ------ DESIGNATION ------------------------------------------------------- IDENT. LOCATION------------------
121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11
121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10
Subtask 52-73-00-865-057
D. Open, safety and tag this(these) circuit breaker(s):
------PANEL -------------------------------------------------------DESIGNATION ------------------IDENT. LOCATION
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