_______________________________________________________________ ADJUSTMENT/TEST
_______________
TASK 52-73-00-710-001
Operational Test of the Emergency Escape Slide Release System of the Passenger/Crew Doors
1. Reason for the Job
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Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific access platform 4.40 m (14 ft. 5 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
Door 52-10-00-860-002 Special Precautions after Work on the Passenger/Crew Door
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3. Job Set-up
__________
Subtask 52-73-00-861-050
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
Subtask 52-73-00-010-053
B. Get Access 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:
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-
THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
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THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
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 front of the FWD passenger/crew door.
(2)
Open the passenger/crew door (Ref. TASK 52-10-00-010-001).
R (3) Obey the special precautions before you start work on the door R (Ref. TASK 52-10-00-860-001).
(4) Close the door from the inside (Ref. TASK 52-10-00-410-001).
Subtask 52-73-00-860-055
C. Aircraft Maintenance Configuration
(1)
Do an EIS start procedure (Ref. TASK 31-60-00-860-001).
(2)
Set the DOOR Page.
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Subtask 52-73-00-865-050
D. 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 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
Subtask 52-73-00-865-056
E. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU LIGHTING/EMER LT/CABIN 2WL H06 49VU LIGHTING/EMER LT/CABIN 1WL H05 122VU LIGHTING/CABIN/EMER/LT 3WL V07
4. Procedure_________
Subtask 52-73-00-710-050
R A. Test of the Emergency Escape-Slide Release-Mechanism.
WARNING : DO NOT OPEN THE PASSENGER/CREW DOORS._______
(1) Do the test below:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R R R R 1. On the emergency control handle mechanism of the FWD left passenger/crew door 831: - remove the SAFETY PIN - SLIDE ARMING (98D52103500000). - put the emergency control handle in the ARMED position. On the lower ECAM display unit, on theDOOR/OXY page:- the symbol for the FWD left passenger/crew door comes on view in green. - the SLIDE message comes on view in white. On the FWD left passenger/crew door: - The SLIDE ARMED indicator light (1WN1) is off.
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