- do a check and repair as necessary the aircraft wiring between: the pin C/39 of the DEU-B (300RH4) and the receptacle pin B of the CYL-DAMPER & EMER OPER, AFT EMER EXIT DR R (360RH8) (Ref. ASM 23-73/11), the receptacle pin A of the CYL-DAMPER & EMER OPER, AFT EMER EXIT DR R (360RH8) and GND (Ref. ASM 23-73/10).

 (4) If the fault continues:

 - do a trouble shooting procedure of the ACTUATOR EMERGENCY EXIT (1603WM) (Ref. TASK 23-73-00-810-827).
 B. Do the test as given in para. 3.

 TASK 52-22-00-810-810

 Water Seepage at the Emergengy Exit Doors
 1. Possible Causes

_______________

 2. Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 52-22-00-010-001 Opening of the Emergency Exit Doors from the
 Passenger Compartment
 AMM 52-22-00-860-003 Special Precaution before Maintenance on the Door
 Damper and Emergency Operation Cylinder
 AMM 52-22-00-860-004 Special Precaution after Maintenance on the Door
 Damper and Emergency Operation Cylinder
 AMM 52-22-18-300-001 Preventive Seepage Procedure

 3. Fault Confirmation
__________________
 A. Visual Inspection
 (1) Open the applicable emergency exit door and make sure that the access platform is in postion below the opened door (Ref. AMM TASK 52-22-00-010-001).

 (2) Make sure that the special precaution procedure on the door damper and emergency operation cylinder is done (Ref. AMM TASK 52-22-00-860-003).

 (3) Visual inspect the lower area of the sealing profile above the opened emergency exit door.

 4. Fault Isolation
_______________
 A. If the sealing profile above the emergency exit door is moist:
 - do the preventive seepage procedure of the sealing profile (Ref. AMM TASK 52-22-18-300-001).
 5. Close-up
________
 A. Aircraft Maintenance Configuration
 (1) Make sure that the special precaution procedure on the door damper and emergency operation cylinder is done (Ref. AMM TASK 52-22-00-860-004).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞52-22-00∞∞∞∞∞∞∞∞∞∞Page 225
 May 01/04 CES (2) Close the applicable emergency exit door and remove the access platform (Ref. AMM TASK 52-22-00-010-001).

 TASK 52-22-00-810-811

 No SLIDE Indication on the DOOR/OXY Page for the LH FWD Emergency Exit when the Slide Control handle is in the Slide Armed Position
 1. Possible Causes
_______________
 - IND LT-SLIDE ARMED, AFT L EMERGENCY EXIT (21WN1)

 - PROX SW-HANDLE, L FWD EMER EXIT ESC SLIDE (5WN1)

 - RELAY-PWR SPLY SWITCH OVER (12WN)

 - aircraft wiring

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 AMM 31-60-00-860-001 EIS Start Procedure
 AMM 52-71-00-820-009 Adjustment of the Proximity Switches (5WN1, 5WN2,

 6WN1, 6WN2) of the Emergency Exits AMM 52-73-11-000-003 Removal of the Proximity Switches (5WN1, 5WN2) of the FWD Emergency Exits AMM 52-73-11-400-003 Installation of the Proximity Switches (5WN1, 5WN2) of the FWD Emergency Exits AMM 52-73-21-000-003 Removal of the SLIDE ARMED Indicator-Light (2WN1, 2WN2) of the Emergency Exit AMM 52-73-21-400-003 Installation of the SLIDE ARMED Indicator-Light
 (2WN1, 2WN2) of the Emergency Exit
 ASM 52-73/01
 ASM 52-73/01

 3. Fault Confirmation
__________________
 A. Job Set-up
 (1) Aircraft Maintenance Configuration
 (a) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).

 (b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞52-22-00∞∞∞∞∞∞∞∞∞∞Page 227
　
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