W DOC AIRBUS | TSM A320F

Door Bottle Pressure (LH Aft Emergency Exit) - Fault


TASK 52-22-00-810-808-A
Door Bottle Pressure (LH Aft Emergency Exit) - Fault


1. Possible Causes
  • ACTUATOR EMERGENCY EXIT [1602WM]
  • CYL-DAMPER & EMER OPER, AFT EMER EXIT DR L (360RH7)
  • aircraft wiring
  • DEU-B [300RH6]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 23-73-00-810-827-A
DEU-B - Fault in DEU-B 300RHx with connected systems/devices
TSM TASK 52-22-00-810-815-A
Pressure Leakage on the Door Damper and Emergency Operation Cylinder
AMM 23-73-00-740-005
BITE-Test of the Cabin Intercommunication Data System (CIDS) through the CFDS
ASM 237325
AMM 52-22-00-010-001
Opening of the Emergency Exit Doors from the Passenger Compartment
AMM 52-22-00-614-002
Charging of the Door Damper and Emergency Operation Cylinders at the Emergency Exit Doors
AMM 52-22-14-000-001
Removal of the Door Damper and Emergency Operation Cylinder
3. Fault Confirmation
Subtask 52-22-00-710-054-A ** ON A/C NOT FOR ALL
A. Do the bite test of the cabin intercommunication data system through the CFDS AMM 23-73-00-740-005.
4. Fault Isolation
Subtask 52-22-00-810-054-C ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message 520000 DOOR BTL 3L/DEU B (300RH6):
  • open the LH Aft emergency-exit door AMM 52-22-00-010-001 and look at the pressure indicator of the ACTUATOR EMERGENCY EXIT [1602WM] .
   (1) If the pressure indicator shows less than 1783 psi (122.9335 bar):
     (a) If the pressure decreases again:
   (2) If the fault continues:
  • do a check for continuity between:
    the pins A and B of the CYL-DAMPER & EMER OPER, AFT EMER EXIT DR L (360RH7) ASM 237325.
     (a) If there is no continuity:
   (3) If the fault continues:
  • do a check and repair as necessary the aircraft wiring between:
    the pin C/38 of the DEU-B [300RH6] and the receptacle pin B of the CYL-DAMPER & EMER OPER, AFT EMER EXIT DR L (360RH7) ASM 237325.
     (a) If the fault continues:
  • do a check and repair as necessary the aircraft wiring between:
    the pin A of the CYL-DAMPER & EMER OPER, AFT EMER EXIT DR L (360RH7) and GND ASM 237325.
   (4) If the fault continues:
Subtask 52-22-00-710-055-A ** ON A/C NOT FOR ALL
B. Do the test as given in para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:34:50 UTC