W DOC AIRBUS | TSM A320F

DCV Failed Deployed


TASK 78-31-00-810-983-A
DCV Failed Deployed


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 71-00-00-810-843-A
Nacelle Component and Harness Troubleshooting Procedure for Guidance Troubleshooting Intermittent Faults
AMM 29-11-35-000-802
Removal of the Green Engine-1 Thrust-Reverser Check-Valve
AMM 29-11-35-000-803
Removal of the Green Engine-1 Thrust-Reverser Case-Drain Check-Valve
AMM 29-11-35-400-802
Installation of the Green Engine-1 Thrust-Reverser Check-Valve
AMM 29-11-35-400-803
Installation of the Green Engine-1 Thrust-Reverser Case-Drain Check-Valve
AMM 29-13-35-000-802
Removal of the Yellow Engine-2 Thrust-Reverser Check-Valve
AMM 29-13-35-000-803
Removal of the Yellow Engine-2 Thrust-Reverser Case-Drain Check-Valve
AMM 29-13-35-400-802
Installation of the Yellow Engine-2 Thrust-Reverser Check-Valve
AMM 29-13-35-400-803
Installation of the Yellow Engine-2 Thrust-Reverser Case-Drain Check-Valve
AMM 71-13-00-010-802
Opening of the Fan Cowl Doors
AMM 71-13-00-410-802
Closing of the Fan Cowl Doors
AMM 73-21-01-000-801
Removal of the Electronic Engine Control (EEC)
AMM 73-21-01-400-801
Installation of the Electronic Engine Control (EEC)
AMM 78-31-00-710-805
Operational Test of Thrust Reverser with MCDU
AMM 78-31-01-000-801
Removal of the TRAS Hydraulic Control Unit (HCU)
AMM 78-31-01-400-801
Installation of the TRAS Hydraulic Control Unit (HCU)
AMM 78-31-02-610-801
Servicing of the TRAS Filter Module 4314KM1, 4314KM2
AMM 78-31-21-000-801
Removal of the Hydraulic Control Unit (HCU) Pressure Switch
AMM 78-31-21-400-801
Installation of the Hydraulic Control Unit (HCU) Pressure Switch
AMM 78-31-50-000-801
Removal of the TRAS Hydraulic Tubes and Hoses
AMM 78-31-50-400-801
Installation of the TRAS Hydraulic Tubes and Hoses
3. Fault Confirmation
Subtask 78-31-00-710-298-A ** ON A/C NOT FOR ALL
A. Do the operational test of the thrust reverser with the MCDU to confirm this fault AMM 78-31-00-710-805.
   (1) If the maintenance message does not come back, troubleshoot as described in the nacelle component and harness troubleshooting procedure for guidance troubleshooting intermittent faults (Ref. TSM TASK 71-00-00-810-843).
     (a) Monitor the engine for reoccurring maintenance message.
   (2) If the maintenance message comes back (hard fault), go to the Para. Fault Isolation.
4. Fault Isolation
WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS WARNING, INJURY CAN OCCUR.
Subtask 78-31-00-810-327-A ** ON A/C NOT FOR ALL
A. If there is confirmation of the fault:
   (1) Check if both transcowls are stowed and locked.
     (a) If both transcowls are not stowed and locked:
       1 Replace HCU-T/R, ENG1 [4310EG1] or HCU-T/R, ENG2 [4310EG2] AMM 78-31-01-000-801 and AMM 78-31-01-400-801.
       2 Do the test given in Para. 3.
   (2) If both transcowls are stowed and locked or if fault persist:
     (a) Check for clogged TRAS filter (4314KM).
       1 Check on filter module if red button is out.
       2 If red button is out, replace filter element AMM 78-31-02-610-801.
       3 Do the test given in Para. 3.
   (3) If filter is not clogged or the fault continues, inspect for hydraulic leakage.
     (a) Get access to HCU:
       1 Remove the access panel on the pylon to get access to the HCU:
         a FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
         b FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
     (b) Open the fan cowl doors AMM 71-13-00-010-802.
     (c) Inspect hydraulic tubes and hoses between HCU and T piece.
       1 Replace tubes as necessary AMM 78-31-50-000-801 and AMM 78-31-50-400-801.
     (d) If hydraulic leakage is corrected:
       1 Do the test given in Para. 3.
   (4) If the fault continues:
     (a) For fault on ENG 1:
     (b) For fault on ENG 2:
     (c) Do the test given in Para. 3.
   (5) If the fault continues:
     (a) Replace HCU-T/R, ENG1 [4310EG1] or HCU-T/R, ENG2 [4310EG2] AMM 78-31-01-000-801 and AMM 78-31-01-400-801.
     (b) Do the test given in Para. 3.
   (6) If no problem is found or fault continues:
     (a) Replace HCU PRESS SWITCH ENG 1B [103EG1] or HCU PRESS SWITCH ENG 2B [103EG2] AMM 78-31-21-000-801 and AMM 78-31-21-400-801.
     (b) Do the test given in Para. 3.
   (7) If no problem found or fault continues:
     (a) Replace [4000KS] AMM 73-21-01-000-801 and AMM 73-21-01-400-801.
     (b) Do the test given in Para. 3.
5. Close-up
Subtask 78-31-00-860-093-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Make sure that the work area is clean and clear of tools and other items.
     (a) Close the fan cowl doors AMM 71-13-00-410-802.
     (b) Close the pylon access panel:
       1 FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
       2 FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
[Rev.8 from Aug 2018] 2026.04.04 04:38:18 UTC