W DOC AIRBUS | TSM A320F

Failure of the Thrust Reverser Deploy Indication


TASK 78-31-00-810-870-A
Failure of the Thrust Reverser Deploy Indication


1. Possible Causes
  • harnesses J5 and J6
  • thrust reverser harness
  • SW-BLOCKER DOOR DEPLOY, L [4103KS1]
  • SW-BLOCKER DOOR DEPLOY, R [4103KS2]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 78-31-00-810-869-A
Slow Operation or non Deployment of the Thrust Reverser
AMM 71-51-43-000-049
Removal of the ECU (Channel A) to Thrust Reverser Junction Box Harnesses
AMM 71-51-43-400-049
Installation of the ECU (Channel A) to Thrust Reverser Junction Box Harnesses
AMM 71-51-44-000-002
Removal of the Thrust Reverser Harness 238W0908
AMM 71-51-44-400-002
Installation of the Thrust Reverser Harness 238W0908
AMM 78-31-00-710-040
Operational Test of the Thrust Reverser System
AMM 78-31-00-710-042
Operational Test of the Thrust Reverser System
AMM 78-31-17-000-001
Removal of the Blocker Door Deploy Switch
AMM 78-31-17-000-002
Removal of the Beam Electrical Harness
AMM 78-31-17-000-040
Removal of the Blocker Door Deploy Switch
AMM 78-31-17-000-041
Removal of the Beam Electrical Harness
AMM 78-31-17-210-001
Detailed Visual Inspection of the Deploy Switches and Triggers
AMM 78-31-17-210-040
Detailed Visual Inspection of the Deploy Switches and Triggers
AMM 78-31-17-400-001
Installation of the Blocker Door Deploy Switch
AMM 78-31-17-400-002
Installation of the Beam Electrical Harness
AMM 78-31-17-400-040
Installation of the Blocker Door Deploy Switch
AMM 78-31-17-400-041
Installation of the Beam Electrical Harness
AMM 78-32-41-000-001
Removal of the Lower Blocker Door
AMM 78-32-41-000-002
Removal of the Upper Blocker Door
AMM 78-32-41-000-040
Removal of the Lower Blocker Door
AMM 78-32-41-000-041
Removal of the Upper Blocker Door
AMM 78-32-41-400-001
Installation of the Lower Blocker Door
AMM 78-32-41-400-002
Installation of the Upper Blocker Door
AMM 78-32-41-400-040
Installation of the Lower Blocker Door
AMM 78-32-41-400-041
Installation of the Upper Blocker Door
3. Fault Confirmation
Subtask 78-31-00-710-184-A ** ON A/C NOT FOR ALL
A. Test
   (1) Not applicable.
   (2) If the amber REV indication was associated to normal deployment of the blocker doors:
  • do the following procedure.
   (3) If the blocker doors did not deploy:
4. Fault Isolation
Subtask 78-31-00-810-129-A ** ON A/C NOT FOR ALL
A. This fault is generated when the deploy switches indication is intermittent or has failed when reverse is selected. This may cause the engine power to fluctuate between idle and full reverse thrust power.
   (1) Do an inspection of the control levers of the thrust-reverser deploy switches and make sure that they operate smoothly AMM 78-31-17-210-040.
NOTE: Most probable cause is seizure of the deploy switches control levers or intermittent electrical contact in the switches or in the associated harnesses or play between switch outer lever and bushing or outer lever pad damaged or missing or gap between pivot bolt and the bushing.
     (a) If damage is found:
  • repair or replace as required.
     (b) If nothing is found:
  • examine the Post Flight Report and Last Leg Report for fault messages DEPL SW, J5/J6, ECU or DEPLSTW, J5/J6, ECU.
       1 If one of these fault messages is present:
  • do the relevant trouble shooting procedure (Ref TSM CFDS ATA 78).
       2 If no fault message is present:
  • do a check of the harnesses J5 and J6 and the thrust reverser harness from the ECU to the deploy switches for any damage, loose or contaminated connectors including the thrust reverser junction box.
         a If damage is found:
     (c) If nothing is found:
     (d) If nothing is found:
     (e) If nothing is found:
Subtask 78-31-00-710-185-A ** ON A/C NOT FOR ALL
B. Do an operational test of the thrust reverser AMM 78-31-00-710-040 and make sure that the ECAM REV indication is correct. (Amber in transit then green when reverser blocker doors are fully deployed).
Subtask 78-31-00-810-129-B ** ON A/C NOT FOR ALL
C. This fault is generated when the deploy switches indication is intermittent or has failed when reverse is selected. This may cause the engine power to fluctuate between idle and full reverse thrust power.
   (1) Do an inspection of the control levers of the thrust-reverser deploy switches and make sure that they operate smoothly AMM 78-31-17-210-001.
NOTE: Most probable cause is seizure of the deploy switches control levers or intermittent electrical contact in the switches or in the associated harnesses or play between switch outer lever and bushing or outer lever pad damaged or missing or gap between pivot bolt and the bushing.
     (a) If damage is found:
  • repair or replace as required.
     (b) If nothing is found:
  • examine the Post Flight Report and Last Leg Report for fault messages DEPL SW, J5/J6, ECU or DEPLSTW, J5/J6, ECU.
       1 If one of these fault messages is present:
  • do the relevant trouble shooting procedure (Ref TSM CFDS ATA 78).
       2 If no fault message is present:
  • do a check of the harnesses J5 and J6 and the thrust reverser harness from the ECU to the deploy switches for any damage, loose or contaminated connectors including the thrust reverser junction box.
         a If damage is found:
     (c) If nothing is found:
     (d) If nothing is found:
     (e) If nothing is found:
Subtask 78-31-00-710-185-B ** ON A/C NOT FOR ALL
D. Do an operational test of the thrust reverser AMM 78-31-00-710-042 and make sure that the ECAM REV indication is correct. (Amber in transit then green when reverser blocker doors are fully deployed).
[Rev.8 from Aug 2018] 2026.04.04 04:38:05 UTC