W DOC AIRBUS | TSM A320F

Failure of the Roll Side Stick Transducer Unit Potentiometer


TASK 27-93-00-810-939-A
Failure of the Roll Side Stick Transducer Unit Potentiometer


1. Possible Causes
  • ELAC-1 [2CE1]
  • SSTU-ROLL CTL, CAPT [4CE1]
  • SSTU-ROLL CTL, F/O [4CE2]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 27-93-00-810-986-A
Failure of the Roll Side Stick Transducer Unit Potentiometer (New-Generation Side-Stick Unit)
AMM 27-92-41-000-002
Removal of the Transducer Units
AMM 27-92-41-400-002
Installation of the Transducer Units
AMM 27-92-41-860-801
Identification of the Side Stick Installed on the Aircraft
AMM 27-93-34-000-001
Removal of the ELAC
AMM 27-93-34-400-001
Installation of the ELAC
3. Fault Confirmation
Subtask 27-93-00-860-108-A
A. Side Stick Identification
   (1) Do the identification of the side stick installed on the aircraft AMM 27-92-41-860-801.
     (a) If a new-generation side-stick is unit installed on the aircraft, refer to the trouble shooting procedure (Ref. TSM TASK 27-93-00-810-986).
     (b) If the side stick installed on the aircraft is not a new-generation side-stick unit, continue this procedure.
Subtask 27-93-00-700-175-A
B. Test
   (1) Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
Subtask 27-93-00-810-194-B
A. If the post flight report gives the maintenance message:
ELAC1
[Rev.8 from Aug 2018] 2026.04.04 04:28:07 UTC