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
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 27-93-00-860-108-A
Subtask 27-93-00-810-194-B
[Rev.8 from Aug 2018]
2026.04.04 04:28:07 UTC
Failure of the Roll Side Stick Transducer Unit Potentiometer
1. Possible Causes
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 |
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 (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.
B. Test
(1) Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation(1) Not applicable, you cannot confirm this fault on the ground.
Subtask 27-93-00-810-194-B
A. If the post flight report gives the maintenance message:
ELAC1
ELAC1
- replace the ELAC-1 [2CE1] AMM 27-93-34-000-001 and AMM 27-93-34-400-001.
- during the subsequent flights, if this message is shown again, replace the SSTU-ROLL CTL, CAPT [4CE1] AMM 27-92-41-000-002 AMM 27-92-41-400-002
- during the subsequent flights, if this message is shown again, replace the SSTU-ROLL CTL, F/O [4CE2] AMM 27-92-41-000-002 AMM 27-92-41-400-002