Failure of the Right Blue Aileron Servo Control Servovalve
TASK 27-10-00-810-830-A
Failure of the Right Blue Aileron Servo Control Servovalve
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 27-10-00-700-095-A ** ON A/C NOT FOR ALL
Subtask 27-10-00-810-079-A
[Rev.8 from Aug 2018]
2026.04.04 04:27:28 UTC
Failure of the Right Blue Aileron Servo Control Servovalve
1. Possible Causes
- servovalve of the servo control 33CE4
wiring POS XDCR signal from the servocontrol (33CE4) to the ELAC 2 (2CE2) COM and MON side - ELAC-2 [2CE2]
- SERVO CTL-R AILERON, OUTBD B [33CE4]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 27-10-00-810-814-A | Disagree between COM & MON Aileron Order Signal in the ELAC 2 |
| AMM 27-14-51-000-001 | Removal of the Aileron Servo Control |
| AMM 27-14-51-000-003 | Removal of the Aileron Servo-Control Servovalve |
| AMM 27-14-51-400-001 | Installation of the Aileron Servo Control |
| AMM 27-14-51-400-003 | Installation of the Aileron Servo-Control Servovalve |
| ASM 279303 | |
| AMM 27-93-34-000-001 | Removal of the ELAC |
| AMM 27-93-34-400-001 | Installation of the ELAC |
| AMM 27-96-00-710-020 | Operational Test of the Side Stick Assembly (Activation for the BITE Test) |
| AMM 27-96-00-740-001 | BITE Test of the EFCS (Ground Scanning) |
| AMM 29-10-00-863-001 | Pressurize the Green Hydraulic System with a Hydraulic Ground Power-Cart |
| AMM 29-10-00-863-002 | Pressurize the Yellow Hydraulic System with a Hydraulic Ground Power-Cart |
| AMM 29-10-00-863-003 | Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart |
Subtask 27-10-00-700-095-A ** ON A/C NOT FOR ALL
A. Test
(1) Make sure that all the hydraulic systems are depressurized.
(2) On the overhead panel 23VU:
(5) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
(6) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
(a) If the ground scanning gives the maintenance message:
R B AIL SERVO VLV 33CE4
Subtask 27-10-00-700-095-B ** ON A/C NOT FOR ALL (1) Make sure that all the hydraulic systems are depressurized.
(2) On the overhead panel 23VU:
- Release the FLT CTL/ELAC 1 pushbutton switch (the OFF legend of the FLT CTL/ELAC 1 pushbutton switch comes on).
- Push the FLT CTL/ELAC 1 pushbutton switch (the OFF legend of the FLT CTL/ELAC 1 pushbutton switch goes off).
NOTE: In case of a reset of the ELAC 1 with the circuit breaker, the supply breaking must be more than 5 seconds.
NOTE: If the ELAC FAULT warning disappears after several resets, replace the computer.
(4) Pressurize all the hydraulic systems AMM 29-10-00-863-001, AMM 29-10-00-863-002 and AMM 29-10-00-863-003. (5) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
(6) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
(a) If the ground scanning gives the maintenance message:
R B AIL SERVO VLV 33CE4
- Refer to the Para. Fault Isolation.
A. Test
(1) Do a check of the Post Flight Report (PFR)
If the R B AIL SERVO VLV 33CE4 maintenance message is shown in flight phase 08 (PH08):
(a) On the overhead panel, on the FLT CTL panel 24VU: release, then push the FLT CTL/ELAC2 pushbutton switch.
(b) Make an entry in the logbook to monitor the aircraft during the subsequent flight.
(c) During the subsequent flight:
(3) On the overhead panel 23VU:
(6) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
(7) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
(a) If the ground scanning gives the maintenance message:
R B AIL SERVO VLV 33CE4
4. Fault Isolation(1) Do a check of the Post Flight Report (PFR)
If the R B AIL SERVO VLV 33CE4 maintenance message is shown in flight phase 08 (PH08):
(a) On the overhead panel, on the FLT CTL panel 24VU: release, then push the FLT CTL/ELAC2 pushbutton switch.
(b) Make an entry in the logbook to monitor the aircraft during the subsequent flight.
(c) During the subsequent flight:
- If the fault occurs again, continue the trouble shooting procedure.
(3) On the overhead panel 23VU:
- Release the FLT CTL/ELAC 1 pushbutton switch (the OFF legend of the FLT CTL/ELAC 1 pushbutton switch comes on).
- Push the FLT CTL/ELAC 1 pushbutton switch (the OFF legend of the FLT CTL/ELAC 1 pushbutton switch goes off).
NOTE: In case of a reset of the ELAC 1 with the circuit breaker, the supply breaking must be more than 5 seconds.
NOTE: If the ELAC FAULT warning disappears after several resets, replace the computer.
(5) Pressurize all the hydraulic systems AMM 29-10-00-863-001, AMM 29-10-00-863-002 and AMM 29-10-00-863-003. (6) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
(7) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
(a) If the ground scanning gives the maintenance message:
R B AIL SERVO VLV 33CE4
- Refer to the Para. Fault Isolation.
Subtask 27-10-00-810-079-A
A. If the test gives the maintenance message:
R B AIL SERVO VLV 33CE4
(1) Do a check of the Previous Leg Reports (PLR) to see if there is the ELAC2 AIL ORDER DISAGREE maintenance message:
(a) If this maintenance message is shown, refer to the trouble shooting procedure (Ref. TSM TASK 27-10-00-810-814).
(b) If this maintenance message is not shown:
Subtask 27-10-00-700-096-A R B AIL SERVO VLV 33CE4
(1) Do a check of the Previous Leg Reports (PLR) to see if there is the ELAC2 AIL ORDER DISAGREE maintenance message:
(a) If this maintenance message is shown, refer to the trouble shooting procedure (Ref. TSM TASK 27-10-00-810-814).
(b) If this maintenance message is not shown:
- Replace the servovalve of the servo control 33CE4 , AMM 27-14-51-000-003 and AMM 27-14-51-400-003.
- At the 33CE4 receptacle, do a check of the resistance between pin E and pin F ASM 279303.
NOTE: The resistance must be 500 ohms +/- 10 %.
(2) If the fault continues: - Do a check of the
wiring POS XDCR signal from the servocontrol (33CE4) to the ELAC 2 (2CE2) COM and MON side , ASM 279303.
- Replace the ELAC-2 [2CE2] , AMM 27-93-34-000-001 and AMM 27-93-34-400-001.
- Replace the SERVO CTL-R AILERON, OUTBD B [33CE4] , AMM 27-14-51-000-001 and AMM 27-14-51-400-001.
B. Do the test given in Para. 3.