Failure of the Left Blue Aileron Servo Control Servovalve
TASK 27-10-00-810-809-A
Failure of the Left Blue Aileron Servo Control Servovalve
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 27-10-00-700-064-A ** ON A/C NOT FOR ALL
Subtask 27-10-00-810-058-A
[Rev.8 from Aug 2018]
2026.04.04 04:27:26 UTC
Failure of the Left Blue Aileron Servo Control Servovalve
1. Possible Causes
- servovalve of the servo control 33CE3
wiring POS XDCR signal from the servocontrol (33CE3) to the ELAC 1 (2CE1) COM and MON side - ELAC-1 [2CE1]
- SERVO CTL-L AILERON, OUTBD B [33CE3]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 27-93-00-810-950-A | Disagree between COM and MON Aileron Order Signals in the ELAC1 |
| 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 279302 | |
| 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) |
Subtask 27-10-00-700-064-A ** ON A/C NOT FOR ALL
A. Test
(1) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
(2) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
Subtask 27-10-00-700-064-B ** ON A/C NOT FOR ALL (1) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
(2) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
A. Test
(1) Do a check of the Post Flight Report (PFR)
If the L B AIL SERVO VLV 33CE3 maintenance message is shown in flight phase 08 (PH08):
(a) On the overhead panel, on the FLT CTL panel 23VU: release, then push the FLT CTL/ELAC1 pushbutton switch.
(b) Make an entry in the logbook to monitor the aircraft during the subsequent flight.
(c) During the subsequent flight:
(3) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
4. Fault Isolation(1) Do a check of the Post Flight Report (PFR)
If the L B AIL SERVO VLV 33CE3 maintenance message is shown in flight phase 08 (PH08):
(a) On the overhead panel, on the FLT CTL panel 23VU: release, then push the FLT CTL/ELAC1 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) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
Subtask 27-10-00-810-058-A
A. If the test gives the maintenance message:
L B AIL SERVO VLV 33CE3
(1) Do a check of the Previous Leg Reports (PLR) to see if there is the ELAC1 AIL ORDER DISAGREE maintenance message:
(a) If this maintenance message is shown, refer to the trouble shooting procedure (Ref. TSM TASK 27-93-00-810-950).
(b) If this maintenance message is not shown:
Subtask 27-10-00-700-065-A L B AIL SERVO VLV 33CE3
(1) Do a check of the Previous Leg Reports (PLR) to see if there is the ELAC1 AIL ORDER DISAGREE maintenance message:
(a) If this maintenance message is shown, refer to the trouble shooting procedure (Ref. TSM TASK 27-93-00-810-950).
(b) If this maintenance message is not shown:
- Replace the servovalve of the servo control 33CE3 , AMM 27-14-51-000-003 and AMM 27-14-51-400-003.
- At the 33CE3 receptacle, do a check of the resistance between pin E and pin F ASM 279302.
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 (33CE3) to the ELAC 1 (2CE1) COM and MON side , ASM 279302.
- Replace the ELAC-1 [2CE1] , AMM 27-93-34-000-001 and AMM 27-93-34-400-001.
- Replace the SERVO CTL-L AILERON, OUTBD B [33CE3] , AMM 27-14-51-000-001 and AMM 27-14-51-400-001.
B. Do the test given in Para. 3.