W DOC AIRBUS | TSM A320F

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
  • 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]
2. Job Set-up Information
 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
3. Fault Confirmation
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:
  • Release the FLT CTL/ELAC 1 pushbutton switch (the OFF legend of the FLT CTL/ELAC 1 pushbutton switch comes on).
   (3) On the overhead panel 23VU:
  • 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.
     (b) If the test gives a different maintenance message, do the trouble shooting procedure related to this message.
Subtask 27-10-00-700-095-B ** ON A/C NOT FOR ALL
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:
  • If the fault occurs again, continue the trouble shooting procedure.
   (2) Make sure that all the hydraulic systems are depressurized.
   (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).
   (4) On the overhead panel 23VU:
  • 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.
     (b) If the test gives a different maintenance message, do the trouble shooting procedure related to this message.
4. 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:
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.
   (3) If the fault continues:
   (4) If the fault continues:
Subtask 27-10-00-700-096-A
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:27:28 UTC