W DOC AIRBUS | TSM A320F

Failure of the Left Blue Elevator-Servocontrol Mode-Transducer


TASK 27-30-00-810-809-A
Failure of the Left Blue Elevator-Servocontrol Mode-Transducer


1. Possible Causes
  • SERVO CTL-L ELEVATOR, OUTBD B [34CE3]
  • wiring of the MODE XDCR SPLY signal from the servocontrol (34CE3) to the first terminal block
  • wiring of the MODE XDCR V1 signal from the servocontrol (34CE3) to the first terminal block
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 27-90-00-810-824-A
Loss of the ACS1 Signal of the ELAC2 MON Side and SEC2 MON Side
TSM TASK 31-32-00-810-933-A
Failure of the Analog Links
AMM 27-34-51-000-006
Removal of the Elevator Servo Control Actuator Mode Selector Valve Transducer MSVT
AMM 27-34-51-400-005
Installation of the Elevator Servo Control Actuator Mode Selector Valve Transducer MSVT
ASM 279308
ASM 279408
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)
3. Fault Confirmation
Subtask 27-30-00-700-062-A
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.
     (a) If the ground scanning gives the maintenance message:
L B ELEV MODE XDCR 34CE3
  • refer to Para. Fault Isolation.
     (b) If the ground scanning gives at least two maintenance messages of the list below:
L B ELEV MODE XDCR 34CE3
L ELEV POS MON XDCR OF ELAC2/SEC2
R B ELEV MODE XDCR 34CE4
R Y ELEV POS MON XDCR OF ELAC2/SEC2
ELAC2 MON OR INPUT OF THS ACTR XDCR1 9CE
SEC2 MON OR INPUT OF THS ACTR XDCR3 9CE
4. Fault Isolation
Subtask 27-30-00-810-056-A
A. If the test gives the maintenance message:
L B ELEV MODE XDCR 34CE3
   (1) If the fault continues:
NOTE: The resistance of the primary winding of the elevator servocontrol mode-transducer (pins C/K and C/L) must be 96 ohms +/- 10 ohms, and the resistance of the secondary winding of the elevator servocontrol mode-transducer (pins (C/U and C/J) must be 700 ohms +/- 70 ohms. The insulation must be more than 10 Mohms.
  • These values are given for information only. You can use these values to do a check of the component electrical part of the wiring before you replace the component. But by this procedure, the check of the component mechanical part is not done.
    For primary winding (power supply):
  • If you do the resistance check from the avionics compartment, you must disconnect the transducer of the Right Blue Elevator Servo Control.
   (2) If the fault continues:
     (a) Do a check of the wiring of the MODE XDCR SPLY signal from the servocontrol (34CE3) to the first terminal block ASM 279308:
  • if there is continuity, see Para. (b)
  • if there is no continuity, repair the above wiring.
     (b) Repair the wiring of the MODE XDCR V1 signal from the servocontrol (34CE3) to the first terminal block ASM 279308.
Subtask 27-30-00-700-063-A
B. Do the tests given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:27:31 UTC