W DOC AIRBUS | TSM A320F

Loss of the Pitch Change Over Signal by the ELAC 1


TASK 27-93-00-810-931-A
Loss of the Pitch Change Over Signal by the ELAC 1


1. Possible Causes
  • ELAC-1 [2CE1]
  • wiring of the PITCH AXIS OK (DSO 09) signal from the ELAC 1 COM part to the MON part (DSI 12)
  • wiring of the PITCH AXIS OK (DSO 09) signal from the ELAC 1 MON part to the COM part (DSI 12)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 31-32-00-810-932-A
Failure of the Discrete Links
ASM 279233
AMM 27-93-34-000-001
Removal of the ELAC
AMM 27-93-34-400-001
Installation of the ELAC
AMM 27-96-00-740-001
BITE Test of the EFCS (Ground Scanning)
3. Fault Confirmation
Subtask 27-93-00-740-186-A
A. Test
   (1) Check the PN of the FCDCs fitted on the aircraft:
     (a) If the PN of the FCDCs is 115370-0105, you cannot confirm the fault, do the fault isolation.
     (b) If the PN of the FCDCs is different from 115370-0105, do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
4. Fault Isolation
Subtask 27-93-00-810-180-A
A. If you cannot confirm the fault (FCDC PN 115370-0105) or if the BITE test gives the maintenance message CHECK PITCH CHANGE OVER WIRING OF ELAC1:
   (1) If the fault continues:
     (a) Do the trouble shooting procedure (Ref. TSM TASK 31-32-00-810-932) related to the:
  • PITCH AXIS OK (DSO 09) signal ELAC 1 COM part ASM 279233
  • PITCH AXIS OK (DSO 09) signal ELAC 1 MON part ASM 279233
   (2) If the fault continues:
     (a) Do a check of the wiring of the PITCH AXIS OK (DSO 09) signal from the ELAC 1 COM part to the MON part (DSI 12) ASM 279233.
  • if there is continuity, see para. (b)
  • if there is no continuity, repair the above wiring.
     (b) Do a check and repair the wiring of the PITCH AXIS OK (DSO 09) signal from the ELAC 1 MON part to the COM part (DSI 12) ASM 279233.
Subtask 27-93-00-740-187-A
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:39:09 UTC