W DOC AIRBUS | TSM A320F

Failure of the Left or Right Pedal Position Transducer Unit for ELAC 2


TASK 27-10-00-810-803-A
Failure of the Left or Right Pedal Position Transducer Unit for ELAC 2


1. Possible Causes
  • ELAC-2 [2CE2]
  • wiring from the ELAC-2 (2CE2) to the XDCR UNIT-PEDAL POS, L (25CE1)
  • wiring from the ELAC-2 (2CE2) to the XDCR UNIT-PEDAL POS, R (25CE2)
  • XDCR UNIT-PEDAL POS, L [25CE1]
  • XDCR UNIT-PEDAL POS, R [25CE2]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 27-24-00-710-001
Operational Test of the Rudder Hydraulic Actuation
AMM 27-92-15-000-001
Removal of the Pedal Position Transducer Unit
AMM 27-92-15-400-001
Installation of the Pedal Position Transducer Unit
ASM 279223
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 27-10-00-700-054-A
A. Test
   (1) Do the operational test of the rudder hydraulic actuation AMM 27-24-00-710-001.
   (2) Do the BITE test of the EFCS (Ground Scanning) AMM 27-96-00-740-001.
4. Fault Isolation
Subtask 27-10-00-810-052-A
A. If the BITE test gives the maintenance message L or R PEDALS XDCR UNIT:
   (1) Replace the ELAC-2 [2CE2] AMM 27-93-34-000-001 and AMM 27-93-34-400-001.
   (2) If the fault continues:
  • Do a check and repair the wiring from the ELAC-2 (2CE2) to the XDCR UNIT-PEDAL POS, L (25CE1) ASM 279223.
     (a) If the fault continues:
  • Do a check and repair the wiring from the ELAC-2 (2CE2) to the XDCR UNIT-PEDAL POS, R (25CE2) ASM 279223.
   (3) If the fault continues:
     (a) If the fault continues:
Subtask 27-10-00-700-097-A
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:27:26 UTC