W DOC AIRBUS | TSM A320F

Failure of the Pedal Force Transducer Unit


TASK 27-92-00-810-836-A
Failure of the Pedal Force Transducer Unit


1. Possible Causes
  • FTU-RUDDER PEDAL [74CE]
  • C/B-RUDDER FTU [75CE]
  • wiring of the +28VDC signal from the pedal force transducer unit to the circuit breaker
  • wiring of the GND signal from the pedal force transducer unit to the ground
  • ground wiring of the pedal force transducer unit
  • wiring of the DGI 10 signal from the pedal force transducer unit to the first terminal block
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 31-32-00-810-934-A
Failure of the Digital Links
ASM 279207
AIPC 27920801
AMM 27-92-27-000-001
Removal of the Rudder Pedal Force Transducer
AMM 27-92-27-400-001
Installation of the Rudder Pedal Force Transducer
AMM 27-96-00-740-001
BITE Test of the EFCS (Ground Scanning)
3. Fault Confirmation
Subtask 27-92-00-740-118-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
4. Fault Isolation
Subtask 27-92-00-810-092-A ** ON A/C NOT FOR ALL
A. If the test confirm the fault:
   (1) If the fault continues:
   (2) If the fault continues:
   (3) If the fault continues:
  • do a check of the wiring of the +28VDC signal from the pedal force transducer unit to the circuit breaker ASM 279207.
  • do a check of the wiring of the GND signal from the pedal force transducer unit to the ground ASM 279207.
  • do a check of the ground wiring of the pedal force transducer unit ASM 279207.
  • do a check and repair the wiring of the DGI 10 signal from the pedal force transducer unit to the first terminal block ASM 279207.
Subtask 27-92-00-740-119-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:27:55 UTC