W DOC AIRBUS | TSM A320F

Failure of the TDC AC1 Sensor


TASK 24-22-00-810-809-A
Failure of the TDC AC1 Sensor


1. Possible Causes
  • SENSOR-TDC AC, 1
  • wiring
  • ENG1 LO OIL PRESS RELAY (7XT)
  • GCU-1 [1XU1]
  • GPCU [1XG]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 242202
AMM 24-22-18-000-001
Removal of the TDC AC Sensor 1(2)
AMM 24-22-18-400-001
Installation of the TDC AC Sensor 1(2)
AMM 24-22-34-000-001
Removal of the GCU-1(2)
AMM 24-22-34-400-001
Installation of the GCU-1(2)
AMM 24-41-00-740-004
Operational Check of the GPCU via the CFDS
ASM 244102
AMM 24-41-34-000-001
Removal of the Ground Power Control Unit (GPCU)
AMM 24-41-34-400-001
Installation of the Ground Power Control Unit (GPCU)
3. Fault Confirmation
Subtask 24-22-00-740-051-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the operational check of the GPCU with the CFDS AMM 24-41-00-740-004.
4. Fault Isolation
Subtask 24-22-00-810-058-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message TDC AC SENSOR 50XU1:
   (1) If the fault continues:
  • do a check of the wiring :
    . from the pin AB/12A of the GPCU (1XG) to the pin A/A1 of the ENG1 LO OIL PRESS RELAY (7XT)
    . from the pin A/A2 of the ENG1 LO OIL PRESS RELAY (7XT)to the pin A/B1 of the TDC AC1 SENSOR (50XU1)
    . from the pin A/B3 of the TDC AC1 sensor to the pin AB/10A of the GPCU
    . from the pin A/B3 of the TDC AC1 sensor to the pin AA/3A of the GCU1 (1XU1) ASM 242202.
     (a) If there is no continuity:
  • repair the wiring.
     (b) If there is continuity:
  • replace the ENG1 LO OIL PRESS RELAY (7XT).
     (c) If the fault continues:
  • do a check of the wiring
    . from the pins AA/13C, AA/14C and AA/11D of the GPCU to the pins AB/14C, AB/14D and AB/15C of the GCU1 ASM 244102.
       1 If there is no continuity:
  • repair the wiring.
       2 If there is continuity:
         a If the fault continues:
Subtask 24-22-00-740-052-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:26:35 UTC