W DOC AIRBUS | TSM A320F

Failure of the RS422 Electrical Connection between the GPCU and the GCU 1


TASK 24-41-00-810-804-A
Failure of the RS422 Electrical Connection between the GPCU and the GCU 1


1. Possible Causes
  • wiring between the circuit breaker (2XU1) and the GCU 1
  • C/B-ELEC/GCU/1 [2XU1]
  • wiring of the RS422 bus
  • GCU-1 [1XU1]
  • GPCU [1XG]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 242202
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 24-41-00-710-055-A ** ON A/C NOT FOR ALL
A. Test
Do the operational check of the GPCU with the CFDS AMM 24-41-00-740-004.
4. Fault Isolation
Subtask 24-41-00-810-053-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message NO DATA FROM GCU 1:
  • on the circuit breaker panel 122VU, do a check of the status of the circuit breaker (2XU1).
   (1) If the circuit breaker is open:
  • close it.
   (2) If the circuit breaker is closed:
  • do a check for 28VDC on the pin A/1D of the GCU 1.
     (a) If there is no 28VDC:
  • do a check of the wiring between the circuit breaker (2XU1) and the GCU 1 ASM 242202.
       1 If there is no continuity:
  • repair the wiring.
       2 If there is continuity:
  • replace the C/B-ELEC/GCU/1 [2XU1] .
     (b) If there is 28VDC:
  • do a check of the wiring of the RS422 bus between respectively the GCU 1 pins B/14C, B/14D and the GPCU pins A/13C, A/14C ASM 244102.
       1 If there is no continuity:
  • repair the above wiring.
       2 If there is continuity:
       3 If the fault continues:
Subtask 24-41-00-710-056-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:26:53 UTC