W DOC AIRBUS | TSM A320F

Failure of the 212XP and 216XP Busbars in Normal Flight Configuration


TASK 24-50-00-810-813-A
Failure of the 212XP and 216XP Busbars in Normal Flight Configuration


1. Possible Causes
  • wiring
  • C/B-BUS 2/212XP/SPLY [10XN]
  • CNTOR-AC SVCE BUS NORM SPLY [12XN]
  • RELAY-GND/FLT SELECT CTL [7XX]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 24-00-00-810-803-A
Circuit Breaker Tripped and/or C/B TRIPPED Warning
AMM 24-41-00-861-002
Energize the Aircraft Electrical Circuits from the External Power
AMM 24-41-00-862-002
De-energize the Aircraft Electrical Circuits Supplied from the External Power
ASM 244201
ASM 245103
AMM 24-51-55-000-001
Removal of the AC Service Bus Normal Supply Contactor
AMM 24-51-55-400-001
Installation of the AC Service Bus Normal Supply Contactor
3. Fault Confirmation
Subtask 24-50-00-860-072-A
A. Job Set-up
   (1) Aircraft Maintenance Configuration
     (a) Energize the aircraft electrical circuits AMM 24-41-00-861-002.
Subtask 24-50-00-710-074-A
B. Test
ACTION
RESULT
1.On the forward attendant panel 120RH, push the CABIN WDO and CABIN CLG pushbutton switches.
  • the ceiling forward and aft lights (L side) do not come on
  • the window forward and aft lights (R side) do not come on.
4. Fault Isolation
Subtask 24-50-00-810-062-A ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
  • Do a check of the status of the circuit breaker (10XN).
   (1) If the circuit breaker is closed:
  • Do a check for 115VAC on the pins A/D, A/E and A/F of the contactor (12XN) ASM 245103.
     (a) If there is no 115VAC:
  • Do a check of the wiring between the circuit breaker (10XN) and the contactor (12XN) ASM 245103.
       1 If there is no continuity:
  • Repair the wiring .
       2 If there is continuity:
  • Replace the C/B-BUS 2/212XP/SPLY [10XN] .
     (b) If there is 115VAC:
       1 If the fault continues:
  • Do a check of the wiring between pins A/N, A/P and A/R of the contactor (12XN) and the busbars 212XP and 216XP ASM 244201.
         a If there is no continuity:
  • Repair the wiring .
         b If there is continuity:
  • Replace the RELAY-GND/FLT SELECT CTL [7XX] .
         c If the fault continues:
  • Do a check and repair the wiring :
    . from the circuit breaker (3XX) to the pin B/3 of the contactor (12XN).
    . from the pin B/5 of the contactor (12XN) to the first terminal block ASM 245103.
   (2) If the circuit breaker is open:
     (a) If the fault continues:
  • Replace the C/B-BUS 2/212XP/SPLY [10XN] .
Subtask 24-50-00-810-062-B ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
  • Do a check of the status of the circuit breaker (10XN).
   (1) If the circuit breaker is closed:
  • Do a check for 115VAC on the pins 10, 11, 12 of the module 20XX ASM 245103.
     (a) If there is no 115VAC:
  • Do a check of the wiring between the circuit breaker (10XN) and the module 20XX ASM 245103.
       1 If there is no continuity:
  • Repair the wiring .
       2 If there is continuity:
  • Replace the C/B-BUS 2/212XP/SPLY [10XN] .
     (b) If there is 115VAC:
       1 If the fault continues:
  • Do the check of the wiring between pins A/N, A/P and A/R of the contactor (12XN) and the busbars 212XP and 216XP ASM 244201.
         a If there is no continuity:
  • Repair the wiring .
         b If there is continuity:
  • Replace the RELAY-GND/FLT SELECT CTL [7XX] .
         c If the fault continues:
  • Do a check and repair the wiring :
    . from the circuit breaker (3XX) to the pin B/3 of the contactor (12XN).
    . from the pin B/5 of the contactor (12XN) to the first terminal block ASM 245103.
   (2) If the circuit breaker is open:
     (a) If the fault continues:
  • Replace the C/B-BUS 2/212XP/SPLY [10XN] .
Subtask 24-50-00-710-075-A
B. Do this test to make sure that the system operates correctly.
   (1) Do the test given in Para. 3. and make sure that:
  • the ceiling forward and aft lights (L side) come on
  • the window forward and aft lights (R side) come on.
5. Close-up
Subtask 24-50-00-860-073-A
A. Put the aircraft back to its initial configuration.
   (1) On the forward attendant panel 120RH release the CABIN WDO and CABIN CLG pushbutton switches.
   (2) De-energize the aircraft electrical circuits AMM 24-41-00-862-002.
[Rev.8 from Aug 2018] 2026.04.04 04:26:56 UTC