W DOC AIRBUS | TSM A320F

Loss of the 601PP and 602PP Busbars in Ground Service Configuration


TASK 24-43-00-810-801-A
Loss of the 601PP and 602PP Busbars in Ground Service Configuration


1. Possible Causes
  • wiring
  • C/B-SVCE/601PP/602PP/SPLY [1PX]
  • CNTOR-DC SVCE BUS GND SPLY [3PX]
  • C/B-ELEC/DC SVCE/BUS/ON TR2 [5PX]
  • CNTOR-AC & DC GND SVCE SPLY [14XX]
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 24-42-00-861-001
Energize the Ground Service Network from the External Power
AMM 24-42-00-862-001
De-energize the Ground Service Network Supplied from the External Power
AMM 24-42-55-000-001
Removal of the Contactors
AMM 24-42-55-400-001
Installation of the Contactors
ASM 244301
AMM 24-43-55-000-001
Removal of the DC Service Bus Ground Supply Contactor
3. Fault Confirmation
Subtask 24-43-00-860-050-A
A. Job Set-up
   (1) Energize the ground service network with the ground power unit AMM 24-42-00-861-001.
Subtask 24-43-00-710-050-A
B. Test
ACTION
RESULT
1.On the overhead panel 25VU, put the INT LT/DOME switch in the BRT position.
The CAPT dome lights do not come on.
4. Fault Isolation
Subtask 24-43-00-810-050-B ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
  • Do a check of the status of the circuit breaker (1PX).
   (1) If the circuit breaker is closed:
  • Do a check for 28VDC on the pin 6 of the module 14PN ASM 244301.
     (a) If there is no 28VDC:
  • Do a check of the wiring between the circuit breaker (1PX) and the pin 6 of the module 14PN ASM 244301.
       1 If there is no continuity:
  • Repair the wiring .
       2 If there is continuity:
  • Replace the C/B-SVCE/601PP/602PP/SPLY [1PX] .
     (b) If there is 28VDC:
       1 If the fault continues:
  • Do a check of the wiring between pin 7 of the module 14PN and the busbars 601PP and 602PP ASM 244301.
         a If there is no continuity:
  • Repair the wiring .
         b If there is continuity:
  • Do a check and repair the wiring :
    . from the pin 6 of the module 14PN to the circuit breaker (5PX)
    . from the circuit breaker (5PX) to the pin B/3 of the contactor (3PX)
    . from the pin B/5 of the contactor (3PX) to the terminal block ASM 244301.
         c If the fault continues:
  • Replace the C/B-ELEC/DC SVCE/BUS/ON TR2 [5PX] .
         d If the fault continues:
   (2) If the circuit breaker is open:
     (a) If the fault continues:
  • Replace the C/B-SVCE/601PP/602PP/SPLY [1PX] .
Subtask 24-43-00-810-050-C ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
  • Do a check of the status of the circuit breaker (1PX).
   (1) If the circuit breaker is closed:
  • Do a check for 28VDC on the pin E of the DC SVCE BUS ground supply contactor (3PX) ASM 244301.
     (a) If there is no 28VDC:
  • Do a check of the wiring between the circuit breaker (1PX) and the DC SVCE BUS ground supply contactor (3PX) ASM 244301.
       1 If there is no continuity:
  • Repair the wiring.
       2 If there is continuity:
  • Replace the C/B-SVCE/601PP/602PP/SPLY [1PX] .
     (b) If there is 28VDC:
       1 If the fault continues:
  • Do a check of the wiring between pin A/F of the DC SVCE BUS ground supply contactor (3PX) and the busbars 601PP and 602PP ASM 244301.
         a If there is no continuity:
  • Repair the wiring .
         b If there is continuity:
  • Do a check and repair the wiring :
    . from the pin A/E of the contactor (3PX) to the circuit breaker (5PX)
    . from the circuit breaker (5PX) to the pin B/3 of the contactor (3PX)
    . from the pin B/3 of the contactor (3PX) to the terminal block ASM 244301.
         c If the fault continues:
  • Replace the C/B-ELEC/DC SVCE/BUS/ON TR2 [5PX] .
         d If the fault continues:
   (2) If the circuit breaker is open:
     (a) If the fault continues:
  • Replace the C/B-SVCE/601PP/602PP/SPLY [1PX] .
Subtask 24-43-00-710-051-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 CAPT dome lights come on.
5. Close-up
Subtask 24-43-00-860-051-A
A. Put the aircraft back to its initial configuration.
   (1) On the overhead panel 25VU, put the INT LT/DOME switch in the OFF position.
   (2) De-energize the ground service network with the ground power unit AMM 24-42-00-862-001.
[Rev.8 from Aug 2018] 2026.04.04 04:26:55 UTC