W DOC AIRBUS | TSM A320F

Failure of the ELEC/GALLEY Pushbutton Switch Circuit after GEN2 Load Shedding

TASK 24-22-00-810-816-A
Failure of the ELEC/GALLEY Pushbutton Switch Circuit after GEN2 Load Shedding

1. Possible Causes
  • P/BSW-ELEC/GALLEY [2XA]
  • GCU-2 [1XU2]
  • diode module 1162VD
  • EGIU-2 [22XU2]
  • wiring
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ESPM 2045110
AMM 24-22-33-000-001
Removal of the EGIU-1(2)
AMM 24-22-33-400-002
Installation of the EGIU-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 24-41-00-861-002
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
AIPC 25710104
AMM 31-60-00-860-001
EIS Start Procedure
AMM 71-00-00-710-003
Engine Automatic Start
AMM 71-00-00-710-028
Engine Shutdown
AMM 71-00-00-860-814
Shutdown of the Engine
AMM 71-00-00-860-823
Start the Engine (Normal Automatic Start)
3. Fault Confirmation
Subtask 24-22-00-860-068-A ** ON A/C NOT FOR ALL
A. Job Set-up
   (1) Push the ELEC/GEN 1 pushbutton switch (3XU1).
   (2) Aircraft Maintenance Configuration
     (a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
     (b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
   (3) Start the engine 2 AMM 71-00-00-710-003.
Subtask 24-22-00-860-068-C ** ON A/C NOT FOR ALL
A. Job Set-up
   (1) In the cockpit, on the ELEC panel 35VU:
  • Push the GEN 1 pushbutton switch (3XU1).
   (2) Aircraft Maintenance Configuration
     (a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
     (b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
   (3) Start engine 2 AMM 71-00-00-860-823.
Subtask 24-22-00-710-071-B
B. Test
ACTION
RESULT
1.On the ECAM control panel:
  • push the ELEC key to get the ELEC page.
On the upper ECAM DU:
  • the GEN 2 OVERLOAD message comes into view.
2.On the ELEC panel 35VU:
  • release the GALY & CAB pushbutton switch (2XA).
If on the upper ECAM DU:
  • the GEN 2 OVERLOAD message goes out of view, stop the trouble shooting.
    If on the upper ECAM DU:
  • the GEN 2 OVERLOAD message stays in view, continue the trouble shooting (refer to the fault isolation which follows).
4. Fault Isolation
Subtask 24-22-00-865-052-A
A. Table of the circuit breakers used in this procedure:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
122VUELEC/GALY & CAB/CTL1XAS26
122VUELEC/GALY & CAB/FAULT/LT CTL8XAS25
122VUELEC/GCU/12XU1T26
Subtask 24-22-00-810-065-A ** ON A/C NOT FOR ALL
B. If the test confirms the fault:
  • open the circuit breakers 8XA and 1XA
  • replace the P/BSW-ELEC/GALLEY [2XA] ESPM 2045110
  • close the circuit breakers 8XA and 1XA.
   (1) If the fault continues:
     (a) If the fault does not continue:
     (b) If the fault continues:
  • open the circuit breakers 8XA and 1XA
  • disconnect the connector of the diode module 1162VD AIPC 25710104
  • close the circuit breakers 8XA and 1XA.
       1 If the fault does not continue:
  • open the circuit breakers 8XA and 1XA
  • replace the diode module 1162VD AIPC 25710104
  • install the GCU2 (1XU2) AMM 24-22-34-400-001
  • close the circuit breakers 8XA and 1XA.
       2 If the fault continues:
         a If the fault does not continue:
  • open the circuit breakers 8XA and 1XA
  • connect the connector of the diode module 1162VD AIPC 25710104
  • install the GCU2 (1XU2) AMM 24-22-34-400-001
  • close the circuit breakers 8XA and 1XA.
         b If the fault continues:
  • open the circuit breakers 8XA and 1XA.
  • do a check and repair the wiring between:
    . the pin A/13 of the diode module 1162VD and the pin AA/13B of the GCU2 (1XU2)
    . the pin A/13 of the diode module 1162VD and the pin AA/6A of the EGIU2 (22XU2)
  • connect the connector of the diode module 1162VD AIPC 25710104
  • install the GCU2 (1XU2) AMM 24-22-34-400-001
  • close the circuit breakers 8XA and 1XA.
Subtask 24-22-00-810-065-B ** ON A/C NOT FOR ALL
B. If the test confirms the fault:
  • open the circuit breakers 8XA and 1XA
  • replace the P/BSW-ELEC/GALLEY [2XA]
  • close the circuit breakers 8XA and 1XA.
   (1) If the fault continues:
     (a) If the fault does not continue:
     (b) If the fault continues:
  • open the circuit breakers 8XA and 1XA
  • disconnect the connector of the diode module 1162VD AIPC 25710104
  • close the circuit breakers 8XA and 1XA.
       1 If the fault does not continue:
  • open the circuit breakers 8XA and 1XA
  • replace the diode module 1162VD AIPC 25710104
  • install the GCU 2 (1XU2) AMM 24-22-34-400-001
  • close the circuit breakers 8XA and 1XA.
       2 If the fault continues:
  • open the circuit breakers 8XA and 1XA.
  • do a check and repair the wiring between the pin A/13 of the diode module 1162VD and the pin AA/6G of the GCU 2 (1XU2)
  • connect the connector of the diode module 1162VD AIPC 25710104
  • install the GCU 2 (1XU2) AMM 24-22-34-400-001
  • close the circuit breakers 8XA and 1XA.
Subtask 24-22-00-710-072-A
C. Do the test given in Para. 3.
5. Close-up
Subtask 24-22-00-860-069-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Stop the engine 2 AMM 71-00-00-710-028.
   (2) Put the aircraft back to its initial configuration.
   (3) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
Subtask 24-22-00-860-069-C ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Stop engine 2 AMM 71-00-00-860-814.
   (2) Put the aircraft back to its initial configuration.
   (3) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
[Rev.8 from Aug 2018] 2026.04.04 04:26:36 UTC
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