W DOC AIRBUS | TSM A320F

Failure of the ELEC/GEN 1 Pushbutton Switch


TASK 24-22-00-810-827-A
Failure of the ELEC/GEN 1 Pushbutton Switch


1. Possible Causes
  • wiring
  • P/BSW-ELEC/GEN 1 [3XU1]
  • GCU-1 [1XU1]
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 24-41-00-740-002
Operational Check of the GAPCU via the CFDS
3. Fault Confirmation
Subtask 24-22-00-740-071-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the GAPCU AMM 24-41-00-740-002.
4. Fault Isolation
Subtask 24-22-00-865-058-A ** ON A/C NOT FOR ALL
A. Table of the circuit breakers used in this procedure:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
122VUELEC/GCU/12XU1T26
Subtask 24-22-00-810-082-A ** ON A/C NOT FOR ALL
B. If the BITE test gives the maintenance message PB SW ELEC GEN1 (3XU1)/ GCU1 (1XU1):
NOTE: After you do the trouble shooting for this fault, open and close the ELEC/GCU1 circuit breaker (2XU1) to remove all 28VDC power supply from the GCU 1.
  • do a check of the wiring of the ELEC/GEN 1 pushbutton switch (3XU1) ASM 242202 for an open circuit or a short to ground between:
    . pin A/1C of the GCU 1 and pin A/D3 of the ELEC/GEN 1 pushbutton switch
    . pin A/4E of the GCU 1 and pin A/D2 of the ELEC/GEN 1 pushbutton switch
    . pin A/2G of the GCU 1 and pin A/D1 of the ELEC/GEN 1 pushbutton switch.
   (1) If the wiring is not correct:
  • repair or replace as necessary.
   (2) If the wiring is correct:
  • do a test of the contacts of the ELEC/GEN 1 pushbutton switch ASM 242202 for correct operation between:
    . pins A/D3 and A/D2 (normally closed)
    . pins A/D3 and A/D1 (normally open).
     (a) If the test is not OK:
  • replace the P/BSW-ELEC/GEN 1 [3XU1] on the ELEC panel 35VU.
     (b) If the test is OK:
Subtask 24-22-00-740-072-A ** ON A/C NOT FOR ALL
C. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:26:38 UTC