W DOC AIRBUS | TSM A320F

Failure of the GLC 2 or Loss of its Status Indication


TASK 24-22-00-810-824-A
Failure of the GLC 2 or Loss of its Status Indication


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 242203
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 24-22-55-000-001
Removal of the Contactors
AMM 24-22-55-400-002
Installation of the Contactors
AMM 24-41-00-740-002
Operational Check of the GAPCU via the CFDS
3. Fault Confirmation
Subtask 24-22-00-740-057-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the GAPCU AMM 24-41-00-740-002.
     (a) If the BITE test gives the message TEST FAILED:
  • do the trouble shooting given in Para 4.A.
     (b) If the BITE test gives the message TEST PASSED:
  • do the trouble shooting given in Para 4.B.
4. Fault Isolation
Subtask 24-22-00-810-087-A ** ON A/C NOT FOR ALL
A. If the BITE test gives the message TEST FAILED:
  • push the line key adjacent to the TEST FAILED message.
   (1) If the maintenance message GCU2 (1XU2) comes into view:
Subtask 24-22-00-810-075-A ** ON A/C NOT FOR ALL
B. If the BITE test gives the message TEST PASSED:
  • do a check of the wiring ASM 242203 for an open circuit between:
    . pin 2 of the ELEC/GCU2 circuit breaker (2XU2) and pin B/18 of the GLC 2 (9XU1)
    . pin B/20 of the GLC 2 and pin A/30 of the diode module 2420VD
    . pin A/15 of the diode module 2420VD and pin A/6A of the GCU 2.
  • do a check of the contact of the GLC 2 (9XU2) for correct operation between pins B/18 and B/20 ASM 242203.
   (1) If the wiring or the contact are not correct:
   (2) If the wiring or the contact are correct:
Subtask 24-22-00-740-058-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