W DOC AIRBUS | TSM A320F

Failure of the GCU 1


TASK 24-20-00-810-868-A
Failure of the GCU 1


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 24-21-51-000-040
Removal of the Integrated Drive Generator - IDG 1(2)
AMM 24-21-51-000-803
Removal of the Integrated Drive Generator - IDG 1(2)
AMM 24-21-51-400-040
Installation of the Integrated Drive Generator - IDG 1(2)
AMM 24-21-51-400-803
Installation of the Integrated Drive Generator - IDG 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 24-41-00-740-002
Operational Check of the GAPCU via the CFDS
3. Fault Confirmation
Subtask 24-20-00-740-050-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:
  • stop the trouble shooting.
4. Fault Isolation
Subtask 24-20-00-810-117-D ** 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 GCU1 (1XU1) comes into view associated with the fault code 121 (SRD FLD (+) FAIL keyword) or 188 (EX FLD (+) SENSE keyword):
     (a) If the fault continues:
   (2) If the maintenance message GCU1 (1XU1) comes into view associated with other fault codes:
Subtask 24-20-00-810-117-G ** 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 GCU1 (1XU1) comes into view associated with the fault code 121 (SRD FLD (+) FAIL keyword) or 188 (EX FLD (+) SENSE keyword):
     (a) If the fault continues:
   (2) If the maintenance message GCU1 (1XU1) comes into view associated with other fault codes:
Subtask 24-20-00-740-051-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:26:16 UTC