W DOC AIRBUS | TSM A320F

Failure of the GCU 1


TASK 24-22-00-810-801-A
Failure of the GCU 1


1. Possible Causes
  • GCU-1 [1XU1]
  • sockets of the 400VC1
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
DYNAMOMETER 15 DAN (33 LBF) - PULL
 B. Referenced Information
REFERENCE
DESIGNATION
ESPM 2048230
AWM 242201
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 24-41-00-740-004
Operational Check of the GPCU via the CFDS
3. Fault Confirmation
Subtask 24-22-00-740-050-A ** ON A/C NOT FOR ALL
A. Test
Do the operational check of the GPCU with the CFDS AMM 24-41-00-740-004.
4. Fault Isolation
Subtask 24-22-00-810-050-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message GCU1:
  • do a check of the voltage of each phase.
   (1) If the voltage on each phase is correct:
   (2) If the voltage on one phase is not correct:
  • do a pin retention check ESPM 2048230 of the sockets of the 400VC1 AWM 242201. Use a DYNAMOMETER 15 DAN (33 LBF) - PULL, the CANNON value is 1.2 daN (2.7 lbf) minimum and the SOURIAU value is 2.8 daN (6.3 lbf) minimum, in relation to pin/socket type used.
[Rev.8 from Aug 2018] 2026.04.04 04:26:34 UTC