W DOC AIRBUS | TSM A320F

DCV A and B Supplies Fault on EIU-2


TASK 73-25-00-810-A19-A
DCV A and B Supplies Fault on EIU-2


1. Possible Causes
  • EIU-2 [1KS2]
  • aircraft wiring
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Referenced Information
REFERENCE
DESIGNATION
AMM 73-25-34-000-802
Removal of the Engine Interface Unit (EIU)
AMM 73-25-34-400-802
Installation of the Engine Interface Unit (EIU)
AMM 73-25-34-710-802
Operational Test of the Engine Interface Unit (EIU) with the Centralized Fault Display System (CFDS)
AWM 783607
3. Fault Confirmation
Subtask 73-25-00-710-456-A ** ON A/C NOT FOR ALL
A. Do the operational test of the Engine Interface Unit (EIU) with the Centralized Fault Display System (CFDS) to confirm this fault AMM 73-25-34-710-802.
4. Fault Isolation
Subtask 73-25-00-810-285-A ** ON A/C NOT FOR ALL
A. If there is confirmation of the fault:
   (1) Check on report for any failure of normal BUS bar (202PP) and (204PP).
     (a) Troubleshoot as necessary (Ref. TSM Chap. 24).
     (b) Do the test given in Para. 3.
     (c) If no fault regarding the busbar is reported or if fault continues, go to the Para. 4.C.
Subtask 73-25-00-865-072-A ** ON A/C NOT FOR ALL
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
121VUDCV B/ENG2 PWR SPLY103KS2K45
121VUDCV A/ENG2 PWR SUPPLY102KS2K43
Subtask 73-25-00-810-286-A ** ON A/C NOT FOR ALL
C. If no fault regarding the BUS bar is reported or if fault continues:
   (1) Remove EIU-2 [1KS2] AMM 73-25-34-000-802.
   (2) Close both circuit breakers. Refer to the Para. 4.D.
   (3) Check for 28 VDC at pins 15A and 15C of connector AB on 85VU.
   (4) Open both circuit breakers. Refer tothe Para. 4.B.
   (5) If any damage found:
     (a) Repair or replace aircraft wiring AWM 783607.
   (6) If no problem is found or if fault continues:
     (a) Replace EIU-2 [1KS2] AMM 73-25-34-400-802.
     (b) Make sure that the both circuit breakers are closed. Refer to the Para. 4.D.
     (c) Do the test given in Para. 3.
Subtask 73-25-00-865-073-A ** ON A/C NOT FOR ALL
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
121VUDCV B/ENG2 PWR SPLY103KS2K45
121VUDCV A/ENG2 PWR SUPPLY102KS2K43
[Rev.8 from Aug 2018] 2026.04.04 04:36:27 UTC