W DOC AIRBUS | TSM A320F

EIU-2 Relay Fault for PHMU Power Supply


TASK 73-25-00-810-A11-A
EIU-2 Relay Fault for PHMU Power Supply


1. Possible Causes
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
PLIERS - JAWED, SOFT
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Referenced Information
REFERENCE
DESIGNATION
AMM 71-13-00-010-802
Opening of the Fan Cowl Doors
AMM 71-13-00-410-802
Closing of the Fan Cowl Doors
AMM 73-21-62-000-802
Removal of the EEC Wiring Harness (WF02)
AMM 73-21-62-400-802
Installation of the EEC Wiring Harness (WF02)
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 732556
3. Fault Confirmation
Subtask 73-25-00-710-446-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 73-25-00-810-273-A ** ON A/C NOT FOR ALL
A. Check for EIU-2 fault
   (1) Replace EIU-2 [1KS2] AMM 73-25-34-000-802 and AMM 73-25-34-400-802.
     (a) Do the test given in Para. 3.
   (2) If the fault continues:
     (a) Go to the Para. 4.B.
Subtask 73-25-00-865-065-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)
121VUPHMU/ENG295KS2P45
Subtask 73-25-00-810-274-A ** ON A/C NOT FOR ALL
C. Check for harness fault
   (1) Open the fan cowl doors AMM 71-13-00-010-802.
   (2) Use a PLIERS - JAWED, SOFT to disconnect connector (402VC2-A).
     (a) Inspect for pins alignment.
     (b) Repair as necessary.
       1 Do the test given in Para. 3.
   (3) If alignment is correct or fault continues, check for 28 VDC to pins 26 of connector (402VC2) AWM 732556.
     (a) If there is 28 VDC at pin, repair aircraft wiring between connector (402VC2) and EIU-2 AWM 732556.
     (b) If there is no 28 VDC at pin, use a PLIERS - JAWED, SOFT to disconnect connector P9 at PHMU (4609KS).
       1 Inspect for pins alignment.
       2 Repair as necessary.
         a Do the test given in Para. 3.
     (c) If alignment is correct or fault continues:
       1 Replace HARNESS-FAN, WF02 [4218KS] AMM 73-21-62-000-802 and AMM 73-21-62-400-802.
         a Do the test given in Para. 3.
5. Close-up
Subtask 73-25-00-860-069-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the fan cowl doors AMM 71-13-00-410-802.
[Rev.8 from Aug 2018] 2026.04.04 04:36:26 UTC