W DOC AIRBUS | TSM A320F

Oil low Press and Ground 2 Fault on EIU-2


TASK 73-25-00-810-A94-A
Oil low Press and Ground 2 Fault on EIU-2


1. Possible Causes
  • RELAY-OIL LOW PRESS AND GROUND, ENG 2 [10KS2]
  • RELAY-OIL LOW PRESS AND GROUND, ENG 2 [12KS2]
  • wiring
  • EIU-2 [1KS2]
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
MULTIMETER - STANDARD
 B. Referenced Information
REFERENCE
DESIGNATION
AWM 732506
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)
AMM 73-25-34-860-803
Engine Interface Unit (EIU) DISCRETE OUTPUTS Simulation
3. Fault Confirmation
Subtask 73-25-00-710-533-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 73-25-00-810-395-A ** ON A/C NOT FOR ALL
A. If there is confirmation of the fault:
   (1) On RELAY BOX 103VU:
     (a) Replace RELAY-OIL LOW PRESS AND GROUND, ENG 2 [10KS2] and RELAY-OIL LOW PRESS AND GROUND, ENG 2 [12KS2] AWM 732506.
     (b) Do the test given in Para. 3.
   (2) If the fault continues, remove both relays (10KS2) and (12KS2).
   (3) On the MCDU, simulate Discrete Output (DSO) 6:
     (a) Push the adjacent button to DSO 6 to have the status equal to 1 AMM 73-25-34-860-803.
     (b) Use a MULTIMETER - STANDARD to at both relays (10KS2) and (12KS2) sockets, do a check for 28 VDC at contacts X:
       1 Stop simulation of DSO 9 AMM 73-25-34-860-803.
   (4) If there is no 28 VDC, do a check of wiring for continuity (less than 5 ohms resistance) and short to ground AWM 732506.
     (a) If there is no 28 VDC at both contacts, do a check of wiring between EIU-2 (1KS2) rack contact 10B and (1154VT).
     (b) If there is no 28 VDC at contact X of (12KS2), do a check of wiring between (12KS2) socket and (1154VT).
     (c) If there is no 28 VDC at contact X of (10KS2), do a check of wiring between (10KS2) socket and (1154VT).
   (5) If you find damage, repair or replace wiring AWM 732506.
   (6) If you find no damage:
     (a) Replace EIU-2 [1KS2] AMM 73-25-34-000-802 and AMM 73-25-34-400-802.
   (7) Install both relays (10KS2) and (12KS2).
     (a) Do the test given in Para. 3.
5. Close-up
Subtask 73-25-00-860-129-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.
[Rev.8 from Aug 2018] 2026.04.04 04:36:48 UTC