W DOC AIRBUS | TSM A320F

Start Valve Closure Fault on EIU-2


TASK 73-25-00-810-A96-A
Start Valve Closure Fault on EIU-2


1. Possible Causes
  • wiring
  • EIU-2 [1KS2]
  • CONT-AIR COND SYSTEM 1 [47HH]
  • CONT-AIR COND SYSTEM 2 [57HH]
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 215103
AMM 21-61-34-000-002
Removal of the Air-Conditioning System Controller
AMM 21-61-34-400-002
Installation of the Air-Conditioning System Controller
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 73-25-00-710-535-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 73-25-00-810-397-A ** ON A/C NOT FOR ALL
A. If there is confirmation of the fault:
   (1) Remove both air-conditioning system controllers (47HH and 57HH) AMM 21-61-34-000-002.
   (2) On the MCDU, simulate the Discrete Output (DSO) 10:
     (a) Push the adjacent button to DSO 10 to have the status equal to 1 AMM 73-25-34-860-803.
     (b) Use a MULTIMETER - STANDARD to at both controllers rack connectors (AB), do a check for ground at contact 2A AWM 215103.
       1 Stop the simulation of DSO 10 AMM 73-25-34-860-803.
   (3) If there is no ground, do a check of wiring for continuity (less than 5 ohms resistance) and short to ground AWM 215103:
     (a) If there is no ground at both contacts 2A, do a check of wiring between EIU-2 (1KS2) rack contact 2F and (209VT) on SHELF 95VU.
     (b) If there is no ground at contact 2A of controller (47HH) rack, do a check of wiring between contact 2A of controller (47HH) rack and (209VT).
     (c) If there is no ground at contact 2A of controller (57HH) rack, do a check of wiring between contact 2A and (209VT).
     (d) If you find damage, repair or replace wiring AWM 215103.
     (e) If you find no damage:
       1 Replace EIU-2 [1KS2] AMM 73-25-34-000-802 and AMM 73-25-34-400-802.
   (4) If there is ground at contacts 2A:
     (a) Replace CONT-AIR COND SYSTEM 1 [47HH] AMM 21-61-34-400-002.
NOTE: Replacement of the controller (47HH) firstly then controller (57HH) secondly can be reversed.
       1 Install the controller (57HH) AMM 21-61-34-400-002.
       2 Do the test given in Para. 3.
   (5) If the fault continues:
     (a) Replace CONT-AIR COND SYSTEM 2 [57HH] AMM 21-61-34-000-002 AMM 21-61-34-400-002.
     (b) Do the test given in Para. 3.
5. Close-up
Subtask 73-25-00-860-149-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