W DOC AIRBUS | TSM A320F

N2 not Below Idle Fault on EIU-2


TASK 73-25-00-810-B00-A
N2 not Below Idle Fault on EIU-2


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AWM 291205
AWM 344202
AMM 34-42-33-000-001
Removal of the Radio Altimeter Transceiver
AMM 34-42-33-400-001
Installation of the Radio Altimeter Transceiver
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 73-25-00-710-539-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 73-25-00-810-401-A ** ON A/C NOT FOR ALL
A. If there is confirmation of the fault:
   (1) On RELAY BOX (103VU):
     (a) Replace RELAY-N2 SPEED CONDTN [2709GJ] AWM 291205.
     (b) Do the test given in Para. 3.
   (2) If the fault continues:
     (a) Remove the XCVR (2SA2) AMM 34-42-33-000-001.
   (3) On RELAY BOX (103VU), remove the relay (2709GJ).
   (4) On MCDU, simulate the Discrete Output (DSO) 12:
     (a) Push the adjacent button to DSO 12 to have the status equal to 1 AMM 73-25-34-860-803.
     (b) At XCVR (2SA2) rack connector (AB), do a check for ground at contact 6K.
     (c) At relay (2709GJ) socket, do a check for ground at contact Z.
     (d) Stop the simulation of DSO 12 AMM 73-25-34-860-803.
   (5) If there is no ground, do a check of wiring for continuity (less than 5 ohms resistance) and short to ground:
     (a) If there is no ground at both contacts, do a check of wiring between EIU-2 (1KS2) rack contact 2F and (1862VT) on SHELF (86VU) AWM 732506.
     (b) If there is no ground at contact of XCVR (2SA2) rack, do a check of wiring between contact 6K of XCVR (2SA2) rack and (1862VT) AWM 344202.
     (c) If there is no ground at relay (2709GJ) socket, do a check of wiring between contact Z and (1862VT) AWM 291205.
     (d) If you find damage, repair or replace wiring AWM 732506.
     (e) If you find no damage:
       1 Replace EIU-2 [1KS2] AMM 73-25-34-000-802 and AMM 73-25-34-400-802.
       2 Do the test given in Para. 3.
   (6) If there is ground at all contacts:
     (a) Replace XCVR-RA, 2 [2SA2] AMM 34-42-33-000-001 and AMM 34-42-33-400-001.
     (b) Install the relay (2709GJ).
     (c) Do the test given in Para. 3.
5. Close-up
Subtask 73-25-00-860-163-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