W DOC AIRBUS | TSM A320F

BMC-1 and BMC-2 buses fault on EIU-2


TASK 73-25-00-810-C67-A
BMC-1 and BMC-2 buses fault on EIU-2


1. Possible Causes
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 361111
AWM 361112
AMM 36-11-34-000-001
Removal of the BMC
AMM 36-11-34-400-001
Installation of the BMC
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 732557
AWM 732558
3. Fault Confirmation
Subtask 73-25-00-710-716-A ** ON A/C NOT FOR ALL
A. Do the operational test of the Engine Interface Unit (EIU) (1KS2) with the Centralized Fault Display System (CFDS) to confirm this fault. Refer to AMM 73-25-34-710-802.
4. Fault Isolation
Subtask 73-25-00-810-668-A ** ON A/C NOT FOR ALL
A. Do as follows:
   (1) Do the operational test of the EIU-1 (1KS1) with the CFDS to confirm this fault. Refer to AMM 73-25-34-710-802.
   (2) If the fault is confirmed on EIU-1 (1KS1) and EIU-2 (1KS2):
     (a) Replace BMC-1 [1HA1] and BMC-2 [1HA2] AMM 36-11-34-000-001 and AMM 36-11-34-400-001.
     (b) Do the test given in Para. 3.
     (c) If the fault continues:
       1 Remove BMC-1 [1HA1] and BMC-2 [1HA2] AMM 36-11-34-000-001.
       2 Use a MULTIMETER - STANDARD to do test of the circuits AWM 732557, AWM 361111 and AWM 361112. Refer to Table 1 and Table 2. Look for:
       3 Wire-to-wire shorts
       4 Shorts to ground
       5 Continuity (less than 5 ohms resistance).
NOTE: A short to ground is found when the resistance is less than 100 000 (100K) ohms.

Table 1: BMC-1 Circuit Connector Contacts
BMC-1 (1HA1) Connector AA Contacts
1862VT (86VU) Contacts
13B
S
15B
G

Table 2: BMC-2 Circuit Connector Contacts
BMC-2 (1HA2) Connector AA Contacts
1862VT (86VU) Contacts
13B
Y
15B
S
   (3) If a problem is found repair or replace wiring .
     (a) Install BMC-1 [1HA1] and BMC-2 [1HA2] AMM 36-11-34-400-001.
     (b) Do the test given in Para. 3.
   (4) If no problem is found or if the fault continues:
     (a) Remove EIU-2 [1KS2] AMM 73-25-34-000-802.
     (b) Use a MULTIMETER - STANDARD to do test of the circuits AWM 732557 and AWM 732558. Refer to Table 3. Look for:
       1 Wire-to-wire shorts
       2 Shorts to ground
       3 Continuity (less than 5 ohms resistance).
NOTE: A short to ground is found when the resistance is less than 100 000 (100K) ohms.

Table 3: EIU-2 Circuit Connector Contacts
EIU-2 (1KS2) Connector AA Contacts
1862VT (86VU) Contacts
14C
R
15C
Y
10F
P
11E
T
   (5) If a problem is found repair or replace wiring .
   (6) If no problem is found or if the fault continues:
     (a) Replace EIU-2 [1KS2] AMM 73-25-34-400-802.
     (b) Do the test given in Para. 3.
5. Close-up
Subtask 73-25-00-860-313-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 04:36:56 UTC