W DOC AIRBUS | AMM A320F

Installation of the BMC


TASK 36-11-34-400-001-A
Installation of the BMC


ZONE: 121
ZONE: 122
FIN: 1HA1
FIN: 1HA2
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
121
AVIONICS COMPARTMENT
122
AVIONICS COMPARTMENT
811
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 36-11-00-610-801-A
Uploading of the Bleed Monitoring Computer (BMC) Data
TASK 36-11-00-740-001-A
BITE Test of the BMC 1(2)
TASK 36-11-00-740-802-A
BITE Test of the Engine Bleed Air System (EBAS) (System Test)
3. Job Set-up
Subtask 36-11-34-860-051-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the ground service network is energized (Ref. AMM TASK 24-42-00-861-001).
Subtask 36-11-34-010-051-A
B. Get Access
   (1) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position at the access door 811.
   (2) Make sure that the access door 811 is open.
Subtask 36-11-34-865-051-A
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 1HA1 (BMC1)
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
FOR FIN: 1HA2 (BMC2)
49VUAIR BLEED/ENG 2/MONG3HA2D12
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL2HA2Z22
4. Procedure
Subtask 36-11-34-420-050-A
A. Installation of the BMC
   (1) Clean the component interface and/or the adjacent area.
   (2) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (3) Make sure that all the electrical connections are clean and in the correct condition.
   (4) Install the BMC (1) on its rack (3).
   (5) Push the BMC (1) on its rack (3) to connect the electrical connectors (2).
   (6) Engage the nut (4) on the lug (5) and tighten.
Subtask 36-11-34-865-052-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 1HA1 (BMC1)
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
FOR FIN: 1HA2 (BMC2)
49VUAIR BLEED/ENG 2/MONG3HA2D12
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-11-34-970-050-B ** ON A/C NOT FOR ALL
C. Do a check of the configuration of the BMC that you installed and, if necessary, upload the applicable software (Ref. AMM TASK 36-11-00-610-801).
Subtask 36-11-34-710-050-A ** ON A/C NOT FOR ALL
D. Do the BITE test of the BMC 1 (BMC 2) (Ref. AMM TASK 36-11-00-740-001).
Subtask 36-11-34-710-050-B ** ON A/C NOT FOR ALL
D. Do the BITE test of the Engine Bleed Air System (EBAS) (System Test) (Ref. AMM TASK 36-11-00-740-802).
5. Close-up
Subtask 36-11-34-410-050-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access door 811.
   (3) Remove the access platform(s).
Subtask 36-11-34-862-050-A
B. De-energize the ground service network (Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.04.01 01:08:59 UTC