W DOC AIRBUS | AMM A320F

Uploading of the Bleed Monitoring Computer (BMC) Data


TASK 36-11-00-610-802-A
Uploading of the Bleed Monitoring Computer (BMC) Data


1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 31-38-00-610-804-A
Onboard Software Uploading Procedure
TASK 36-11-00-740-804-A
BITE Test of the Engine Bleed Air System (EBAS) (System Test)
3. Job Set-up
Subtask 36-11-00-861-159-A
A. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 36-11-00-941-153-A
B. Safety Precautions
   (1) On ENG panel 115VU:
     (a) Make sure that engine 1(2) is(are) shutdown.
     (b) Make sure that the ENG MODE switch is in the NORM position.
Subtask 36-11-00-865-153-A
C. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUL/G/LGCIU/SYS1/NORM1GAC09
49VUAIR BLEED/ENG 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
49VUAUTO FLT/MCDU/111CA1H07
121VUAUTO FLT/MCDU/211CA2N20
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-11-00-860-134-A
D. Make sure that the aircraft is in the GROUND configuration:
ACTION
RESULT
1.On the ECAM control panel:
  • Press the pushbutton to call the BLEED page.
ON the SD:
  • The BLEED page is shown.
2.Make sure that the GND indication is displayed.
  • GND is displayed in white in the middle area of the page.
Subtask 36-11-00-740-057-A
E. Check the P/N update
   (1) Do the LRU identification check
     (a) Get access to LRU ident page:
       1 Select on MCDU the sequence that follow:
  • MCDU MENU->CFDS->SYSTEM REPORT/TEST->PAGE 2/2->AIR BLEED->BMC1(2)->LRU IDENT.
   (2) Make sure that the installed BMC software P/N shown on the LRU IDENTIFICATION page is not the same as the BMC software P/N written on the front face of the new storage device to load.
4. Procedure
Subtask 36-11-00-970-051-A
A. Uploading Procedure
NOTE: The two BMCs are uploaded at the same time, BMC1 is directly uploaded through DLRB and BMC2 is uploaded through X-TALK from BMC1.
   (1) Upload the BMC software (Ref. AMM TASK 31-38-00-610-804).
Subtask 36-11-00-280-052-A
B. Check the P/N updated
   (1) Do the LRU identification check
     (a) Get access to LRU ident page:
       1 Select on MCDU the sequence that follow:
  • MCDU MENU->CFDS->SYSTEM REPORT/TEST->PAGE 2/2->AIR BLEED->BMC1(2)->LRU IDENT.
   (2) Make sure that the installed BMC software P/N shown on the LRU IDENTIFICATION page is the same as the BMC software P/N written on the front face of the new storage device just loaded.
Subtask 36-11-00-740-063-A
C. BITE Test of the EBAS
   (1) Do the BITE test of the EBAS (Ref. AMM TASK 36-11-00-740-804).
5. Close-up
Subtask 36-11-00-860-136-A
A. Put the aircraft back to its initial configuration.
   (1) On the MCDU, push the MCDU MENU key to get the MCDU MENU page.
   (2) Put the storage device back into the cockpit storage-box.
Subtask 36-11-00-862-142-A
B. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 01:06:17 UTC