W DOC AIRBUS | AMM A320F

Procedure for FDIMU Software loading with PDL for ADC/ FOMAX


TASK 31-36-00-710-806-A
Procedure for FDIMU Software loading with PDL for ADC/ FOMAX


NOTE: The CARD2 capacity must be no more than 2GB.
NOTE: It is not permitted to format CARD2 when the stored ACMS data is being retrieved.
NOTE: It is no permitted to change the content of CARD2. If any modification occurs, the CARD2 must be formatted according to the procedure described in this task.
NOTE: The full data-loading sequence must be done if a different card than CARD2 is inserted in the FDIMU.
NOTE: The CARD2 must be prepared according to the AGS allocation. The allocation defined in the ADC Configuration File B will be discarded.
NOTE: If you insert the unprepared CARD2 after data loading of software 10TVSW9, the CARD2 will be rejected by the FDIMU (PCMCIA led will be red).
NOTE: You can also load the FDIMU software with PCMCIA cards (Ref. AMM TASK 31-36-00-710-805).
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT)
No specific
1
LOADER - DATA, PORTABLE
No specific
3
PCMCIA-CARD
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
ALT45200001
1
PORTABLE DATA LOADER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
824
 C. 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 31-36-00-000-001-A
Removal of the Personal Computer Memory Card (PCMCIA) of the FDIMU/DMU
TASK 31-36-00-710-805-A
Procedure for FDIMU Software loading and preparation of PCMCIA cards for ADC/ FOMAX
TASK 31-36-00-740-012-A
Test of the Flight Data Interface and Management Unit (FDIMU)
TASK 31-36-00-740-013-A
Update of the APU Hours and Cycles in the FDIMU after APU, ECB or FDIMU Replacement
TASK 31-36-00-740-014-A
Update of the Engine Hours and Cycles in the Flight Data Interface and Management Unit (FDIMU)
TASK 31-36-00-740-015-A
Printout of the Engine/APU Hours and Cycles Stored in the Flight Data Interface and Management Unit (FDIMU)
TASK 52-41-00-010-002-A
Open the Avionics Compartment Doors for Access
TASK 52-41-00-410-002-A
Close the Avionics Compartment Doors after Access
TSM 31360003
3. Job Set-up
Subtask 31-36-00-861-092-A
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) Do a printout of the engine and APU hours and cycles (Ref. AMM TASK 31-36-00-740-015).
NOTE: The software load can erase the data of the engine and APU hours and cycles in the FDIMU. The printout gives a hard copy of this data. If necessary, refer to the printout to correct the engine and APU hours and cycles later.
All modifications done before through MCDU programming menu can be lost after the software loading. Reports counters are also set to their initial condition.
   (3) Make sure that the cards with the 10TVSW2, 10TVSW8 and 10TVSW9 software are in writeprotected status (writeprotection ON).
Subtask 31-36-00-010-102-A
B. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) in position at access door 824 in zone 128.
   (2) Open access door 824 (Ref. AMM TASK 52-41-00-010-002).
   (3) For the location of the components, refer to the paragraph component location TSM 31360003.
4. Procedure
Subtask 31-36-00-000-064-A
A. Aircraft Maintenance Configuration
   (1) Remove the PCMCIA that is inserted in the FDIMU (Ref. AMM TASK 31-36-00-000-001).
Subtask 31-36-00-865-195-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
121VUCFDS/CFDIU/SPLY2TWJ18
121VUCFDS/CFDIU/BACK/UP8TWJ17
121VUDLS&/DLRB/SPLY5TDJ15
121VUPDL/PWR/SPLY14TDK19
121VUAIDS & RCDR/QAR14TUK17
121VUAIDS & RCDR/FDIMU5TVK15
121VUENGINE/ENG1 AND 2/EVMU1EVR44
Subtask 31-36-00-480-061-A
C. Installation of the Portable Data Loader (PDL)
   (1) On the center pedestal 11VU:
     (a) On the DATA LOADING panel 117VU, loosen the two middle quick-release fasteners of the access cover and remove it.
     (b) Connect the ALT45200001 PORTABLE DATA LOADER or LOADER - DATA, PORTABLE to the DATA LOADING connector.
     (c) Start the PDL (Refer to the PDL user guide).
Subtask 31-36-00-710-172-A
D. System Software Load Procedure
NOTE: The standard system software package has two system media disks. System software updates in the future can have more than two disks in the package. All software disks has to be loaded until the loading procedure is completed.
NOTE: If the PDL has the digital signature check, the PDL can trigger two messages:
  • When the software has no signature (refer to the PDL user guide), this message has no effect on the A/C software upload and you can ignore it.
  • When the signature is incorrect or corrupted (refer to the PDL user guide), the software upload is not possible and it is necessary to use other software.
As a data security precaution, Airbus recommends that the user does a report of the fault to his Aircraft Security Focal Point.
ACTION
RESULT
On the overhead panel, on the Data Loading Selector (DLS):
On the DLS display:
  • Put the data loading selector ON/OFF switch to the ON position.
  • The DB/N:XXXXXXXX and PUSH NEXT/PREV indications show.
  • Push the NEXT or PREV key until the ACMS NOT SELECTED indication shows on the display.
  • The ACMS NOT SELECTED indication shows.
  • Push the SEL CTL key.
  • The ACMS SELECTED indication shows.



NOTE: The display shows AIDS or ACMS.
On the PDL:
  • Upload the FDIMU AIDS software (Refer to the PDL user guide).

On the DLS panel:
On the DLS display:
  • Push the SEL CTL key.
  • The ACMS NOT SELECTED indication shows.


NOTE: The display shows AIDS or ACMS.
  • Set the ON/OFF switch to OFF position.

Subtask 31-36-00-710-167-A
E. Set-Up Database Software Load Procedure
NOTE: The software part number is shown in the IPC.
NOTE: The upload of the database files can be monitored on the MCDU in the AIDS menu LOAD STATUS page.
   (1) Upload the FINs in this sequence:
  • 10TVSW2
  • 10TVSW8
  • 10TVSW9.
ACTION
RESULT
On the overhead panel, on the Data Loading Selector (DLS):
On the DLS display:
  • Put the data loading selector ON/OFF switch to the ON position.
  • The DB/N:XXXXXXXX and PUSH NEXT/PREV indications show.
  • Push the NEXT or PREV key until the ACMS NOT SELECTED indication shows on the display.
  • The ACMS NOT SELECTED indication shows.
  • Push the SEL CTL key.
  • The ACMS SELECTED indication shows.



NOTE: The display shows AIDS or ACMS.
On the PDL:
  • Upload the FDIMU database software (Refer to the PDL user guide).

On the DLS panel:
On the DLS display:
  • Push the SEL CTL key.
  • The ACMS NOT SELECTED indication shows.


NOTE: The display shows AIDS or ACMS.
  • Set the ON/OFF switch to OFF position.

Subtask 31-36-00-710-171-A
F. Check of the Part Number of the FDIMU Software
ACTION
RESULT
On the MCDU:
On the MCDU display:
  • Push the line key adjacent to the AIDS indication.
  • The AIDS page comes into view.
  • Push the line key adjacent to the REPROGRAMMING indication.
  • The AIDS:SPECIAL FUNC/REPROG page comes into view.
  • Push the line key adjacent to the DOC DATA indication.
  • The AIDS:DOCUMENTARY DATA page comes into view.
  • Make sure that the FDIMU software part-number and FDIMU hardware part-number are correct.

  • Push the line key adjacent to the RETURN indication.
  • The AIDS:SPECIAL FUNC/REPROG page comes into view.
  • Push the line key adjacent to the RETURN indication.
  • The AIDS page comes into view.
Subtask 31-36-00-860-163-A
G. Stop the PDL
   (1) Stop the ALT45200001 PORTABLE DATA LOADER or LOADER - DATA, PORTABLE (Refer to the PDL user guide).
   (2) Remove the PDL:
     (a) On center pedestal 11VU, on DATA LOADING panel 117VU:
       1 Disconnect the ALT45200001 PORTABLE DATA LOADER or LOADER - DATA, PORTABLE from the DATA LOADING connector.
       2 Install the access cover and tighten the two middle quick-release fasteners.
Subtask 31-36-00-865-196-A
H. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUCFDS/CFDIU/SPLY2TWJ18
121VUCFDS/CFDIU/BACK/UP8TWJ17
121VUDLS&/DLRB/SPLY5TDJ15
121VUPDL/PWR/SPLY14TDK19
121VUAIDS & RCDR/QAR14TUK17
121VUAIDS & RCDR/FDIMU5TVK15
121VUENGINE/ENG1 AND 2/EVMU1EVR44
Subtask 31-36-00-400-063-A
I. Install the Personal Computer Memory Card (PCMCIA)
CAUTION: MAKE SURE THAT THE PCMCIA CARD IS CORRECTLY ALIGNED BEFORE YOU INSTALL IT IN THE RELATED SLOT. ALSO DO NOT USE FORCE TO INSTALL IT. IF YOU DO NOT OBEY THESE INSTRUCTIONS, DAMAGE TO THE EQUIPMENT CAN OCCUR.
   (1) Open the door to get access to the PCMCIA-CARD.
NOTE: The PCMCIA must be inserted with the NOTCH on the bottom.
   (2) Insert the PCMCIA-CARD CARD2 carefully into the interface until the card has connected with the contacts.
   (3) Close the door.
Subtask 31-36-00-865-197-A
J. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUAIDS & RCDR/FDIMU5TVK15
Subtask 31-36-00-710-168-A
K. PCMCIA Card status
   (1) Do the Test of the Correct PCMCIA-Card Function.
ACTION
RESULT
On the MCDU:
On the MCDU display:
  • Push the Line Select Key (LSK) adjacent to the <AIDS indication.
  • The AIDS menu shows.
  • Push the LSK adjacent to the PCMCIA> indication.
  • The AIDS: PCMCIA MAIN MENU shows.
  • Push the LSK adjacent to the <QAR DATA indication.
  • The AIDS: PCMCIA QAR STATUS shows.
  • Push the LSK adjacent to the RETURN indication.
  • The AIDS: PCMCIA MAIN MENU shows.
  • Push the LSK adjacent to the <SAR DATA indication.
  • The AIDS: PCMCIA SAR STATUS shows.
  • Push the LSK adjacent to the RETURN indication.
  • The AIDS: PCMCIA MAIN MENU shows.
  • Push the LSK adjacent to the DAR DATA> indication.
  • The AIDS: PCMCIA DAR STATUS shows.
  • Push the LSK adjacent to the RETURN indication.
  • The AIDS: PCMCIA MAIN MENU shows.
  • Push the LSK adjacent to the REPORT DATA> indication.
  • The AIDS: PCMCIA RPT STATUS shows.
  • Push the MCDU Main Menu key.
  • The MCDU Main Menu shows.
   (2) Make sure that the green LED comes on.
   (3) Wait until green LED stops flashing and go off.
Subtask 31-36-00-865-198-A
L. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUAIDS & RCDR/FDIMU5TVK15
Subtask 31-36-00-000-063-A
M. Removal of the Personal Computer Memory Card (PCMCIA)
   (1) Open the door to get access to the PCMCIA-CARD.
   (2) Remove the PCMCIA-CARD CARD2.
   (3) Close the access door.
Subtask 31-36-00-710-169-A
N. Software load procedure
   (1) Do the points B, C, D, E, F and G for loading of software 10TVSW8.
   (2) Do the points B, C, D, E, F and G for loading of software 10TVSW9.
Subtask 31-36-00-400-065-A
O. Install the Personal Computer Memory Card (PCMCIA)
CAUTION: MAKE SURE THAT THE PCMCIA CARD IS CORRECTLY ALIGNED BEFORE YOU INSTALL IT IN THE RELATED SLOT. ALSO DO NOT USE FORCE TO INSTALL IT. IF YOU DO NOT OBEY THESE INSTRUCTIONS, DAMAGE TO THE EQUIPMENT CAN OCCUR.
   (1) Open the door to get access to the PCMCIA-CARD.
NOTE: The PCMCIA must be inserted with the NOTCH on the bottom.
   (2) Insert the PCMCIA-CARD CARD2 carefully into the interface until the card has connected with the contacts.
   (3) Close the door.
Subtask 31-36-00-710-170-A
P. Operational Test
   (1) Do the Test of the FDIMU (Ref. AMM TASK 31-36-00-740-012).
5. Close-up
Subtask 31-36-00-410-101-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close access door 824 (Ref. AMM TASK 52-41-00-410-002).
   (3) Remove the access platform(s).
   (4) If necessary, do an update of the engine and APU hours and cycles (Ref. AMM TASK 31-36-00-740-013) (Ref. AMM TASK 31-36-00-740-014).
NOTE: The update is necessary if the software load erases the data of the engine and APU hours and cycles in the FDIMU.
Subtask 31-36-00-862-095-A
B. Aircraft Maintenance Configuration
   (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 08:35:37 UTC