FDIMU AIDS Software Load Procedure with the PDL

TASK 31-36-00-710-013-A
FDIMU AIDS Software Load Procedure with the PDL

ZONE: 120
ZONE: 210
FIN: 10TV ** ON A/C NOT FOR ALL

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	SAFETY CLIP - CIRCUIT BREAKER
2231560-1-B	1	PORTABLE DATA LOADER
2243942-1	1	Adapter Cable
YV68A110	1	PORTABLE DATA LOADER

B. Consumable Materials

REFERENCE	DESIGNATION
No specific	adapter cable

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
120	AVIONICS COMPARTMENT
210	CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD
824

D. 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 31-36-00-740-012-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

3. Job Set-up
Subtask 31-36-00-860-147-A ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the 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 stored in the FDIMU.
The printout gives a hard copy of this data. Use the printout as a reference to correct the engine and APU hours and cycles later, if necessary.
All modifications done before through the MCDU programming menu can be lost after the software loading. Reports counters will be also reinitialized.

(3) Make sure that the aircraft is in Ground configuration (Landing Gear compressed and all Engines stopped).

Subtask 31-36-00-010-067-A ** ON A/C NOT FOR ALL

B. Get Access
(1) Open access door 824, in order to get access to the avionics compartment (Ref. AMM TASK 52-41-00-010-002).

Subtask 31-36-00-865-092-A ** ON A/C NOT FOR ALL

C. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	AIDS & RCDR/FDIMU	5TV	K15

Subtask 31-36-00-860-082-C ** ON A/C NOT FOR ALL

D. Aircraft Maintenance Configuration
(1) On the front panel of the FDIMU, open the access door to get access to the OPERATIONAL/STORAGE switch.
(2) Make sure that the OPERATIONAL/STORAGE switch is in the 'ON' position.

NOTE: The switch activates the battery backup buffering of all internal AIDS data stored in the volatile memory in case of external power shut-down.

(3) On the YV68A110 PORTABLE DATA LOADER, make sure that the 'ON/OFF' switch is in 'OFF' position.
(4) Connect the adapter cable to the FDIMU front connector.
(5) Connect the adapter cable to the YV68A110 PORTABLE DATA LOADER interface.
(6) Make sure that the subsequent disks are in the write-protected status (write-protection ON): [10TV2] [10TV3]

NOTE: The number of disks can be different, related to the software version.

Subtask 31-36-00-860-082-F ** ON A/C NOT FOR ALL

NOTE: The switch activates the battery backup buffering of all internal AIDS data stored in the volatile memory in case of external power shut-down.

(3) On the YV68A110 PORTABLE DATA LOADER, make sure that the 'ON/OFF' switch is in 'OFF' position.
(4) Connect the adapter cable to the front connector of the FDIMU.
(5) Connect the adapter cable to the YV68A110 PORTABLE DATA LOADER interface.
(6) Make sure that the subsequent disk is in the write-protected status (write-protection ON): [10TV2]
(7) Make sure that the subsequent disk is in the write-protected status (write-protection ON): [10TV3]

NOTE: The number of disks can be different, related to the software version.

Subtask 31-36-00-860-082-H ** ON A/C NOT FOR ALL

D. Aircraft Maintenance Configuration
(1) On the front panel of the FDIMU, open the access door to get access to the front connector.
(2) On the 2231560-1-B PORTABLE DATA LOADER, make sure that the 'ON/OFF' switch is in 'OFF' position.
(3) Connect the 2243942-1 Adapter Cable to the front connector of the FDIMU.
(4) Connect the 2243942-1 Adapter Cable to the 2231560-1-B PORTABLE DATA LOADER interface.
(5) Make sure that the subsequent disk is in the write-protected status (write-protection ON): [10TV2]

NOTE: The number of disks can be different, related to the software version.

Subtask 31-36-00-865-151-A ** ON A/C NOT FOR ALL

E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	AIDS & RCDR/FDIMU	5TV	K15

Subtask 31-36-00-865-087-A ** ON A/C NOT FOR ALL

F. Make sure that this(these) circuit breaker(s) is(are) closed:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	AIDS & RCDR/FDIMU	5TV	K15
** ON A/C NOT FOR ALL
121VU	CFDS/CFDIU/SPLY	2TW	J18
121VU	CFDS/CFDIU/BACK/UP	8TW	J17
121VU	DATA/LOADER/SPLY	3TD	J16
121VU	ENGINE/ENG1 AND 2/EVMU	1EV	R44
** ON A/C NOT FOR ALL
121VU	DLS&/DLRB/SPLY	5TD	J15

4. Procedure
Subtask 31-36-00-710-078-C ** ON A/C NOT FOR ALL

A. System Software Load Procedure

ACTION	RESULT
On the Portable Data Loader (PDL) interface:	On the PDL display:
Put the 'ON/OFF' switch to the 'ON' position.	The Software Loading in Progress.
Put the [10TV2] into the PDL disk drive. NOTE: Each software version has a specified number of disks. It is necessary to load all disks until the loading process is completed.	The subsequent messages come into view: READY WAIT RESPONSE TRANSF IN PROG.
NOTE: Some PDLs show the BUS-number and the file-sizes between the messages TRANSF IN PROG and TRANSF COMPLETE. The file-sizes decrease to zero during the data loading. This shows the progress of the data loading.
Wait until the TRANSF COMPLETE indication comes into view.	TRANSF COMPLETE comes into view after the load procedure is completed correctly.
Push the EJECT button and remove the [10TV2] .
Put the 'ON/OFF' switch to the 'OFF' position.
On the MCDU front panel:	On the MCDU display:
Push the MCDU MENU mode key.	The MCDU menu comes into view.

Subtask 31-36-00-710-079-B ** ON A/C NOT FOR ALL

B. Set-Up Database Software Load Procedure

NOTE: You can monitor the upload of the database files on the MCDU, in the AIDS menu LOAD STATUS page.

ACTION	RESULT
On the PDL interface:	On the PDL display:
Put the 'ON/OFF' switch to the 'ON' position.	MDDU READY comes into view.
Put the [10TV3] into the PDL disk drive.	The subsequent messages come into view: READY WAIT RESPONSE TRANSF IN PROG.
NOTE: Some PDLs show the BUS-number and the file-sizes between the messages TRANSF IN PROG and TRANSF COMPLETE. The file-sizes decrease to zero during the data loading. This shows the progress of the data loading.
Wait until the TRANSF COMPLETE indication comes into view.	TRANSF COMPLETE comes into view after the load procedure is completed correctly.
Push the EJECT button and remove the [10TV3] .	MDDU READY comes into view.
Put the 'ON/OFF' switch to the 'OFF' position.	MDDU READY goes out of view.

Subtask 31-36-00-710-078-F ** ON A/C NOT FOR ALL

C. System Software Load Procedure

ACTION	RESULT
On the Portable Data Loader (PDL) interface:	On the PDL display:
Put the 'ON/OFF' switch to the 'ON' position.	The Software Loading in Progress.
Put the [10TVMD2] (which contains the [10TVSW2] into the PDL disk drive. NOTE: Each software version has a specified number of disks. It is necessary to load all disks until the loading process is completed.	The subsequent messages come into view: READY WAIT RESPONSE TRANSF IN PROG.
NOTE: Some PDLs show the BUS-number and the file sizes between the messages TRANSF IN PROG and TRANSF COMPLETE. The file sizes decrease to zero during the data loading. This shows the progress of the data loading.
Wait until the TRANSF COMPLETE indication comes into view.	TRANSF COMPLETE comes into view after the load procedure is completed correctly.
Push the EJECT button and remove the [10TVMD2] (which contains the [10TVSW2] .
Put the 'ON/OFF' switch to the 'OFF' position.
On the MCDU front panel:	On the MCDU display:
Push the MCDU MENU mode key.	The MCDU menu comes into view.

Subtask 31-36-00-710-079-D ** ON A/C NOT FOR ALL

D. Set-Up Database Software Load Procedure

NOTE: You can monitor the upload of the database files on the MCDU, in the AIDS menu LOAD STATUS page.

ACTION	RESULT
On the PDL interface:	On the PDL display:
Put the 'ON/OFF' switch to the 'ON' position.	MDDU READY comes into view.
Put the [10TVMD3] with the [10TVSW3] into the PDL disk drive.	The subsequent messages come into view: READY WAIT RESPONSE TRANSF IN PROG.
NOTE: Some PDLs show the BUS-number and the file-sizes between the messages TRANSF IN PROG and TRANSF COMPLETE. The file-sizes decrease to zero during the data loading. This shows the progress of the data loading.
Wait until the TRANSF COMPLETE indication comes into view.	TRANSF COMPLETE comes into view after the load procedure is completed correctly.
Push the EJECT button and remove the [10TVMD3] with the [10TVSW3] .	MDDU READY comes into view.
Put the 'ON/OFF' switch to the 'OFF' position.	MDDU READY goes out of view.

Subtask 31-36-00-970-050-A ** ON A/C NOT FOR ALL

E. Do a 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 PROGRAMMING indication.	The AIDS DMU PROGRAMMING 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 page comes into view.
Push the line key adjacent to the STOP indication.	The MCDU MENU page comes into view.

5. Close-up
Subtask 31-36-00-865-093-A ** ON A/C NOT FOR ALL

A. Open this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	AIDS & RCDR/FDIMU	5TV	K15

Subtask 31-36-00-860-092-A ** ON A/C NOT FOR ALL

B. Aircraft Maintenance Configuration
(1) Disconnect the adapter cable from the front connector of the FDIMU.
(2) Disconnect the adapter cable from the PDL interface.
(3) Close the access door on the front of the FDIMU.

Subtask 31-36-00-865-094-A ** ON A/C NOT FOR ALL

C. Close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	AIDS & RCDR/FDIMU	5TV	K15

Subtask 31-36-00-710-080-A ** ON A/C NOT FOR ALL

D. Test
(1) Do the test of the FDIMU (Ref. AMM TASK 31-36-00-740-012).

Subtask 31-36-00-410-066-A ** ON A/C NOT FOR ALL

E. 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) Make sure the access platform(s) is(are) removed.

Subtask 31-36-00-860-083-A ** ON A/C NOT FOR ALL

F. Aircraft Maintenance Configuration
(1) If necessary, do the update of the engine and APU hours and cycles (Ref. AMM TASK 31-36-00-740-013) and (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 stored in the FDIMU.

(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)

[Rev.10 from 2021] 2026.04.01 00:35:36 UTC