Uploading of the Flight Guidance (FG) Data

TASK 22-83-00-610-802-A
Uploading of the Flight Guidance (FG) Data

ZONE: 210
FIN: 1CA1 ** ON A/C NOT FOR ALL
FIN: 1CA2 ** 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
ALT45200001	4	PORTABLE DATA LOADER

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
210	CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD

C. Referenced Information

REFERENCE	DESIGNATION
TASK 22-96-00-710-001-A	Operational Test of the AFS
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 29-10-00-864-003-A	Depressurize the Blue Hydraulic System
TASK 29-23-00-864-001-A	Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU
TASK 29-24-00-864-001-A	Depressurize the Yellow Hydraulic System
TASK 31-32-00-860-001-A	Procedure to Get Access to the SYSTEM REPORT/TEST Menu Page
TASK 31-38-00-610-804-A	Onboard Software Uploading Procedure

3. Job Set-up
Subtask 22-83-00-861-050-A ** ON A/C NOT FOR ALL

A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).

Subtask 22-83-00-610-050-A ** ON A/C NOT FOR ALL

B. Prepare the media.
(1) Get the media from the storage box in the cockpit.
(2) Make sure that the Part Number(s) (P/N) written on the media is(are) the same as the P/N(s) written in the airline configuration-management document.
(3) If the media is(are) not available or not the correct one(s), contact your airline engineering department to get the correct P/N(s) applicable to the aircraft.

Subtask 22-83-00-610-050-C ** ON A/C NOT FOR ALL

B. Prepare the software.
(1) Make sure that the Part Number(s) (P/N) of the software is the same as the P/N(s) written in the airline configuration-management document.
(2) If the software is not available or not the correct one(s), contact your airline engineering department to get the correct P/N(s) applicable to the aircraft.

Subtask 22-83-00-480-050-B ** ON A/C NOT FOR ALL

C. Installation of the Portable Data Loader (PDL)
(1) On the ALT45200001 PORTABLE DATA LOADER, make sure that the ON/OFF switch is in the OFF position.
(2) On the center pedestal, on DATA LOADING panel 117VU:

Connect the cable to the ALT45200001 PORTABLE DATA LOADER and to the data loader connector on the front face of the Data Loading Selector Unit (DLSU) (103TD).

Subtask 22-83-00-865-051-A ** ON A/C NOT FOR ALL

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

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	AUTO FLT/FMGC/1	10CA1	B02
49VU	AUTO FLT/MCDU/1	11CA1	B01
** ON A/C NOT FOR ALL
49VU	L/G/LGCIU/SYS1/NORM	1GA	C09
** ON A/C NOT FOR ALL
49VU	AUTO FLT/FMGC/1	10CA1	H08
49VU	AUTO FLT/MCDU/1	11CA1	H07
** ON A/C NOT FOR ALL
121VU	DLS&/DLRB/SPLY	5TD	J15
** ON A/C NOT FOR ALL
121VU	PDL/PWR/SPLY	14TD	K19
** ON A/C NOT FOR ALL
121VU	AUTO FLT/FMGC/2	10CA2	M17
121VU	AUTO FLT/MCDU/2	11CA2	N20
** ON A/C NOT FOR ALL
121VU	DLSU &/DLRB/SPLY	5TD	J15
** ON A/C NOT FOR ALL
121VU	PDL/PWR/SPLY	14TD	J45
121VU	DLSU &/DLRB/SPLY	5TD	J38

Subtask 22-83-00-860-057-B ** ON A/C NOT FOR ALL

E. Start the PDL.
(1) Start the ALT45200001 PORTABLE DATA LOADER (refer to the PDL user guide).

Subtask 22-83-00-860-056-A ** ON A/C NOT FOR ALL

F. Aircraft Maintenance Configuration
(1) Make sure that the aircraft is in the ground configuration:

ACTION	RESULT
1.On the ECAM control panel: Push the BLEED key to get access to the "BLEED" page.	On the lower ECAM Display Unit (DU): The "BLEED" page comes into view. The white "GND" indication comes into view in the middle of the page.

(2) Make sure that the hydraulic systems are depressurized
(Ref. AMM TASK 29-10-00-864-003), (Ref. AMM TASK 29-23-00-864-001) and (Ref. AMM TASK 29-24-00-864-001).

Subtask 22-83-00-280-052-A ** ON A/C NOT FOR ALL

G. Check of the P/N(s) of the Software Component(s) Uploaded to the FMGC
(1) Get access to the "SYSTEM REPORT/TEST" menu page (Ref. AMM TASK 31-32-00-860-001).

ACTION	RESULT
1.Push the line select key adjacent to the "AFS" indication.	The "AFS MAIN MENU" page comes into view.
2.Push the line select key adjacent to the "LRU IDENTIFICATION" indication.	The "LRU IDENTIFICATION" page comes into view.
3.Make sure that the FMGC P/N(s) on the "LRU IDENTIFICATION" page is(are) of the "C1320XXXXX" type.
4.Do a check of: A.The three digits that follow ”C1320” of the FMGC P/N(s) shown on the "LRU IDENTIFICATION" page, and B.The LRU IDENT P/N(s) written on the media. If the three digits are the same, continue the procedure. If one digit is different (the FMGC and the media is(are) not compatible), stop the procedure and contact the airline engineering department to get the correct P/N(s) applicable to the aircraft.
5.Do a check of: A.The last two digits of the FMGC P/N(s) shown on the "LRU IDENTIFICATION" page, and B.The LRU IDENT P/N(s) written on the media. If the last two digits are different, continue the procedure. If the last two digits are the same (the software component(s) is(are) uploaded), the uploading is not necessary.

Subtask 22-83-00-280-052-D ** ON A/C NOT FOR ALL

G. Check of the P/N(s) of the Software Component(s) Uploaded to the FMGC
(1) Get access to the "SYSTEM REPORT/TEST" menu page (Ref. AMM TASK 31-32-00-860-001).

ACTION	RESULT
1.Push the line select key adjacent to the "AFS" indication.	The "AFS MAIN MENU" page comes into view.
2.Push the line select key adjacent to the "LRU IDENTIFICATION" indication.	The "LRU IDENTIFICATION" page comes into view.
3.Make sure that the FMGC P/N(s) on the "LRU IDENTIFICATION" page is(are) of the "C1320XXXXX" type.
4.Do a check of: A.The three digits that follow ”C1320” of the FMGC P/N(s) shown on the "LRU IDENTIFICATION" page, and B.The P/N(s) of the software. If the three digits are the same, continue the procedure. If one digit is different (the FMGC and the software is not compatible), stop the procedure and contact the airline engineering department to get the correct P/N(s) applicable to the aircraft.
5.Do a check of: A.The last two digits of the FMGC P/N(s) shown on the "LRU IDENTIFICATION" page, and B.The P/N(s) of the software. If the last two digits are different, continue the procedure. If the last two digits are the same (the software component(s) is(are) uploaded), the uploading is not necessary.

4. Procedure
Subtask 22-83-00-970-051-A ** ON A/C NOT FOR ALL

A. Uploading of the FG Software Component
(1) Make sure that the Data Loading Selector (DLS) is set to the FG1 or FG2 position.
(2) Upload the FG software component (Ref. AMM TASK 31-38-00-610-804).

Subtask 22-83-00-970-051-D ** ON A/C NOT FOR ALL

A. Uploading of the FG Software Component

NOTE: It is possible to upload the FG software component with the low or high speed dataloading.

(1) Make sure that the Data Loading Selector Unit (DLSU) is set to the FG1 or FG2 position.
(2) Upload the FG software component (Ref. AMM TASK 31-38-00-610-804).

Subtask 22-83-00-280-053-A ** ON A/C NOT FOR ALL

B. Do two checks of the P/N(s) of the FG software component(s) uploaded to the FMGC.

CAUTION: MAKE SURE THAT THE SOFTWARE INSTALLED AGREES WITH THE AIRLINE CONFIGURATION MANAGEMENT DOCUMENT. THE SYSTEM OPERATIONAL TEST OR BITE TEST DOES NOT DETECT INCORRECT SOFTWARE CONFIGURATION.

(1) Do a check of the P/N(s) of the FG software component(s) uploaded to the FMGC on the "LRU IDENTIFICATION" page.
(a) Get access to the "SYSTEM REPORT/TEST" menu page (Ref. AMM TASK 31-32-00-860-001).

ACTION	RESULT
1.Close circuit breaker 10CA1(2).
2.Make sure that: FMGC1(2) is on. No ECAM message related to FMGC1(2) is shown. The "1FD2" indication is shown on the Flight Mode Annunciator (FMA).
3.On the Multipurpose Control & Display Unit (MCDU): Push the line select key adjacent to the "AFS" indication.	On the MCDU: The "AFS MAIN MENU" page comes into view.
4.Push the line select key adjacent to the "LRU IDENTIFICATION" indication.	The "LRU IDENTIFICATION" page comes into view. The P/N(s) shown on this page is(are) the P/N(s) of the FG software component(s).
5.Make sure that the P/N(s) of the FMGC shown on the "LRU IDENTIFICATION" page is(are) the same as the LRU IDENT P/N(s) written on the media.
6.Push the MCDU MENU mode key.	The "MCDU MENU" page comes into view.

(2) Do a check of the P/N(s) of the FG software component(s) uploaded to the FMGC with the avionics configuration report:

ACTION	RESULT
1.On the MCDU: Push the line select key adjacent to the "CFDS" indication.	On the MCDU: The "CFDS MENU" page comes into view.
Push the NEXT key. Push the line select key adjacent to the "AVIONICS CONFIG REPORT" indication. Enter 22 (the applicable ATA number) in the scratchpad. Push the line select key adjacent to the "START" indication. Push the line select key adjacent to the FMGC.
2.Make sure that the P/N(s) of the FMGC shown on the "LRU IDENTIFICATION" page is(are) the same as the LRU IDENT P/N(s) written on the media.	The P/N(s) shown on this page is(are) the P/N(s) of the FG software component(s).

Subtask 22-83-00-280-053-C ** ON A/C NOT FOR ALL

B. Do two checks of the P/N(s) of the FG software component(s) uploaded to the FMGC.

CAUTION: MAKE SURE THAT THE SOFTWARE INSTALLED AGREES WITH THE AIRLINE CONFIGURATION MANAGEMENT DOCUMENT. THE SYSTEM OPERATIONAL TEST OR BITE TEST DOES NOT DETECT INCORRECT SOFTWARE CONFIGURATION.

ACTION	RESULT
1.Close circuit breaker 10CA1(2).
2.Make sure that: FMGC1(2) is on. No ECAM message related to FMGC1(2) is shown. The "1FD2" indication is shown on the Flight Mode Annunciator (FMA).
3.On the Multipurpose Control & Display Unit (MCDU): Push the line select key adjacent to the "AFS" indication.	On the MCDU: The "AFS MAIN MENU" page comes into view.
4.Push the line select key adjacent to the "LRU IDENTIFICATION" indication.	The "LRU IDENTIFICATION" page comes into view. The P/N(s) shown on this page is(are) the P/N(s) of the FG software component(s).
5.Do a check of the configuration of the uploaded software component(s).
6.Push the MCDU MENU mode key.	The "MCDU MENU" page comes into view.

(2) Do a check of the P/N(s) of the FG software component(s) uploaded to the FMGC with the avionics configuration report:

ACTION	RESULT
1.On the MCDU: Push the line select key adjacent to the "CFDS" indication.	On the MCDU: The "CFDS MENU" page comes into view.
Push the NEXT key. Push the line select key adjacent to the "AVIONICS CONFIG REPORT" indication. Enter 22 (the applicable ATA number) in the scratchpad. Push the line select key adjacent to the "START" indication. Push the line select key adjacent to the FMGC.
2.Do a check of the configuration of the uploaded software component(s).

Subtask 22-83-00-710-050-B ** ON A/C NOT FOR ALL

C. Operational Test of the Automatic Flight System (AFS)
(1) Do the operational test of the AFS only after the uploading of the FG software component (Ref. AMM TASK 22-96-00-710-001).

Subtask 22-83-00-860-059-B ** ON A/C NOT FOR ALL

D. Stop the PDL.
(1) Stop the ALT45200001 PORTABLE DATA LOADER (refer to PDL user guide).

Subtask 22-83-00-080-050-B ** ON A/C NOT FOR ALL

E. Removal of the PDL
(1) On the center pedestal, on DATA LOADING panel 117VU:

Disconnect the cable from the ALT45200001 PORTABLE DATA LOADER and from the data loader connector on the front face of the DLSU (103TD).

5. Close-up
Subtask 22-83-00-860-053-A ** ON A/C NOT FOR ALL

A. Put the aircraft back to its initial configuration.
(1) On the MCDU, push the MCDU MENU key to get access to the "MCDU MENU" page.
(2) Fully decrease the brightness of the MCDU screen (display off).
(3) If there is(are) media in the storage box, remove it(them). Then put the new media in the storage box.

Subtask 22-83-00-860-053-C ** ON A/C NOT FOR ALL

Subtask 22-83-00-862-050-A ** ON A/C NOT FOR ALL

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

[Rev.10 from 2021] 2026.03.31 23:11:13 UTC