Deactivation of the BSCU Channel/System 1 or 2
TASK 32-42-00-040-007-A
Deactivation of the BSCU Channel/System 1 or 2
1. Reason for the Job
MMEL 32-42-03A
BRAKING/STEERING CONTROL UNIT (BSCU) CHANNEL 1
MMEL 32-42-04A
BRAKING/STEERING CONTROL UNIT (BSCU) CHANNEL 2
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 32-42-00-860-100-A
Subtask 32-42-00-040-057-D
Subtask 32-42-00-860-101-A
[Rev.10 from 2021]
2026.04.01 00:47:27 UTC
Deactivation of the BSCU Channel/System 1 or 2
1. Reason for the Job
MMEL 32-42-03A
BRAKING/STEERING CONTROL UNIT (BSCU) CHANNEL 1
MMEL 32-42-04A
BRAKING/STEERING CONTROL UNIT (BSCU) CHANNEL 2
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 31-32-00-860-009-A | Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
Subtask 32-42-00-860-100-A
A. Aircraft Maintenance Configuration
(1) On the panel 400VU, make sure that the landing gear control lever is in the DOWN position.
(2) Make sure that the CAPT and F/O brake pedals are released.
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) On the panel 402VU, make sure that the A/SKID & N/W STRG switch is at ON.
(5) Put the WARNING NOTICE(S) in position to tell persons not to operate:
Subtask 32-42-00-865-074-A (1) On the panel 400VU, make sure that the landing gear control lever is in the DOWN position.
(2) Make sure that the CAPT and F/O brake pedals are released.
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) On the panel 402VU, make sure that the A/SKID & N/W STRG switch is at ON.
(5) Put the WARNING NOTICE(S) in position to tell persons not to operate:
- the landing gear control-lever
- the A/SKID & N/W STRG switch
- the brake pedals.
B. Table of the circuit breakers used in this procedure:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY | 4GG | M36 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY | 2GG | M33 |
Subtask 32-42-00-040-057-D
A. Deactivation of the BSCU System 1 or 2
(1) If there is loss of one BSCU system, on the upper ECAM DU, make sure that the BRAKES SYS 1 FAULT or BRAKES SYS 2 FAULT warning is shown.
(a) Get access to the SYSTEM REPORT/TEST/L/G page (Ref. AMM TASK 31-32-00-860-009).
(b) Print the trouble shooting data, the ground report, the ground scanning, the class 3 fault messages, and the Post Flight Report (PFR) of the related BSCU as follows:
(4) Make an entry in the log book to tell persons that the BSCU system 1 or 2 is deactivated.
5. Close-up(1) If there is loss of one BSCU system, on the upper ECAM DU, make sure that the BRAKES SYS 1 FAULT or BRAKES SYS 2 FAULT warning is shown.
(a) Get access to the SYSTEM REPORT/TEST/L/G page (Ref. AMM TASK 31-32-00-860-009).
(b) Print the trouble shooting data, the ground report, the ground scanning, the class 3 fault messages, and the Post Flight Report (PFR) of the related BSCU as follows:
| ACTION | RESULT |
|---|---|
| - Push the line key adjacent to the BSCU1 or BSCU2 indication. | - The BSCU1 or BSCU2 page comes into view. |
| - Push the line key adjacent to the TROUBLE SHOOT DATA indication. | - The TROUBLE SHOOT DATA page comes into view. |
| - Push the line key adjacent to the PRINT indication. | |
| - Push the line key adjacent to the RETURN indication. | - The BSCU1 or BSCU2 page comes into view. |
| - Push the line key adjacent to the GROUND REPORT indication. | - The GROUND REPORT page comes into view. |
| - Push the line key adjacent to the PRINT indication. | |
| - Push the line key adjacent to the RETURN indication. | - The BSCU1 or BSCU2 page comes into view. |
| - Push the line key adjacent to the GROUND SCANNING indication. | - The GROUND SCANNING page comes into view. |
| - Push the line key adjacent to the PRINT indication. | |
| - Push the line key adjacent to the RETURN indication. | - The BSCU1 or BSCU2 page comes into view. |
| - Push the line key adjacent to the CLASS 3 FAULTS indication. | - The CLASS 3 FAULTS page comes into view. |
| - Push the line key adjacent to the PRINT indication. | |
| - Push the line key adjacent to the RETURN indication until you get the CFDS MENU page. | - The CFDS MENU page comes into view. |
| - Push the line key adjacent to the POST FLIGHT REP PRINT indication. | |
NOTE: It is important to keep these documents to do the maintenance of the BSCU in shop.
(c) On the upper ECAM DU, if the BRAKES SYS 1 FAULT warning is shown: - Open, safety and tag the circuit breaker 2GG.
- Open, safety and tag the circuit breaker 4GG.
- On the MCDU, get access to the CFDS MENU page.
- Push the line key adjacent to the CFDS indication.
- Push the line key adjacent to the LAST LEG REPORT indication.
- On the LAST LEG REPORT page, make sure that none of the following fault messages related to the L/G SYS DISAGREE caution message is recorded:
R L/G DOOR CLOSED PROX SNSR 26GA TGT POS
L L/G DOOR CLOSED PROX SNSR 27GA TGT POS
R L/G DOOR CLOSED PROX SNSR 28GA TGT POS
L L/G DOOR CLOSED PROX SNSR 29GA TGT POS
N L/G DOOR CLOSED PROX SNSR 30GA TGT POS
N L/G DOOR CLOSED PROX SNSR 31GA TGT POS
R L/G DOOR OPEN PROX SNSR 32GA TGT POS
L L/G DOOR OPEN PROX SNSR 33GA TGT POS
R L/G DOOR OPEN PROX SNSR 34GA TGT POS
L L/G DOOR OPEN PROX SNSR 35GA TGT POS
N L/G R DOOR OPEN PROX SNSR 36GA TGT POS
N L/G L DOOR OPEN PROX SNSR 37GA TGT POS
N L/G R DOOR OPEN PROX SNSR 38GA TGT POS
N L/G L DOOR OPEN PROX SNSR 39GA TGT POS
(4) Make an entry in the log book to tell persons that the BSCU system 1 or 2 is deactivated.
Subtask 32-42-00-860-101-A
A. Put the aircraft back to the serviceable condition.
(1) Remove the WARNING NOTICE(S).
(1) Remove the WARNING NOTICE(S).