DOC AIRBUS | AMM A320FOperational Test of the Brake Temperature System
TASK 32-47-00-710-001-A
Operational Test of the Brake Temperature System
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 32-47-00-860-051-A
Subtask 32-47-00-710-050-A
Subtask 32-47-00-942-052-A
[Rev.10 from 2021]
2026.04.01 12:30:06 UTC
Operational Test of the Brake Temperature System
WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | WARNING NOTICE(S) |
| 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 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 32-47-00-860-051-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) On the panel 400 VU, make sure that the landing gear control-lever is in the DOWN position.
(3) Do the EIS Start procedure (Ref. AMM TASK 31-60-00-860-001).
Subtask 32-47-00-865-050-A (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) On the panel 400 VU, make sure that the landing gear control-lever is in the DOWN position.
(3) Do the EIS Start procedure (Ref. AMM TASK 31-60-00-860-001).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 32-47-00-941-052-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/BRK/TEMP/DET/UNIT | 1GW | M37 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY | 4GG | M36 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS2/CTL | 3GG | M35 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS1/CTL | 1GG | M34 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY | 2GG | M33 |
C. Safety Precautions
(1) Put the WARNING NOTICE(S) on the landing gear control-lever to tell persons not to operate it.
4. Procedure(1) Put the WARNING NOTICE(S) on the landing gear control-lever to tell persons not to operate it.
Subtask 32-47-00-710-050-A
A. Test of the Brake Temperature System
Subtask 32-47-00-860-050-A | ACTION | RESULT |
|---|---|
| On the ECAM control panel: | |
| - on the lower ECAM DU, the WHEEL page comes into view. Make sure that the temperatures shown relate to the ambient temperature with a precision of plus or minus 25 deg.C (45 deg.F). NOTE: In case of negative temperatures, or temperatures near 0 deg.C (32 deg.F), the indication on the display unit ranges from 0 deg.C to 25 deg.C (32 deg.F to 77 deg.F) approximately. |
B. Aircraft Maintenance Configuration
(1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
5. Close-up(1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 32-47-00-942-052-A
A. Removal of Equipment
(1) Remove the WARNING NOTICE(S).
(1) Remove the WARNING NOTICE(S).