Loss of the Signal from the Tachometer (Wheel 4) to the BSCU
TASK 32-42-00-810-815-A
Loss of the Signal from the Tachometer (Wheel 4) to the BSCU
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 32-42-00-720-050-A ** ON A/C NOT FOR ALL Subtask 32-42-00-720-050-B ** ON A/C NOT FOR ALL
Subtask 32-42-00-810-064-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:31:31 UTC
Loss of the Signal from the Tachometer (Wheel 4) to the BSCU
1. Possible Causes
- DRIVE ASSY-TACHOMETER,WHEEL 4 [2678GM]
- BSCU [10GG]
- TACHOMETER-WHEEL 4 [22GG]
- wiring
- SEC-2 [1CE2]
- SEC-3 [1CE3]
wiring from the tachometer (22GG) pins A/A and A/C to the BSCU (10GG) pins AB/8K, AB/8J
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 27-94-34-000-001 | Removal of the SEC |
| AMM 27-94-34-400-001 | Installation of the SEC |
| AMM 32-41-11-000-006 | Removal of the MLG Wheel |
| AMM 32-41-11-400-006 | Installation of the MLG Wheel |
| AMM 32-42-00-720-002 | Functional Test of the Tachometers and the Anti-Skid System with the Normal Braking System ON |
| AMM 32-42-00-720-003 | Functional Test of the tachometers with the AIDS. |
| ASM 324202 | |
| AMM 32-42-34-000-001 | Removal of the Braking/Steering Control Unit (BSCU) |
| AMM 32-42-34-400-001 | Installation of the Braking/Steering Control Unit (BSCU) |
| AMM 32-42-57-000-001 | Removal of the Tachometer |
| AMM 32-42-57-400-001 | Installation of the Tachometer |
| AMM 32-42-68-000-003 | Removal of the MLG Tachometer-Drive |
| AMM 32-42-68-400-003 | Installation of the MLG Tachometer-Drive |
| TSM TASK 32-42-00-03 | NORMAL BRAKING - TASK SUPPORTING DATA |
Subtask 32-42-00-720-050-A ** ON A/C NOT FOR ALL Subtask 32-42-00-720-050-B ** ON A/C NOT FOR ALL
A. Do a Check to Know if the Fault Message is Spurious or Not.
(1) If you find all of the conditions that follow, the fault message is spurious:
(a) Do a check of the last five entries in the aircraft logbook and make sure that these ECAM warnings are not shown:
1 Make sure that the PFR gives the ECAM warning:
32-42-00-03 TSM TASK 32-42-00-03 .
(d) Make sure that the REFERENCE SPEED is more than 100 kts in the TSD, page 1/232-42-00-03 TSM TASK 32-42-00-03 .
4. Fault Isolation(1) If you find all of the conditions that follow, the fault message is spurious:
(a) Do a check of the last five entries in the aircraft logbook and make sure that these ECAM warnings are not shown:
- BRAKES AUTO BRK FAULT/BRAKE RELEASED
- BRAKES RELEASED.
1 Make sure that the PFR gives the ECAM warning:
- BRAKES AUTO BRK FAULT/BRAKE RELEASED, or
- BRAKES RELEASED.
NOTE: If the PFR gives also the message SEC2 OR INPUT OF WHEEL TACHOMETER or SEC3 OR INPUT OF WHEEL TACHOMETER, it is necessary to do the related troubleshooting procedure.
(c) Make sure that the TROUBLE SHOOTING DATA (TSD) gives the fault code 853 (d) Make sure that the REFERENCE SPEED is more than 100 kts in the TSD, page 1/2
Subtask 32-42-00-810-064-A ** ON A/C NOT FOR ALL
A. If the test does not confirm the fault:
(1) Do a visual inspection of the tachometer drive mechanism and make sure that:
Subtask 32-42-00-810-064-B ** ON A/C NOT FOR ALL (1) Do a visual inspection of the tachometer drive mechanism and make sure that:
- The tachometer drive shaft moves freely.
- The splines of the tachometer drive shaft are in the correct condition.
- The splines of the tachometer hubcap or the splines of the debris guard (if brake fans are installed) are in the correct condition.
NOTE: The functional test of the tachometer can be correct although the splines are worn.
(2) If the tachometer drive is damaged: - Replace the DRIVE ASSY-TACHOMETER,WHEEL 4 [2678GM] AMM 32-42-68-000-003 and AMM 32-42-68-400-003.
- Replace the tachometer hubcap or the debris guard of the MLG wheel AMM 32-41-11-000-006 and AMM 32-41-11-400-006.
A. Confirmation of the type of failure on the TROUBLE SHOOTING DATA of the BSCU:
(1) If the TROUBLE SHOOTING DATA gives fault code 853:
Subtask 32-42-00-810-252-A ** ON A/C NOT FOR ALL (1) If the TROUBLE SHOOTING DATA gives fault code 853:
- Refer to Para. B.
- Refer to Para. C.
B. Do a check to know if the fault message is spurious or not.
(1) If the two conditions that follow occur at the same time, the fault is spurious:
(a) Do a check of the last five flight entries in the aircraft logbook:
32-42-00-03 TSM TASK 32-42-00-03 .
(2) If the fault is spurious:
Subtask 32-42-00-810-245-A ** ON A/C NOT FOR ALL (1) If the two conditions that follow occur at the same time, the fault is spurious:
(a) Do a check of the last five flight entries in the aircraft logbook:
- Make sure that there are no other BRAKES AUTO BRK FAULT/BRAKE RELEASED or other BRAKES RELEASED ECAM warnings in the last five flights.
(2) If the fault is spurious:
- Do a reset of the BSCU [10GG] : set the A/SKID & N/W STRG switch to OFF, then to ON, on landing gear control and indicating panel 402VU.
- Refer to Para. C.
C. If the test confirms the fault:
(1) Do a visual inspection of the tachometer drive mechanism and make sure that:
Subtask 32-42-00-720-051-A ** ON A/C NOT FOR ALL (1) Do a visual inspection of the tachometer drive mechanism and make sure that:
- The tachometer drive shaft moves freely and the splines of the tachometer drive shaft are in the correct condition.
- The splines of the tachometer hubcap or the splines of the debris guard (if brake fans are installed) are in the correct condition.
- Replace the DRIVE ASSY-TACHOMETER,WHEEL 4 [2678GM] AMM 32-42-68-000-003 and AMM 32-42-68-400-003.
- Replace the tachometer hubcap or the debris guard of the MLG wheel AMM 32-41-11-000-006 and AMM 32-41-11-400-006.
- Replace the TACHOMETER-WHEEL 4 [22GG] AMM 32-42-57-000-001 and AMM 32-42-57-400-001.
- Do a check of the wiring ASM 324202 between:
. Pin A/A of the TACHOMETER-WHEEL 4 [22GG] and pin AB/8K of the BSCU [10GG]
. Pin A/C of the TACHOMETER-WHEEL 4 [22GG] and pin AB/8J of the BSCU [10GG]
- Repair the wiring .
- Replace the BSCU [10GG] AMM 32-42-34-000-001 and AMM 32-42-34-400-001.
- Replace the SEC-2 [1CE2] AMM 27-94-34-000-001 and AMM 27-94-34-400-001.
- Replace the SEC-3 [1CE3] AMM 27-94-34-000-001 and AMM 27-94-34-400-001.
D. Do the functional test given in Para. 3.A.
Subtask 32-42-00-810-245-B ** ON A/C NOT FOR ALL E. Do the functional test of the tachometer AMM 32-42-00-720-002 or AMM 32-42-00-720-003.
(1) If the test does not confirm the fault:
(a) Do a visual inspection of the tachometer drive mechanism and make sure that:
(a) Do a visual inspection of the tachometer drive mechanism and make sure that:
Subtask 32-42-00-720-051-B ** ON A/C NOT FOR ALL (1) If the test does not confirm the fault:
(a) Do a visual inspection of the tachometer drive mechanism and make sure that:
- The tachometer drive shaft moves freely.
- The splines of the tachometer drive shaft are in the correct condition.
- The splines of the tachometer hubcap or the splines of the debris guard (if brake fans are installed) are in the correct condition.
NOTE: The functional test of the tachometer can be correct although the splines are worn.
(b) If the tachometer drive is damaged: - Replace the DRIVE ASSY-TACHOMETER,WHEEL 4 [2678GM] AMM 32-42-68-000-003 and AMM 32-42-68-400-003.
- Replace the tachometer hubcap or the debris guard of the MLG wheel AMM 32-41-11-000-006 and AMM 32-41-11-400-006.
(a) Do a visual inspection of the tachometer drive mechanism and make sure that:
- The tachometer drive shaft moves freely.
- The splines of the tachometer drive shaft are in the correct condition.
- The splines of the tachometer hubcap or the splines of the debris guard (if brake fans are installed) are in the correct condition.
- Replace the DRIVE ASSY-TACHOMETER,WHEEL 4 [2678GM] AMM 32-42-68-000-003 and AMM 32-42-68-400-003.
- Replace the tachometer hubcap or the debris guard of the MLG wheel AMM 32-41-11-000-006 and AMM 32-41-11-400-006.
- Replace the TACHOMETER-WHEEL 4 [22GG] AMM 32-42-57-000-001 and AMM 32-42-57-400-001.
- Do a check and repair the
wiring from the tachometer (22GG) pins A/A and A/C to the BSCU (10GG) pins AB/8K, AB/8J ASM 324202. - Do the functional test of the tachometer AMM 32-42-00-720-002 or AMM 32-42-00-720-003.
- Replace the BSCU [10GG] AMM 32-42-34-000-001 and AMM 32-42-34-400-001.
- Replace the SEC-2 [1CE2] AMM 27-94-34-000-001 and AMM 27-94-34-400-001.
- Replace the SEC-3 [1CE3] AMM 27-94-34-000-001 and AMM 27-94-34-400-001.
F. After the subsequent flight, make sure that the fault does not continue.