Failure of the AC BUS 1 with the External Power in Use
TASK 24-50-00-810-808-A
Failure of the AC BUS 1 with the External Power in Use
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 24-50-00-860-062-A
Subtask 24-50-00-865-052-A
Subtask 24-50-00-860-063-A
[Rev.8 from Aug 2018]
2026.04.04 04:26:56 UTC
Failure of the AC BUS 1 with the External Power in Use
1. Possible Causes
- BTC-1 [11XU1]
- wiring
- RELAY-EPC AUX CTL [5XG]
- RELAY-GLC 1 AUX CTL [4XU1]
- GLC-1 [9XU1]
- RELAY-BUS TIE [30XU1]
- C/B-ELEC/EXT PWR/CTL [11XG]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 24-00-00-810-803-A | Circuit Breaker Tripped and/or C/B TRIPPED Warning |
| ASM 242202 | |
| AMM 24-22-55-000-001 | Removal of the Contactors |
| AMM 24-22-55-400-002 | Installation of the Contactors |
| ASM 242302 | |
| AMM 24-41-00-861-002 | Energize the Aircraft Electrical Circuits from the External Power |
| AMM 24-41-00-862-002 | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| ASM 244101 | |
| AMM 31-60-00-860-001 | EIS Start Procedure |
Subtask 24-50-00-860-062-A
A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
Subtask 24-50-00-710-064-A (1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
B. Test
(1) Do this test:
4. Fault Isolation(1) Do this test:
| ACTION | RESULT |
|---|---|
1.On the ELEC panel 35VU:
| On the ELEC panel 35VU:
|
Subtask 24-50-00-865-052-A
A. Table of the circuit breakers used in this procedure:
Subtask 24-50-00-810-057-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 122VU | ELEC/EXT PWR/CTL | 11XG | X29 |
B. If the test confirms the fault:
Subtask 24-50-00-810-057-B ** ON A/C NOT FOR ALL - Do a check of the status of the circuit breaker (11XG).
- Replace the BTC-1 [11XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
- Do a check and repair the wiring between the pin B/5 of the BTC1 and the pin AA/9C of the GCU1 ASM 242202.
- Do a check for 28VDC:
- Replace the RELAY-EPC AUX CTL [5XG] .
- Repair the wiring between the circuit breaker ELEC/EXT PWR/CTL (11XG) and the relay (5XG) ASM 244101.
- Replace the RELAY-GLC 1 AUX CTL [4XU1] .
- Repair the wiring between the pin A/D2 of the relay (5XG) and the pin A/A3 of the relay (4XU1) ASM 242202 and ASM 242302.
- Replace the GLC-1 [9XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
- Repair the wiring between the pin A/A2 of the relay (4XU1) and the pin B/8 of the GLC1 (9XU1) ASM 242202.
- Replace the RELAY-BUS TIE [30XU1] .
- Do a check and repair the wiring between:
. the pin B/6 of the GLC1 (9XU1) and the pin A/B2 of the relay (30XU1) ASM 242202,
. the pin A/B3 of the relay (30XU1) and the pin B/3 of the BTC1 (11XU1) ASM 242202.
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace the C/B-ELEC/EXT PWR/CTL [11XG] .
B. If the test confirms the fault:
Subtask 24-50-00-810-057-C ** ON A/C NOT FOR ALL - Do a check of the status of the circuit breaker (11XG).
- Replace BTC-1 [11XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
- Do a check and repair the wiring between pin B/5 of BTC1 and pin AA/9C of GCU1 ASM 242202.
- Do a check for 28VDC:
- Replace RELAY-EPC AUX CTL [5XG] .
- Repair the wiring between the circuit breaker ELEC/EXT PWR/CTL (11XG) and the relay (5XG) ASM 244101.
- Replace RELAY-GLC 1 AUX CTL [4XU1] .
- Repair the wiring between pin A/D2 of the relay (5XG) and pin A/A3 of the relay (4XU1) ASM 242202 and ASM 242302.
- Replace GLC-1 [9XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
- Repair the wiring between pin A/A2 of the relay (4XU1) and pin B/24 of GLC1 (9XU1) ASM 242202.
- Replace RELAY-BUS TIE [30XU1] .
- Do a check and repair the wiring between:
. Pin B/22 of the GLC1 (9XU1) and pin A/B2 of the relay (30XU1) ASM 242202
. Pin A/B3 of the relay (30XU1) and pin B/3 of BTC1 (11XU1) ASM 242202.
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace C/B-ELEC/EXT PWR/CTL [11XG] .
B. If the test confirms the fault:
Subtask 24-50-00-710-065-A - Do a check of the status of the circuit breaker (11XG).
- Replace BTC-1 [11XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
- Do a check and repair the wiring between pin B/5 of BTC1 and pin AA/9A of GCU1 ASM 242202.
- Do a check for 28VDC:
- Replace RELAY-EPC AUX CTL [5XG] .
- Repair the wiring between the circuit breaker ELEC/EXT PWR/CTL (11XG) and the relay (5XG) ASM 244101.
- Replace RELAY-GLC 1 AUX CTL [4XU1] .
- Repair the wiring between pin A/D2 of the relay (5XG) and pin A/A3 of the relay (4XU1) ASM 242202 and ASM 242302.
- Replace GLC-1 [9XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
- Repair the wiring between pin A/A2 of the relay (4XU1) and pin B/24 of GLC1 (9XU1) ASM 242202.
- Replace RELAY-BUS TIE [30XU1] .
- Do a check and repair the wiring between:
. Pin B/22 of GLC1 (9XU1) and pin A/B2 of the relay (30XU1) ASM 242202,
. Pin A/B3 of the relay (30XU1) and pin B/3 of BTC1 (11XU1) ASM 242202.
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace C/B-ELEC/EXT PWR/CTL [11XG] .
C. Do this test to make sure that the system operates correctly:
5. Close-up| ACTION | RESULT |
|---|---|
1.On the ECAM control panel:
| On the lower ECAM display unit:
|
Subtask 24-50-00-860-063-A
A. Put the aircraft back to its initial configuration.
(1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(2) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
(1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(2) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.