Failure of the TR2 or TR2 Contactor or Related Wiring
TASK 24-30-00-810-802-A
Failure of the TR2 or TR2 Contactor or Related Wiring
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 24-30-00-860-052-A
Subtask 24-30-00-865-051-A
Subtask 24-30-00-860-053-A
[Rev.8 from Aug 2018]
2026.04.04 04:39:04 UTC
Failure of the TR2 or TR2 Contactor or Related Wiring
1. Possible Causes
- CNTOR-TR 2 [5PU2]
- CNTOR-TR 2/AC SVCE BUS NORM SPLY [14PU]
- TR-2 [1PU2]
- wiring
- RELAY-GND/FLT SELECT CTL [7XX]
- CNTOR-AC & DC GND SVCE SPLY [14XX]
- C/B-TR2/214XP/SPLY [2PU2]
- C/B-TR2/CNTOR/SPLY [4PU2]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 24-00-00-810-803-A | Circuit Breaker Tripped and/or C/B TRIPPED Warning |
| ASM 243201 | |
| AMM 24-32-51-000-001 | Removal of the Transformer Rectifier |
| AMM 24-32-51-400-001 | Installation of the Transformer Rectifier |
| AMM 24-32-55-000-001 | Removal of the TR 1 and TR 2 Contactors and the TR 2/AC Service Bus Normal Supply Contactor |
| AMM 24-32-55-400-001 | Installation of the TR 1 and TR 2 Contactors and the TR 2/AC Service Bus Normal Supply Contactor |
| 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 244201 | |
| AMM 24-42-55-000-001 | Removal of the Contactors |
| AMM 24-42-55-400-001 | Installation of the Contactors |
| AMM 31-32-00-860-004 | Procedure to Get Access to the SYSTEM REPORT/TEST/ELEC Page |
| AMM 31-60-00-860-001 | EIS Start Procedure |
| AMM 31-60-00-860-002 | EIS Stop Procedure |
Subtask 24-30-00-860-052-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.
(c) On the MCDU, get the ELEC menu on the SYSTEM REPORT/TEST page AMM 31-32-00-860-004.
Subtask 24-30-00-710-052-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.
(c) On the MCDU, get the ELEC menu on the SYSTEM REPORT/TEST page AMM 31-32-00-860-004.
B. Test
4. Fault IsolationNOTE: Before you do the test of the TR2, make sure that the AC BUS 2 supplies its primary winding, in any RESET mode.
| ACTION | RESULT |
|---|---|
1.On the ECAM control panel:
| On the upper ECAM DU:
|
| | On the lower ECAM DU, on the ELEC page:
|
2.On the MCDU:
| The TR2 page comes into view. |
NOTE: If the CFDS is not available, you can reset with the TR RESET pushbutton switch (15PU) which is on the relay box 103VU. | If on the TR2 page:
|
Subtask 24-30-00-865-051-A
A. Table of the circuit breakers used in this procedure:
Subtask 24-30-00-810-051-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 123VU | TR2/214XP/SPLY | 2PU2 | AB04 |
| 124VU | TR2/CNTOR/SPLY | 4PU2 | BC01 |
B. If the fault continues:
Subtask 24-30-00-810-051-B ** ON A/C NOT FOR ALL - Do a check of the status of the circuit breakers 4PU2 and 2PU2.
- Do a check of the TR2 voltage on the lower ECAM DU, on the ELEC page.
- Replace the CNTOR-TR 2 [5PU2] AMM 24-32-55-000-001 and AMM 24-32-55-400-001.
- Replace CNTOR-TR 2/AC SVCE BUS NORM SPLY [14PU] AMM 24-32-55-000-001 and AMM 24-32-55-400-001.
- Replace TR-2 [1PU2] AMM 24-32-51-000-001 and AMM 24-32-51-400-001.
- Do a check and repair the wiring between ASM 243201:
- Pin B/3 of the TR2 contactor (5PU2) and the pin B/11 of the contactor 14PU
- Pin B/13 of the contactor 14PU and the circuit-breaker 4PU2.
- Do a check and repair the wiring between ASM 243201:
- Pin B/F of the TR-2 (1PU2) and the pin A/41 of the diode module (2420VD)
- Pin A/42 of the diode module (2420VD) and the B/5 of the TR2 contactor (5PU2).
- Replace RELAY-GND/FLT SELECT CTL [7XX] .
- Replace CNTOR-AC & DC GND SVCE SPLY [14XX] AMM 24-42-55-000-001 and AMM 24-42-55-400-001.
- Do a check and repair the wiring between ASM 243201:
- Pin A2 of the TR2 supply circuit-breaker (2PU2) and the pin D of the contactor (14PU)
- Pin B2 of the TR2 supply circuit-breaker (2PU2) and the pin E of the contactor (14PU)
- Pin C2 of the TR2 supply circuit-breaker (2PU2) and the pin F of the contactor (14PU)
- Pin M of the contactor (14PU) and the pin A/A of the TR-2 (1PU2)
- Pin L of the contactor (14PU) and the pin A/A of the TR-2 (1PU2)
- Pin K of the contactor (14PU) and the pin A/A of the TR-2 (1PU2).
- Do a check for 115VAC on the pins M, L, K of the contactor (14PU) ASM 243201
- Replace TR-2 [1PU2] AMM 24-32-51-000-001 and AMM 24-32-51-400-001.
- Do a check and repair the wiring between ASM 243201.
- Pin AA of the TR2 (1PU2) and the pin M of the the contactor (14PU)
- Pin AB of the TR2 (1PU2) and the pin L of the the contactor (14PU)
- Pin AC of the TR2 (1PU2) and the pin K of the the contactor (14PU).
- Do a check for 115VAC on the pins D, E, F of the contactor (14PU).
- Replace RELAY-GND/FLT SELECT CTL [7XX] .
* If the fault continues:
* - Replace CNTOR-TR 2/AC SVCE BUS NORM SPLY [14PU] AMM 24-32-55-000-001 and AMM 24-32-55-400-001.
* If the fault continues:
* - Replace CNTOR-AC & DC GND SVCE SPLY [14XX] AMM 24-42-55-000-001 and AMM 24-42-55-400-001.
* If the fault continues:
* - Do a check and repair the wiring between ASM 244201:
** - Pin 3 of the contactor (14PU) and the ELEC/AC PWR/SVCE/CTL circuit breaker(3XX)
** - Pin 5 of the contactor (14PU) and the ground.
- Do a check and repair the wiring between the circuit breaker (2PU2) and the contactor (14PU) ASM 244201.
- Do a check and repair the wiring between pin 5 of the TR2 contactor 5U2 and the circuit breaker 4PU2 ASM 243201.
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace C/B-TR2/214XP/SPLY [2PU2] .
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace C/B-TR2/CNTOR/SPLY [4PU2] .
B. If the fault continues:
Subtask 24-30-00-710-053-A - Do a check of the status of the circuit breakers 4PU2 and 2PU2.
- Do a check of the TR2 voltage on the lower ECAM DU, on the ELEC page.
- Replace CNTOR-TR 2 [5PU2] AMM 24-32-55-000-001 and AMM 24-32-55-400-001.
- Replace CNTOR-TR 2/AC SVCE BUS NORM SPLY [14PU] AMM 24-32-55-000-001 and AMM 24-32-55-400-001.
- Replace TR-2 [1PU2] AMM 24-32-51-000-001 and AMM 24-32-51-400-001.
- Do a check and repair the wiring between the ASM 243201.
- Pin B/3 of the TR2 contactor (5PU2) and the pin B/11 of the contactor 14PU
- Pin B/13 of the contactor 14PU and the circuit-breaker 4PU2.
- Do a check and repair the wiring between the ASM 243201:
- Pin B/F of the TR-2 (1PU2) and the pin A/41 of the diode module (2420VD)
- Pin A/42 of the diode module (2420VD) and the B/5 of the TR2 contactor (5PU2).
- Replace RELAY-GND/FLT SELECT CTL [7XX] .
- Replace CNTOR-AC & DC GND SVCE SPLY [14XX] AMM 24-42-55-000-001 and AMM 24-42-55-400-001.
- Do a check and repair the wiring between the ASM 243201:
- Pin A2 of the TR2 supply circuit-breaker (2PU2) and the pin 22 of the module AC-service-bus contactor (20XX)
- Pin B2 of the TR2 supply circuit-breaker (2PU2) and the pin 23 of the module AC-service-bus contactor (20XX)
- Pin C2 of the TR2 supply circuit-breaker (2PU2) and the pin 24 of the module AC-service-bus contactor (20XX)
- Pin 16 of the module AC-service-bus contactor (20XX) and the pin A/A of the TR-2 (1PU2)
- Pin 20 of the module AC-service-bus contactor (20XX) and the pin A/B of the TR-2 (1PU2)
- Pin 18 of the module AC-service-bus contactor (20XX) and the pin A/C of the TR-2 (1PU2).
- Do a check for 115VAC on the pins 16, 20, 18 of the module 20XX ASM 243201.
- Replace TR-2 [1PU2] AMM 24-32-51-000-001 and AMM 24-32-51-400-001.
- Do a check and repair the wiring between ASM 243201:
- Pin AA of the TR2 (1PU2) and the pin 16 of the module AC-service-bus contactor (20XX)
- Pin AB of the TR2 (1PU2) and the pin 20 of the module AC-service-bus contactor (20XX)
- Pin AC of the TR2 (1PU2) and the pin 18 of the module AC-service-bus contactor (20XX).
- Do a check for 115VAC on the pins 22, 23, 24 of the module 20XX.
- Replace RELAY-GND/FLT SELECT CTL [7XX] .
* If the fault continues:
* - Replace CNTOR-TR 2/AC SVCE BUS NORM SPLY [14PU] AMM 24-32-55-000-001 and AMM 24-32-55-400-001.
* If the fault continues:
* - Replace CNTOR-AC & DC GND SVCE SPLY [14XX] AMM 24-42-55-000-001 and AMM 24-42-55-400-001.
* If the fault continues:
* - Do a check and repair the wiring between ASM 244201:
** - Pin 3 of the contactor (14PU) and the ELEC/AC PWR/SVCE/CTL circuit breaker(3XX)
** - Pin 5 of the contactor (14PU) and the ground.
- Do a check and repair the wiring between the circuit breaker (2PU2) and the module 20XX ASM 244201.
- Do a check and repair the wiring between pin 5 of the TR2 contactor 5PU2 and the circuit breaker 4PU2 ASM 243201.
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace the C/B-TR2/214XP/SPLY [2PU2] .
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace the C/B-TR2/CNTOR/SPLY [4PU2] .
C. Do the Test:
5. Close-up| ACTION | RESULT |
|---|---|
1.On the MCDU:
| The TR2 page comes into view. |
| The NO FAULT indication comes into view. |
Subtask 24-30-00-860-053-A
A. Put the aircraft back to its initial configuration.
(1) On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) Do the EIS stop procedure AMM 31-60-00-860-002.
(3) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
(1) On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) Do the EIS stop procedure AMM 31-60-00-860-002.
(3) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.