Failure of the 212XP and 216XP Busbars in Normal Flight Configuration
TASK 24-50-00-810-813-A
Failure of the 212XP and 216XP Busbars in Normal Flight Configuration
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 24-50-00-860-072-A
Subtask 24-50-00-810-062-A ** ON A/C NOT FOR ALL
Subtask 24-50-00-860-073-A
[Rev.8 from Aug 2018]
2026.04.04 04:26:56 UTC
Failure of the 212XP and 216XP Busbars in Normal Flight Configuration
1. Possible Causes
- wiring
- C/B-BUS 2/212XP/SPLY [10XN]
- CNTOR-AC SVCE BUS NORM SPLY [12XN]
- RELAY-GND/FLT SELECT CTL [7XX]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 24-00-00-810-803-A | Circuit Breaker Tripped and/or C/B TRIPPED Warning |
| 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 | |
| ASM 245103 | |
| AMM 24-51-55-000-001 | Removal of the AC Service Bus Normal Supply Contactor |
| AMM 24-51-55-400-001 | Installation of the AC Service Bus Normal Supply Contactor |
Subtask 24-50-00-860-072-A
A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits AMM 24-41-00-861-002.
Subtask 24-50-00-710-074-A (1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits AMM 24-41-00-861-002.
B. Test
4. Fault Isolation| ACTION | RESULT |
|---|---|
| 1.On the forward attendant panel 120RH, push the CABIN WDO and CABIN CLG pushbutton switches. |
|
Subtask 24-50-00-810-062-A ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
Subtask 24-50-00-810-062-B ** ON A/C NOT FOR ALL - Do a check of the status of the circuit breaker (10XN).
- Do a check for 115VAC on the pins A/D, A/E and A/F of the contactor (12XN) ASM 245103.
- Do a check of the wiring between the circuit breaker (10XN) and the contactor (12XN) ASM 245103.
- Repair the wiring .
- Replace the C/B-BUS 2/212XP/SPLY [10XN] .
- Replace the CNTOR-AC SVCE BUS NORM SPLY [12XN] AMM 24-51-55-000-001 and AMM 24-51-55-400-001.
- Do a check of the wiring between pins A/N, A/P and A/R of the contactor (12XN) and the busbars 212XP and 216XP ASM 244201.
- Repair the wiring .
- Replace the RELAY-GND/FLT SELECT CTL [7XX] .
- Do a check and repair the wiring :
. from the circuit breaker (3XX) to the pin B/3 of the contactor (12XN).
. from the pin B/5 of the contactor (12XN) to the first terminal block ASM 245103.
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace the C/B-BUS 2/212XP/SPLY [10XN] .
A. If the test confirms the fault:
Subtask 24-50-00-710-075-A - Do a check of the status of the circuit breaker (10XN).
- Do a check for 115VAC on the pins 10, 11, 12 of the module 20XX ASM 245103.
- Do a check of the wiring between the circuit breaker (10XN) and the module 20XX ASM 245103.
- Repair the wiring .
- Replace the C/B-BUS 2/212XP/SPLY [10XN] .
- Replace the CNTOR-AC SVCE BUS NORM SPLY [12XN] AMM 24-51-55-000-001 and AMM 24-51-55-400-001.
- Do the check of the wiring between pins A/N, A/P and A/R of the contactor (12XN) and the busbars 212XP and 216XP ASM 244201.
- Repair the wiring .
- Replace the RELAY-GND/FLT SELECT CTL [7XX] .
- Do a check and repair the wiring :
. from the circuit breaker (3XX) to the pin B/3 of the contactor (12XN).
. from the pin B/5 of the contactor (12XN) to the first terminal block ASM 245103.
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace the C/B-BUS 2/212XP/SPLY [10XN] .
B. Do this test to make sure that the system operates correctly.
(1) Do the test given in Para. 3. and make sure that:
5. Close-up(1) Do the test given in Para. 3. and make sure that:
- the ceiling forward and aft lights (L side) come on
- the window forward and aft lights (R side) come on.
Subtask 24-50-00-860-073-A
A. Put the aircraft back to its initial configuration.
(1) On the forward attendant panel 120RH release the CABIN WDO and CABIN CLG pushbutton switches.
(2) De-energize the aircraft electrical circuits AMM 24-41-00-862-002.
(1) On the forward attendant panel 120RH release the CABIN WDO and CABIN CLG pushbutton switches.
(2) De-energize the aircraft electrical circuits AMM 24-41-00-862-002.