Operational Test of the Commercial Electrical Load Shedding
TASK 24-51-00-710-001-A
Operational Test of the Commercial Electrical Load Shedding
Refer to the MPD TASK: 245100-02
OPERATIONAL CHECK OF COMMERCIAL ELECTRIC LOAD SHEDDING
Make sure that the commercial electrical load shedding is effective
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 24-51-00-861-050-A ** ON A/C NOT FOR ALL Subtask 24-51-00-865-050-A ** ON A/C NOT FOR ALL
Subtask 24-51-00-710-050-A ** ON A/C NOT FOR ALL
Subtask 24-51-00-860-051-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.03.31 23:24:47 UTC
Operational Test of the Commercial Electrical Load Shedding
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 245100-02
OPERATIONAL CHECK OF COMMERCIAL ELECTRIC LOAD SHEDDING
Make sure that the commercial electrical load shedding is effective
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 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 24-51-00-861-050-A ** ON A/C NOT FOR ALL Subtask 24-51-00-865-050-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 24-51-00-860-050-C ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 122VU | ELEC/GALY & CAB/CTL | 1XA | S26 |
| 122VU | ELEC/GALY & CAB/FAULT/LT CTL | 8XA | S25 |
| 122VU | ELEC/GALY & CAB/GND/FLT/LOGIC | 7XA | S24 |
C. Aircraft Maintenance Configuration
(1) In all galley areas, make sure that all the circuit breakers are closed.
(2) On the AC power center 123VU and the rear circuit breaker panel 122VU, make sure that all the circuit breakers related to the galley feeder (xxMC) are closed.
(3) On circuit breaker panel 2000VU, make sure that all the circuit breakers related to the cabin lighting (xxxLG) are closed.
(5) On this panel, make sure that the ELEC/COMMERCIAL pushbutton switch is released (OFF legend on).
(6) On the FWD ATTENDANT panel 120RH, make sure that the pushbutton switches that supply the ceiling and window lights are pushed.
(7) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
4. Procedure(1) In all galley areas, make sure that all the circuit breakers are closed.
(2) On the AC power center 123VU and the rear circuit breaker panel 122VU, make sure that all the circuit breakers related to the galley feeder (xxMC) are closed.
(3) On circuit breaker panel 2000VU, make sure that all the circuit breakers related to the cabin lighting (xxxLG) are closed.
NOTE: The applicable circuit breakers xxMC and xxxLG are related to the different cabin configurations.
(4) On the ELEC panel 35VU, make sure that the GALY & CAB pushbutton switch is pushed (OFF legend off). (5) On this panel, make sure that the ELEC/COMMERCIAL pushbutton switch is released (OFF legend on).
(6) On the FWD ATTENDANT panel 120RH, make sure that the pushbutton switches that supply the ceiling and window lights are pushed.
(7) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
Subtask 24-51-00-710-050-A ** ON A/C NOT FOR ALL
A. Test of the Commercial Electrical Load Shedding
5. Close-up| ACTION | RESULT |
|---|---|
1.On the ECAM control panel:
| On the lower ECAM DU:
|
2.On the electrical panel 35VU:
| On the electrical panel 35VU:
|
| | On the lower ECAM DU:
|
| | In the forward and aft galleys:
If the mid galleys are installed:
|
| | In the passenger cabin:
|
3.On the electrical panel 35VU:
| On the electrical panel 35VU:
|
| | On the lower ECAM DU:
|
| | In the forward and aft galleys:
If the mid galleys are installed:
|
| | In the passenger cabin:
|
Subtask 24-51-00-860-051-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial 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).
(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).