Operational Test of the Battery Charge Limiter (BCL), (with the CFDS)
TASK 24-38-00-710-001-A
Operational Test of the Battery Charge Limiter (BCL), (with the CFDS)
Refer to the MPD TASK: 243800-01
OPERATIONAL CHECK OF BATTERY CHARGE LIMITER NO 1 AND NO 2 VIA CFDS
Operational test of the BITE function of the BCL. Make sure that the FAULT legends of the BAT pushbutton switches and the RAT & EMER GEN annunciator come on.
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 24-38-00-860-051-A
Subtask 24-38-00-710-050-A
Subtask 24-38-00-410-051-A
[Rev.10 from 2021]
2026.03.31 23:23:49 UTC
Operational Test of the Battery Charge Limiter (BCL), (with the CFDS)
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 243800-01
OPERATIONAL CHECK OF BATTERY CHARGE LIMITER NO 1 AND NO 2 VIA CFDS
Operational test of the BITE function of the BCL. Make sure that the FAULT legends of the BAT pushbutton switches and the RAT & EMER GEN annunciator come on.
NOTE: If the CFDS is not available, there is an alternative method for this procedure. This task gives the first method. For the alternative method, refer to the other task in this page block.
2. Job Set-up InformationA. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 812, 822 |
| 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 31-32-00-860-004-A | Procedure to Get Access to the SYSTEM REPORT/TEST/ELEC Page |
Subtask 24-38-00-860-051-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) In the cockpit, on the overhead panel 35VU, make sure that the BAT 1 and BAT 2 pushbutton switches are released. (On these pushbutton switches, the OFF legend is on).
(3) On the MCDU, on the SYSTEM REPORT/TEST page, get the ELEC menu (Ref. AMM TASK 31-32-00-860-004).
Subtask 24-38-00-010-051-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) In the cockpit, on the overhead panel 35VU, make sure that the BAT 1 and BAT 2 pushbutton switches are released. (On these pushbutton switches, the OFF legend is on).
(3) On the MCDU, on the SYSTEM REPORT/TEST page, get the ELEC menu (Ref. AMM TASK 31-32-00-860-004).
B. Get access to the avionics compartment.
(1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE at the avionics compartment doors 812 and 822.
(2) Open the access doors 812 and 822.
(3) Open the access panels of the AC/DC emergency power center 106VU and BATTERY power center 105VU.
Subtask 24-38-00-865-050-A (1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE at the avionics compartment doors 812 and 822.
(2) Open the access doors 812 and 822.
(3) Open the access panels of the AC/DC emergency power center 106VU and BATTERY power center 105VU.
C. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 105VU | ELEC/HOT BUS/702PP SPLY | 5PB2 | D02 |
| 105VU | ELEC/HOT BUS/701PP SPLY | 5PB1 | D01 |
| 105VU | ELEC/BAT REF/BCL2 | 9PB2 | F02 |
| 105VU | ELEC/BAT REF/BCL1 | 9PB1 | F01 |
| 105VU | ELEC/BAT BUS/REF/BCL1 | 8PB1 | G01 |
| 105VU | ELEC/BAT BUS/REF/BCL2 | 8PB2 | J02 |
| 106VU | CSM/G /EV/MAN/SPLY | 6XE | B04 |
| 125VU | BAT BUS/301PP/SPLY | 11PB | CC01 |
Subtask 24-38-00-710-050-A
A. Operational Test of the BCL (with the CFDS)
5. Close-up| ACTION | RESULT |
|---|---|
1.On the panel 35VU:
| On the panel 35VU:
|
2.On the MCDU, on the ELEC page:
| On the MCDU:
|
3.On the BCL page:
| On the panel 35VU:
|
| | On the panel 21VU:
|
| | On the BCL page:
|
4.On the MCDU:
| |
5.On the panel 35VU:
| On the panel 35VU:
|
6.On the MCDU, on the ELEC page:
| On the MCDU:
|
7.On the BCL page:
| On the panel 35VU:
|
| | On the panel 21VU:
|
| | On the BCL page:
|
8.On the panel 35VU:
| On the panel 35VU:
|
Subtask 24-38-00-410-051-A
A. Close Access
(1) Close the access panels of the AC/DC emergency power center 106VU and BATTERY power center 105VU.
(2) Close the access doors 812 and 822.
(3) Remove the access platform(s).
Subtask 24-38-00-860-050-A (1) Close the access panels of the AC/DC emergency power center 106VU and BATTERY power center 105VU.
(2) Close the access doors 812 and 822.
(3) Remove the access platform(s).
B. Put the aircraft back to its initial configuration.
(1) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).