Operational Test of the In-Seat Power-Supply System (PED Power Supply)
TASK 25-21-00-710-002-A
Operational Test of the In-Seat Power-Supply System (PED Power Supply)
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 25-21-00-861-053-A ** ON A/C NOT FOR ALL Subtask 25-21-00-865-065-A ** ON A/C NOT FOR ALL
Subtask 25-21-00-710-053-R ** ON A/C NOT FOR ALL
Subtask 25-21-00-862-053-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 06:05:29 UTC
Operational Test of the In-Seat Power-Supply System (PED Power Supply)
ZONE: 200
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | MULTIMETER - STANDARD |
| No specific | 1 | TOOL-TEST |
| Z289H0010110 | AR | LOAD UNIT-MOBILE,SEAT |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 200 | UPPER HALF FUSELAGE |
| 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 27-50-00-866-008-A | Extension of the Flaps on the Ground |
| TASK 27-50-00-866-008-A-01 | Extension of the Flaps/Slats on the Ground |
| TASK 27-50-00-866-009-A | Retraction of the Flaps on the Ground |
| TASK 27-50-00-866-009-A-01 | Retraction of the Flaps/Slats on the Ground |
Subtask 25-21-00-861-053-A ** ON A/C NOT FOR ALL Subtask 25-21-00-865-065-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 2000VU | IFE/SEAT-POWER-PAX SYS | 20MK | D08 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | INSEAT POWER-MCU 2 | 59HP | B08 |
| 2000VU | INSEAT POWER-MCU 1 | 58HP | B05 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | SEAT POWER-MCU 2 | 59HP | B08 |
| 2000VU | SEAT POWER-MCU 1 | 58HP | B05 |
Subtask 25-21-00-710-053-R ** ON A/C NOT FOR ALL
A. Operational Test of the PED Power Supply
(1) Make sure that the flaps are fully retracted (Ref. AMM TASK 27-50-00-866-009).
(2) Do this test:
(3) Put the aircraft back to its initial configuration.
(4) Make sure that the work area is clean and clear of tools and other items.
Subtask 25-21-00-710-053-AU ** ON A/C NOT FOR ALL (1) Make sure that the flaps are fully retracted (Ref. AMM TASK 27-50-00-866-009).
(2) Do this test:
NOTE: The extension of the flaps/slats is only necessary after a MCU is replaced.
| ACTION | RESULT |
|---|---|
1.On Flight Attendant Panel (FAP) 120RH:
| At the PED power outlet unit:
|
2.On the related seat:
| At the PED power outlet unit:
|
3.On FAP 120RH:
| At the PED power outlet unit:
|
4.On the related seat:
| |
5.On FAP 120RH:
| On the related seat:
|
| 6.Extend the flaps/slats (Ref. AMM TASK 27-50-00-866-008). | On the related seat:
|
(4) Make sure that the work area is clean and clear of tools and other items.
A. Operational Test of the Portable Electronic Device (PED) Power Supply
(1) Make sure that the PAX SYS ON/OFF switch in the VCC is in the ON position.
(2) Do this test:
(3) Make sure that the work area is clean and clear of tools and other items.
Subtask 25-21-00-710-053-OA ** ON A/C NOT FOR ALL (1) Make sure that the PAX SYS ON/OFF switch in the VCC is in the ON position.
(2) Do this test:
| ACTION | RESULT |
|---|---|
1.On Flight Attendant Panel (FAP) 120RH:
| At the related outlet unit:
|
2.On the related seat:
| At the related power outlet unit:
|
3.On FAP 120RH:
| At the related power outlet unit:
|
4.On the related seat:
| |
A. Operational Test of the Portable Electronic Device (PED) Power Supply
(1) On Flight Attendant Panel (FAP) 120RH, make sure that the PED POWER switch is in the off position.
(2) On FAP 120RH, make sure that the PED POWER switch indicator-light is in amber.
(3) Make sure that the flaps/slats are fully retracted (Ref. AMM TASK 27-50-00-866-009).
(4) Do this test:
(5) Put the aircraft back to its initial configuration.
(6) Make sure that the work area is clean and clear of tools and other items.
5. Close-up(1) On Flight Attendant Panel (FAP) 120RH, make sure that the PED POWER switch is in the off position.
(2) On FAP 120RH, make sure that the PED POWER switch indicator-light is in amber.
(3) Make sure that the flaps/slats are fully retracted (Ref. AMM TASK 27-50-00-866-009).
(4) Do this test:
NOTE: The extension of the flaps/slats is only necessary after the Master Control Unit (MCU) is replaced.
| ACTION | RESULT |
|---|---|
| 1.On FAP 120RH, push the PED POWER switch to the on position. | On FAP 120RH, the PED POWER switch indicator-light changes from amber to green. On the related seat:
|
2.On the related seat:
| On the related seat:
|
| 3.On FAP 120RH, push the PED POWER switch to the off position. | On FAP 120RH, the PED POWER switch indicator-light changes from green to amber. On the related seat:
|
| 4.On the related seat, disconnect the interface cable from the related power outlet unit. | |
| 5.On FAP 120RH, push the PED POWER switch to the on position. | On FAP 120RH, the PED POWER switch indicator-light changes from amber to green. On the related seat:
|
| 6.Extend the flaps/slats (Ref. AMM TASK 27-50-00-866-008). | On FAP 120RH, the PED POWER switch indicator-light changes from green to amber. On the related seat:
|
(6) Make sure that the work area is clean and clear of tools and other items.
Subtask 25-21-00-862-053-A ** ON A/C NOT FOR ALL