Installation of the Seat Electronic Box (SEB) / Power Ethernet Box (PEB)
TASK 23-33-46-400-001-A
Installation of the Seat Electronic Box (SEB) / Power Ethernet Box (PEB)
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 23-33-46-860-052-O ** ON A/C NOT FOR ALL
Subtask 23-33-46-420-051-A ** ON A/C NOT FOR ALL
Subtask 23-33-46-410-050-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:12:07 UTC
Installation of the Seat Electronic Box (SEB) / Power Ethernet Box (PEB)
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 200 | UPPER HALF FUSELAGE |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 23-33-00-600-802-A | Software / Media Download and Configuration of the IFE system |
| TASK 23-33-00-710-005-A | Operational Test of the Integrated In-Flight Entertainment (IFE) System |
| TASK 23-73-00-861-001-A | Energize the Cabin Intercommunication Data System (CIDS) |
| TASK 23-73-00-862-001-A | De-energize the Cabin Intercommunication Data System (CIDS) |
| 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) |
Subtask 23-33-46-860-052-O ** ON A/C NOT FOR ALL
A. Preparation for Installation
(1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
Subtask 23-33-46-865-063-A ** ON A/C NOT FOR ALL (1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 2000VU | IFE-IFEC-AC | 22MK | C04 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | INSEAT POWER-MCU 2 | 59HP | B08 |
| 2000VU | INSEAT POWER-MCU 1 | 58HP | B05 |
| 2000VU | IFE-VCC-AC | 21MH | C02 |
| 2000VU | IFE-VCC-DC | 20MH | C01 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | IFE-IFEC-AC | 22MK | C06 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | PES-MUSIC - CTL | 21MK | D01 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | PES-VIDEO-CONTROL-VCC-DS/C | 21MH | C02 |
| 2000VU | PES-VIDEO-CONTROL-MAIN | 20MH | C01 |
| 2000VU | PES-MUSIC-CABIN AFT-RH | 25MK | D05 |
| 2000VU | PES-MUSIC-CABIN AFT-LH | 22MK | D04 |
| 2000VU | PES-MUSIC-CABIN FWD-RH | 24MK | D03 |
| 2000VU | PES-MUSIC-CABIN FWD-LH | 23MK | D02 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | PES-MUSIC-CTL | 21MK | D01 |
Subtask 23-33-46-420-051-A ** ON A/C NOT FOR ALL
A. Installation of the Seat Electronic Box (SEB)
(1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Carefully install the SEB (1) and lock the nylatches (3).
(4) Remove the blanking caps from the electrical connectors.
(6) Connect the electrical connectors (4) to the related SEB connectors and fasten with the spring latches (2).
(7) Connect the electrical connector (5) to the related SEB SEAT connector.
Subtask 23-33-46-865-058-A ** ON A/C NOT FOR ALL (1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Carefully install the SEB (1) and lock the nylatches (3).
| NOTE: |
|---|
| 1.At the end of the WDB-SEB-lines the SEB has to be ended with a termination plug. If a related SEB is installed, connect the termination plug to SEB connector J2. |
| 2.The SEB connector J4 is not used on A320. |
CAUTION:
REFER TO THE MATCH MARKS MADE DURING THE REMOVAL WHEN YOU CONNECT THE ELECTRICAL WIRES.
INCORRECT CONNECTION OF THE WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
(5) Make sure that all the electrical connections are clean and in the correct condition.(6) Connect the electrical connectors (4) to the related SEB connectors and fasten with the spring latches (2).
(7) Connect the electrical connector (5) to the related SEB SEAT connector.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 23-33-46-750-050-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 2000VU | IFE-IFEC-AC | 22MK | C04 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | INSEAT POWER-MCU 2 | 59HP | B08 |
| 2000VU | INSEAT POWER-MCU 1 | 58HP | B05 |
| 2000VU | IFE-VCC-AC | 21MH | C02 |
| 2000VU | IFE-VCC-DC | 20MH | C01 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | IFE-IFEC-AC | 22MK | C06 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | PES-MUSIC - CTL | 21MK | D01 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | PES-VIDEO-CONTROL-VCC-DS/C | 21MH | C02 |
| 2000VU | PES-VIDEO-CONTROL-MAIN | 20MH | C01 |
| 2000VU | PES-MUSIC-CABIN AFT-RH | 25MK | D05 |
| 2000VU | PES-MUSIC-CABIN AFT-LH | 22MK | D04 |
| 2000VU | PES-MUSIC-CABIN FWD-RH | 24MK | D03 |
| 2000VU | PES-MUSIC-CABIN FWD-LH | 23MK | D02 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | PES-MUSIC-CTL | 21MK | D01 |
C. Do the software/media download and configuration of the IFE system (Ref. AMM TASK 23-33-00-600-802).
Subtask 23-33-46-860-050-A ** ON A/C NOT FOR ALL D. Preparation for the Test
(1) Make sure that the CIDS is energized (Ref. AMM TASK 23-73-00-861-001).
Subtask 23-33-46-710-051-D ** ON A/C NOT FOR ALL (1) Make sure that the CIDS is energized (Ref. AMM TASK 23-73-00-861-001).
E. Do the Operational Test of the integrated In-Flight Entertainment (IFE) System (Ref. AMM TASK 23-33-00-710-005).
5. Close-upSubtask 23-33-46-410-050-A ** ON A/C NOT FOR ALL
A. Close Access
(1) De-energize the CIDS (Ref. AMM TASK 23-73-00-862-001).
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Install the protective cap (7) with the quick-release fasteners (6).
Subtask 23-33-46-862-050-A ** ON A/C NOT FOR ALL (1) De-energize the CIDS (Ref. AMM TASK 23-73-00-862-001).
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Install the protective cap (7) with the quick-release fasteners (6).
B. Put the aircraft back to the serviceable condition.
(1) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002)
(1) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002)
Seat Electronic Box