Installation of the Cabin LED Unit (CLEDU)/Mini Cabin LED Unit (mCLEDU)
TASK 33-21-11-400-802-A
Installation of the Cabin LED Unit (CLEDU)/Mini Cabin LED Unit (mCLEDU)
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 33-21-11-860-057-A ** ON A/C NOT FOR ALL
Subtask 33-21-11-910-052-A ** ON A/C NOT FOR ALL
Subtask 33-21-11-410-054-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 06:07:39 UTC
Installation of the Cabin LED Unit (CLEDU)/Mini Cabin LED Unit (mCLEDU)
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | STEPLADDER 1.0 M (3.3 FT) |
| No specific | AR | TIE WRAP(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.05TFB2) | Adhesive Tape-Hook Loop Flame Retardant Hook |
| (Material No.05TFB4) | Adhesive Tape-Hook Loop Flame Retardant Loop |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 220 | FWD CAB UTILITY AREAS |
| 230 | FWD PASSENGER COMPARTMENT |
| 240 | MID PASSENGER COMPARTMENT |
| 250 | AFT PASSENGER COMPARTMENT |
| 260 | AFT CABIN UTILITY AREA |
| 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 25-23-41-000-001-A | Removal of the Ceiling Panels |
| TASK 25-23-41-400-001-A | Installation of the Ceiling Panels |
| TASK 25-23-48-000-001-A | Removal of the Cove Light Panel |
| TASK 25-23-48-400-001-A | Installation of the Cove Light Panel |
Subtask 33-21-11-860-057-A ** ON A/C NOT FOR ALL
A. Get Access
(1) For the ceiling Cabin LED Unit (CLEDU):
Subtask 33-21-11-860-057-E ** ON A/C NOT FOR ALL (1) For the ceiling Cabin LED Unit (CLEDU):
- Make sure that the STEPLADDER 1.0 M (3.3 FT) is available.
- Make sure that the related ceiling panel is removed (Ref. AMM TASK 25-23-41-000-001).
- Make sure that the related cove light panel is removed (Ref. AMM TASK 25-23-48-000-001).
A. Get Access
(1) For the ceiling CLEDU:
Subtask 33-21-11-865-062-A ** ON A/C NOT FOR ALL (1) For the ceiling CLEDU:
- Make sure that the STEPLADDER 1.0 M (3.3 FT) is in the position.
- Make sure that the related ceiling panel is removed (Ref. AMM TASK 25-23-41-000-001).
- Make sure that the STEPLADDER 1.0 M (3.3 FT) is in the position.
- Make sure that the related cover light panel is removed (Ref. AMM TASK 25-23-48-000-001).
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 | CAB LIGHT PWR-CEILING-AFT | 307LG | H08 |
| 2000VU | CAB LIGHT PWR-CEILING-AFT | 304LG | H07 |
| 2000VU | CAB LIGHT PWR-CEILING-FWD | 306LG | H06 |
| 2000VU | CAB LIGHT PWR-CEILING-FWD | 305LG | H05 |
| 2000VU | CAB LIGHT PWR-WINDOW-AFT | 302LG | H04 |
| 2000VU | CAB LIGHT PWR-WINDOW-AFT | 301LG | H03 |
| 2000VU | CAB LIGHT PWR-WINDOW-FWD | 303LG | H02 |
| 2000VU | CAB LIGHT PWR-WINDOW-FWD | 300LG | H01 |
| 2000VU | LIGHT-CABIN-ENTRY | 308LG | J02 |
Subtask 33-21-11-910-052-A ** ON A/C NOT FOR ALL
A. Preparation for Installation
(1) Make sure that the parts retained from the removed component are clean and in the correct condition.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Clean the component interfaces and the adjacent area.
Subtask 33-21-11-420-052-A ** ON A/C NOT FOR ALL (1) Make sure that the parts retained from the removed component are clean and in the correct condition.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Clean the component interfaces and the adjacent area.
B. Installation of the CLEDU
(2) Remove the CAP-BLANKING from each electrical connector and receptacle.
(4) If necessary attach the electrical wire with TIE WRAP(S).
Subtask 33-21-11-420-052-D ** ON A/C NOT FOR ALL CAUTION:
DO NOT TOUCH THE LAMP GLASS WITH YOUR FINGERS.
THE OILS FROM YOUR SKIN WILL QUICKLY CAUSE DETERIORATION OF THE LAMP.
IF YOU ACCIDENTALLY TOUCH THE LAMP GLASS, CLEAN IT WITH A LINT-FREE CLOTH.
(1) Put the CLEDU (1) in the correct position on the aircraft structure and engage the brackets (3). (2) Remove the CAP-BLANKING from each electrical connector and receptacle.
WARNING:
WHEN YOU CONNECT/DISCONNECT THE CLEDU ELECTRICAL CONNECTORS, YOU MUST PUSH THE BUTTON ON THE ELECTRICAL CONNECTORS TO CONNECT/DISCONNECT THEM. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT CAN OCCUR.
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.
CAUTION:
MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
(3) Connect the electrical connector (2). (4) If necessary attach the electrical wire with TIE WRAP(S).
B. Installation of the CLEDU/mCLEDU
(a) Put the CLEDU (1) in the correct position on the aircraft structure and engage the brackets (3).
(b) Remove the CAP-BLANKING from each electrical connector and receptacle.
(d) If necessary, attach the electrical wires with the TIE WRAP(S).
(2) For mCLEDU:
(a) Put the mCLEDU (4) in the correct position on the aircraft structure and engage the brackets (6).
(b) Remove the CAP-BLANKING from each electrical connector and receptacle.
(d) If necessary, attach the electrical wires with the TIE WRAP(S).
Subtask 33-21-11-865-063-A ** ON A/C NOT FOR ALL WARNING:
WHEN YOU CONNECT/DISCONNECT THE CLEDU ELECTRICAL CONNECTORS, YOU MUST PUSH THE BUTTON ON THE ELECTRICAL CONNECTORS TO CONNECT/DISCONNECT THEM. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT CAN OCCUR.
CAUTION:
DO NOT TOUCH THE LAMP GLASS WITH YOUR FINGERS.
THE OILS FROM YOUR SKIN WILL QUICKLY CAUSE DETERIORATION OF THE LAMP.
IF YOU ACCIDENTALLY TOUCH THE LAMP GLASS, CLEAN IT WITH A LINT-FREE CLOTH.
(1) For CLEDU: (a) Put the CLEDU (1) in the correct position on the aircraft structure and engage the brackets (3).
(b) Remove the CAP-BLANKING from each electrical connector and receptacle.
CAUTION:
MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
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.
(c) Connect the electrical connector (2). (d) If necessary, attach the electrical wires with the TIE WRAP(S).
(2) For mCLEDU:
(a) Put the mCLEDU (4) in the correct position on the aircraft structure and engage the brackets (6).
(b) Remove the CAP-BLANKING from each electrical connector and receptacle.
CAUTION:
MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
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.
(c) Connect the electrical connector (5). (d) If necessary, attach the electrical wires with the TIE WRAP(S).
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 33-21-11-860-056-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 2000VU | CAB LIGHT PWR-CEILING-AFT | 307LG | H08 |
| 2000VU | CAB LIGHT PWR-CEILING-AFT | 304LG | H07 |
| 2000VU | CAB LIGHT PWR-CEILING-FWD | 306LG | H06 |
| 2000VU | CAB LIGHT PWR-CEILING-FWD | 305LG | H05 |
| 2000VU | CAB LIGHT PWR-WINDOW-AFT | 302LG | H04 |
| 2000VU | CAB LIGHT PWR-WINDOW-AFT | 301LG | H03 |
| 2000VU | CAB LIGHT PWR-WINDOW-FWD | 303LG | H02 |
| 2000VU | CAB LIGHT PWR-WINDOW-FWD | 300LG | H01 |
| 2000VU | LIGHT-CABIN-ENTRY | 308LG | J02 |
D. Preparation for the Test
(1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the cockpit door is closed and the engines are stopped.
(3) Push the LIGHT MAIN ON/OFF membrane switch on the Flight Attendant Panel (FAP) 120RH.
(4) Make sure that the indications on all of the BRT, DIM1, DIM2, WDO and CLG buttons on FAP 120RH are off.
Subtask 33-21-11-710-053-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).
(2) Make sure that the cockpit door is closed and the engines are stopped.
(3) Push the LIGHT MAIN ON/OFF membrane switch on the Flight Attendant Panel (FAP) 120RH.
(4) Make sure that the indications on all of the BRT, DIM1, DIM2, WDO and CLG buttons on FAP 120RH are off.
E. Operational Test
(1) Do this test of the entrance-Lights, window-lights and ceiling-lights:
5. Close-up(1) Do this test of the entrance-Lights, window-lights and ceiling-lights:
| ACTION | RESULT |
|---|---|
| 1.For the entrance lighting: | |
| On Flight Attendant Panel (FAP) 120RH: | On FAP 120RH: |
|
|
|
|
| | In the cabin:
|
| | On FAP 120RH: |
|
|
| | In the cabin:
|
| | On FAP 120RH: |
|
|
| | In the cabin:
|
| | On FAP 120RH: |
|
|
| | In the cabin:
|
| 2.For the window or ceiling lighting: | |
| On FAP 120RH: | On FAP 120RH: |
|
|
| | In the cabin:
|
| | On FAP 120RH: |
|
|
| | In the cabin:
|
| | On FAP 120RH: |
|
|
| | In the cabin:
|
| | On FAP 120RH: |
|
|
| | In the cabin:
|
Subtask 33-21-11-410-054-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) For the ceiling CLEDU:
Subtask 33-21-11-410-054-E ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) For the ceiling CLEDU:
- Install the related ceiling panel (Ref. AMM TASK 25-23-41-400-001).
- Install the related cove light panel (Ref. AMM TASK 25-23-48-400-001).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) For the ceiling CLEDU:
(a) Install the related ceiling panel (Ref. AMM TASK 25-23-41-400-001).
(3) For the ceiling mCLEDU:
(a) 1 Clean the component interface and/or the adjacent area of the upper mCLEDU cover (1) and on the top of the OHSC (3) with Non Aqueous Cleaner-General - - (Material No.08BAA9) and a Textile-Lint free Cotton - (Material No.14SBA1) .
2 Put a Adhesive Tape-Hook Loop Flame Retardant Hook (Material No.05TFB2) and a Adhesive Tape-Hook Loop Flame Retardant Loop (Material No.05TFB4) (2) on the upper mCLEDU cover (1) and the top of the OHSC (3).
3 Install the upper mCLEDU cover (1) on the top of the OHSC (3) in its position and lightly push it.
(4) For the window mCLEDU:
Subtask 33-21-11-862-053-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) For the ceiling CLEDU:
(a) Install the related ceiling panel (Ref. AMM TASK 25-23-41-400-001).
(3) For the ceiling mCLEDU:
(a) 1 Clean the component interface and/or the adjacent area of the upper mCLEDU cover (1) and on the top of the OHSC (3) with Non Aqueous Cleaner-General - - (Material No.08BAA9) and a Textile-Lint free Cotton - (Material No.14SBA1) .
2 Put a Adhesive Tape-Hook Loop Flame Retardant Hook (Material No.05TFB2) and a Adhesive Tape-Hook Loop Flame Retardant Loop (Material No.05TFB4) (2) on the upper mCLEDU cover (1) and the top of the OHSC (3).
3 Install the upper mCLEDU cover (1) on the top of the OHSC (3) in its position and lightly push it.
(4) For the window mCLEDU:
- Install the related cover light panel (Ref. AMM TASK 25-23-48-400-001).
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).
Upper mCLEDU Cover