Operational Test of the Logo Lights
TASK 33-47-00-710-002-A
Operational Test of the Logo Lights
To make sure that the logo lights operate correctly.
2. Job Set-up Information
A. Referenced Information
3. Job Set-up
Subtask 33-47-00-860-050-A
Subtask 33-47-00-710-050-C
Subtask 33-47-00-860-051-A
[Rev.10 from 2021]
2026.04.01 04:04:06 UTC
Operational Test of the Logo Lights
WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
1. Reason for the JobTo make sure that the logo lights operate correctly.
2. Job Set-up Information
A. Referenced Information
| 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 |
| TASK 31-32-00-860-009-A | Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page |
| TASK 32-00-00-860-001-A | Flight Configuration Precautions with Electrical Power |
| TASK 32-00-00-860-001-A-01 | Flight Configuration Precautions without Electrical Power |
| TASK 32-00-00-860-002-A | Ground Configuration after Flight Configuration with Electrical Power |
| TASK 32-00-00-860-002-A-01 | Ground Configuration after Flight Configuration without Electrical Power |
Subtask 33-47-00-860-050-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Do the procedure of the flight configuration precautions (Ref. AMM TASK 32-00-00-860-001).
(3) Get access to the L/G page on the MCDU (Ref. AMM TASK 31-32-00-860-009).
Subtask 33-47-00-865-051-A (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Do the procedure of the flight configuration precautions (Ref. AMM TASK 32-00-00-860-001).
(3) Get access to the L/G page on the MCDU (Ref. AMM TASK 31-32-00-860-009).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 122VU | LIGHTING/LOGO/L | 2LY | V03 |
| 122VU | LIGHTING/LOGO/R | 1LY | V02 |
| 122VU | LIGHTING/EXT LT/TAXI AND TAKE OFF/CTL | 2LR | W09 |
Subtask 33-47-00-710-050-C
A. Do this test.
5. Close-up| ACTION | RESULT |
|---|---|
| 1.On the overhead panel 25VU: | On the Trimmable Horizontal Stabilizer (THS): |
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| 2.In the cockpit, on the MCDU: | On the MCDU: |
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| On the THS:
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| 3.Put the slat/flap control lever to position '2' to extend the flaps (Ref. AMM TASK 27-50-00-866-008) | On the THS:
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| 4.On the overhead panel 25VU: | On the THS: |
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| 5.Put the slat/flap control lever to position '0' to retract the flaps (Ref. AMM TASK 27-50-00-866-009) | On the THS:
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6.In the cockpit, on the MCDU:
| On the THS:
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| 7.On the overhead panel 25VU: | On the THS: |
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Subtask 33-47-00-860-051-A
A. Put the aircraft back to its initial configuration.
(1) On the MCDU, put the BRT switch to OFF.
(2) Do the procedure of ground configuration after flight configuration (Ref. AMM TASK 32-00-00-860-002).
(3) De- energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(4) Make sure that the work area is clean and clear of tools and other items.
(1) On the MCDU, put the BRT switch to OFF.
(2) Do the procedure of ground configuration after flight configuration (Ref. AMM TASK 32-00-00-860-002).
(3) De- energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(4) Make sure that the work area is clean and clear of tools and other items.