Operational Test of the Cabin Signs
TASK 23-73-00-710-017-A
Operational Test of the Cabin Signs
This procedure gives the instructions necessary to make sure that the cabin signs operate correctly.
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 23-73-00-860-091-C ** ON A/C NOT FOR ALL
Subtask 23-73-00-710-291-C ** ON A/C NOT FOR ALL
Subtask 23-73-00-710-221-L ** ON A/C NOT FOR ALL
Subtask 23-73-00-710-221-V ** ON A/C NOT FOR ALL
Subtask 23-73-00-865-098-A
[Rev.10 from 2021]
2026.03.31 23:17:21 UTC
Operational Test of the Cabin Signs
ZONE: 200
1. Reason for the JobThis procedure gives the instructions necessary to make sure that the cabin signs operate correctly.
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 200 | UPPER HALF FUSELAGE |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 21-31-34-000-001-A | Removal of the Cabin Pressure Controller (CPC) |
| TASK 21-31-34-400-001-A | Installation of the Cabin Pressure Controller (CPC) |
| TASK 23-73-00-860-002-A | Cabin Layout Selection |
| TASK 23-73-00-860-003-A | Cabin Zones Programming |
| TASK 23-73-00-860-006-A | Programming of a NON SMOKER A/C |
| TASK 23-73-00-860-008-A | Cabin Zones Programming |
| TASK 23-73-00-861-001-A | 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) |
| 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 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| 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 23-73-00-860-091-C ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the NO SMOKING switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(6) Make sure that the A/C is not in a NON SMOKER configuration and a NO SMOKING area is not programmed
(Ref. AMM TASK 23-73-00-860-003).
(Ref. AMM TASK 21-31-34-000-001).
Subtask 23-73-00-860-091-G ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the NO SMOKING switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(6) Make sure that the A/C is not in a NON SMOKER configuration and a NO SMOKING area is not programmed
(Ref. AMM TASK 23-73-00-860-003).
NOTE: The Non Smoker Section (NSS) signs come on together with the No Smoking (NS) signs.
(7) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment (Ref. AMM TASK 21-31-34-000-001).
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the slats are fully retracted to lever 0 position.
(Ref. AMM TASK 27-50-00-866-009).
(6) Make sure that the NO SMOKING switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(7) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
Subtask 23-73-00-860-091-K ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the slats are fully retracted to lever 0 position.
(Ref. AMM TASK 27-50-00-866-009).
(6) Make sure that the NO SMOKING switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(7) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the NO SMOKING switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(6) Make sure that the A/C is not in a NON SMOKER configuration and a NO SMOKING area is not programmed
(Ref. AMM TASK 23-73-00-860-008).
(Ref. AMM TASK 21-31-34-000-001).
Subtask 23-73-00-860-091-N ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the NO SMOKING switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(6) Make sure that the A/C is not in a NON SMOKER configuration and a NO SMOKING area is not programmed
(Ref. AMM TASK 23-73-00-860-008).
NOTE: This step is applicable only if CAM configuration allows you to change NON SMOKER A/C configuration or NO SMOKING area on the "CABIN PROGRAMMING" page on the FAP.
(7) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment (Ref. AMM TASK 21-31-34-000-001).
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the EXIT switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(6) Make sure that the EMER EXIT LT switch 4WL on the cockpit overhead panel 25VU is in the ARM position.
(7) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
Subtask 23-73-00-860-091-R ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the EXIT switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(6) Make sure that the EMER EXIT LT switch 4WL on the cockpit overhead panel 25VU is in the ARM position.
(7) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the slats are fully retracted to lever 0 position
(Ref. AMM TASK 27-50-00-866-009).
(6) Make sure that the NO SMOKING switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(7) Make sure that the A/C is not in a NON SMOKER configuration and a NO SMOKING area is not programmed
(Ref. AMM TASK 23-73-00-860-008).
(8) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
Subtask 23-73-00-860-091-T ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the slats are fully retracted to lever 0 position
(Ref. AMM TASK 27-50-00-866-009).
(6) Make sure that the NO SMOKING switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(7) Make sure that the A/C is not in a NON SMOKER configuration and a NO SMOKING area is not programmed
(Ref. AMM TASK 23-73-00-860-008).
(8) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the slats are fully retracted to lever 0 position
(Ref. AMM TASK 27-50-00-866-009).
(6) Make sure that the NO PORTABLE ELEC DEVICE switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(7) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
Subtask 23-73-00-860-091-X ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the slats are fully retracted to lever 0 position
(Ref. AMM TASK 27-50-00-866-009).
(6) Make sure that the NO PORTABLE ELEC DEVICE switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(7) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the NO PORTABLE ELEC DEVICE switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(6) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
Subtask 23-73-00-865-091-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Do the procedure of flight configuration precaution
(Ref. AMM TASK 32-00-00-860-001).
(5) Make sure that the NO PORTABLE ELEC DEVICE switch 190RH and the SEAT BELTS switch 191RH on the cockpit overhead panel 25VU are in the OFF position.
(6) Get access to the Cabin Pressure Controller 11HL and 12HL in the avionics compartment
(Ref. AMM TASK 21-31-34-000-001).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 23-73-00-865-097-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| 49VU | FWS/FWC1/SPLY | 3WW | F01 |
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | EIS/FWC2/SPLY | 2WW | Q07 |
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | AIR COND/CAB/PRESS/CTL1 | 1HL | D09 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
| ** ON A/C ALL | |||
| 122VU | AIR COND/CAB PRESS/CTL/MAN | 3HL | Y23 |
| 122VU | AIR COND/CAB PRESS/CTL/2 | 2HL | Y22 |
Subtask 23-73-00-710-291-C ** ON A/C NOT FOR ALL
A. Test of the Passenger Lighted Signs
Subtask 23-73-00-710-291-S ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO SMOKING and SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on the overhead panel 25VU: | In the cabin: |
|
|
| |
|
| |
|
| | In all lavatories: |
| |
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
A. Test of the Passenger Lighted Signs
Subtask 23-73-00-710-291-T ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: If a Non Smoker A/C has been programmed, the NS signs will remain on.
NOTE: The deactivation of a Non Smoker A/C on the FAP will lead to the deactivation of the NS signs in the attendant areas when there are no seatrows configured as a smoker zones.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on the overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | |
| | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
A. Test of the Passenger Lighted Signs
Subtask 23-73-00-710-291-A0 ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: The No Smoking (NS) signs in the cabin stay permanently on.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on the overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | |
| | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
A. Test of the Passenger Lighted Signs
Subtask 23-73-00-710-291-AE ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO SMOKING and SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: If a Non Smoker A/C has been programmed, the NS signs will remain on.
NOTE: The deactivation of a Non Smoker A/C on the FAP will lead to the deactivation of the NS signs in the attendant areas when there are no seatrows configured as a smoker zones.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| |
|
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | |
| | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit on the ECAM upper display unit: |
| |
|
A. Test of the Passenger Lighted Signs
Subtask 23-73-00-710-221-A ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO PORTABLE DEVICES and SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| |
|
| | In all lavatories: |
| |
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| |
|
| | In the cockpit on the ECAM upper display unit: |
| |
|
CAUTION:
BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING.
B. Test of the Passenger Lighted Signs automatic-function if the landing gear is extended NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO SMOKING message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on the overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 2.In the cockpit, on the circuit breaker panel 49VU: | |
| CAUTION : BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING. | |
| |
| 3.In the cockpit, on the circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the cockpit, on the circuit breaker panel 49VU: | |
| |
| 5.In the cockpit, on the circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 6.In the cockpit, on the overhead panel 25VU: | |
| | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
CAUTION:
BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING.
B. Test of the Passenger Lighted Signs automatic-function if the landing gear is extended NOTE: The No Smoking (NS) signs in the cabin stay permanently on.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on the overhead panel 25VU: | In the cabin: |
|
|
| |
|
| 2.In the cockpit, on the circuit breaker panel 49VU: | |
| CAUTION : BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING. | |
| |
| 3.In the cockpit, on the circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| 4.In the cockpit, on the circuit breaker panel 49VU: | |
| |
| 5.In the cockpit, on the circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| 6.In the cockpit, on the overhead panel 25VU: | In the cabin: |
|
|
| |
|
B. Test of the Passenger Lighted Signs automatic-function if the landing gear is extended
Subtask 23-73-00-710-221-W ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO SMOKING and SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: If a Non Smoker A/C has been programmed, the NS signs will remain on.
NOTE: The deactivation of a Non Smoker A/C on the FAP will lead to the deactivation of the NS signs in the attendant areas when there are no seatrows configured as a smoker zones.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| In the cabin: |
| |
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 2.In the cockpit, on circuit breaker panel 49VU: | |
CAUTION:
BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING.
| |
| 3.In the cockpit, on circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| |
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the cockpit, on circuit breaker panel 49VU: | |
| |
| 5.In the cockpit, on circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| |
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 6.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| In the cabin: |
| |
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
B. Test of the Passenger Lighted Signs Automatic-Function if the Landing Gear is Extended
Subtask 23-73-00-710-221-AC ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the "NO SMOKING" message on the ECAM upper display unit. Therefore circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: If a Non Smoker A/C has been programmed, the NS signs will remain on.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 2.In the cockpit, on circuit breaker panel 49VU: | |
CAUTION:
BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING.
| |
| 3.In the cockpit, on circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the cockpit, on circuit breaker panel 49VU and 121VU: | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 5.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
B. Test of the Passenger Lighted Signs automatic-function if the landing gear is extended
Subtask 23-73-00-710-225-B ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO PORTABLE DEVICES and SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 2.In the cockpit, on circuit breaker panel 49VU: | |
CAUTION:
BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING.
| |
| 3.In the cockpit, on circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the cockpit, on circuit breaker panel 49VU: | |
| |
| 5.In the cockpit, on circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 6.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
C. Test of the Passenger Lighted Signs automatic-function if a cabin-decompression occurs
Subtask 23-73-00-710-225-R ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO SMOKING and SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
| ACTION | RESULT |
|---|---|
| 1.In the avionics compartment: | |
| |
| 2.In the avionics compartment, on the rack 95VU: | In the cabin: |
|
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 3.In the avionics compartment, on the rack 96VU: | In the cabin: |
|
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the avionics compartment: | |
| |
C. Test of the Passenger Lighted Signs automatic-function if a cabin-decompression occurs
Subtask 23-73-00-710-225-T ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: The No Smoking (NS) signs in the cabin stay permanently on.
| ACTION | RESULT |
|---|---|
| 1.In the avionics compartment: | |
| |
| 2.In the avionics compartment, on the rack 95VU: | In the cabin: |
|
|
| |
|
| | At all entry areas: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | At all entry areas: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 3.In the avionics compartment, on the rack 96VU: | In the cabin: |
|
|
| |
|
| | At all entry areas: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | At all entry areas: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the avionics compartment: | |
| |
C. Test of the Passenger Lighted Signs automatic-function if a cabin decompression occurs.
Subtask 23-73-00-710-225-Z ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: The No Smoking (NS) signs in the cabin stay permanently on.
| ACTION | RESULT |
|---|---|
| 1.In the avionics compartment: | |
| |
| 2.In the avionics compartment, on the rack 95VU: | In the cabin: |
|
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 3.In the avionics compartment, on the rack 96VU: | In the cabin: |
|
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the avionics compartment: | |
| |
C. Test of the Passenger Lighted Signs Automatic-Function if a Cabin-Decompression Occurs
Subtask 23-73-00-710-225-AB ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the "NO SMOKING" and "SEAT BELTS" messages on the ECAM upper display unit. Therefore circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: If a Non Smoker A/C has been programmed, the NS signs will remain on.
NOTE: The deactivation of a Non Smoker A/C on the FAP will lead to the deactivation of the NS signs in the attendant areas when there are no seatrows configured as a smoker zones.
| ACTION | RESULT |
|---|---|
| 1.In the avionics compartment: | |
| |
| 2.In the avionics compartment, on rack 95VU: | In the cabin: |
|
|
| |
|
| |
|
| |
|
| | |
| | At all entry areas: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| |
|
| |
|
| | |
| | At all entry areas: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 3.In the avionics compartment, on rack 96VU: | In the cabin: |
|
|
| |
|
| |
|
| |
|
| | |
| | At all entry areas: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| |
|
| |
|
| | |
| | At all entry areas: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the avionics compartment: | |
| |
C. Test of the Passenger Lighted Signs automatic-function if a cabin-decompression occurs
Subtask 23-73-00-710-226-G ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO PORTABLE DEVICES and SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
| ACTION | RESULT |
|---|---|
| 1.In the avionics compartment: | |
| |
| 2.In the avionics compartment, on rack 95VU: | In the cabin: |
|
|
| |
|
| | At all entry areas: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | At all entry areas: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 3.In the avionics compartment, on rack 96VU: | In the cabin: |
|
|
| |
|
| | At all entry areas: |
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | At all entry areas: |
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the avionics compartment: | |
| |
D. Test of the Passenger Lighted Signs automatic-function if the slats are extended
Subtask 23-73-00-710-226-M ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on the overhead panel 25VU: | |
| |
| 2.In the cockpit, on the pedestal panel 114VU: | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| | In the cabin: |
|
|
| |
|
| | In all lavatories: |
| |
|
| |
|
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 3.In the cockpit, on the overhead panel 25VU: | |
| |
D. Test of the Passenger Lighted Signs automatic-function if the slats are extended
Subtask 23-73-00-710-226-O ** ON A/C NOT FOR ALL NOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
NOTE: If a Non Smoker A/C has been programmed, the NS signs will remain on.
NOTE: The deactivation of a Non Smoker A/C on the FAP will lead to the deactivation of the NS signs in the attendant areas when there are no seatrows configured as a smoker zones.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 2.In the cockpit, on circuit breaker panel 49VU: | |
CAUTION:
BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING.
| |
| 3.In the cockpit, on circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the cockpit, on pedestal panel 114VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, at the ECAM upper display unit: |
| |
|
| | |
| | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 5.In the cockpit, on circuit breaker panel 49VU: | |
| |
| 6.In the cockpit, on circuit breaker panel 121VU: | |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 7.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
D. Test of the Passenger Lighted Signs automatic-function if the slats are extended
5. Close-upNOTE: All ECAM warnings have to be cleared by pushing the CLR pushbutton switch on the ECAM control panel to indicate the NO PORTABLE DEVICE and SEAT BELTS message on the ECAM upper display unit. Therefore the circuit breakers 2WW and 3WW have to stay closed through the whole test.
| ACTION | RESULT |
|---|---|
| 1.In the cockpit, on overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 2.In the cockpit, on circuit breaker panel 49VU: | |
CAUTION:
BEFORE YOU DO THE STEP THAT FOLLOWS, MAKE SURE THAT YOU OBEYED THE FLIGHT CONFIGURATION PRECAUTIONS. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU WILL CAUSE DAMAGE TO THE ANTI-ICE HEATING.
| |
| 3.In the cockpit, on circuit breaker panel 121VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 4.In the cockpit, on pedestal panel 114VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, at the ECAM upper display unit: |
| |
|
| | |
| | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 5.In the cockpit, on circuit breaker panel 49VU: | |
| |
| 6.In the cockpit, on circuit breaker panel 121VU: | |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
| 7.In the cockpit, on the overhead panel 25VU: | In the cabin: |
|
|
| |
|
| | |
| | In all lavatories: |
| |
|
| |
|
| | |
| | In the cockpit, on the ECAM upper display unit: |
| |
|
Subtask 23-73-00-865-098-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 23-73-00-860-092-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | AIR COND/CAB/PRESS/CTL1 | 1HL | D09 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
| ** ON A/C ALL | |||
| 122VU | AIR COND/CAB PRESS/CTL/MAN | 3HL | Y23 |
| 122VU | AIR COND/CAB PRESS/CTL/2 | 2HL | Y22 |
B. Put the aircraft back to its initial configuration.
(1) Do the procedure of ground configuration after flight configuration.
(Ref. AMM TASK 32-00-00-860-002)
(2) Make sure that the required cabin layout is selected in the CAM.
(Ref. AMM TASK 23-73-00-860-002)
(3) Make sure that the initial aircraft cabin configuration is programmed.
(Ref. AMM TASK 23-73-00-860-003)
(Ref. AMM TASK 23-73-00-860-006)
(4) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
Subtask 23-73-00-860-092-B ** ON A/C NOT FOR ALL (1) Do the procedure of ground configuration after flight configuration.
(Ref. AMM TASK 32-00-00-860-002)
(2) Make sure that the required cabin layout is selected in the CAM.
(Ref. AMM TASK 23-73-00-860-002)
(3) Make sure that the initial aircraft cabin configuration is programmed.
(Ref. AMM TASK 23-73-00-860-003)
(Ref. AMM TASK 23-73-00-860-006)
(4) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
B. Put the aircraft back to its initial configuration.
(1) Do the procedure of ground configuration after flight configuration.
(Ref. AMM TASK 32-00-00-860-002)
(2) Make sure that the slats are fully retracted to lever 0 position.
(Ref. AMM TASK 27-50-00-866-009)
(3) Make sure that the required cabin layout is selected in the CAM.
(Ref. AMM TASK 23-73-00-860-002)
(4) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
Subtask 23-73-00-860-092-C ** ON A/C NOT FOR ALL (1) Do the procedure of ground configuration after flight configuration.
(Ref. AMM TASK 32-00-00-860-002)
(2) Make sure that the slats are fully retracted to lever 0 position.
(Ref. AMM TASK 27-50-00-866-009)
(3) Make sure that the required cabin layout is selected in the CAM.
(Ref. AMM TASK 23-73-00-860-002)
(4) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
B. Put the aircraft back to its initial configuration.
(1) Do the procedure of ground configuration after flight configuration.
(Ref. AMM TASK 32-00-00-860-002)
(2) Make sure that the active cabin layout is the same as before you started the test.
(Ref. AMM TASK 23-73-00-860-008)
(3) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
Subtask 23-73-00-860-092-D ** ON A/C NOT FOR ALL (1) Do the procedure of ground configuration after flight configuration.
(Ref. AMM TASK 32-00-00-860-002)
(2) Make sure that the active cabin layout is the same as before you started the test.
(Ref. AMM TASK 23-73-00-860-008)
(3) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
B. Put the aircraft back to its initial configuration.
(1) Do the procedure of ground configuration after flight configuration.
(Ref. AMM TASK 32-00-00-860-002)
(2) Make sure that the slats are fully retracted to lever 0 position.
(Ref. AMM TASK 27-50-00-866-009)
(3) Make sure that the active cabin layout is the same as before you started the test.
(Ref. AMM TASK 23-73-00-860-008)
(4) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
(1) Do the procedure of ground configuration after flight configuration.
(Ref. AMM TASK 32-00-00-860-002)
(2) Make sure that the slats are fully retracted to lever 0 position.
(Ref. AMM TASK 27-50-00-866-009)
(3) Make sure that the active cabin layout is the same as before you started the test.
(Ref. AMM TASK 23-73-00-860-008)
(4) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)