Operational Check of Cargo Compartment Smoke Detection by CFDS to Confirm Isolation Valves Latching Circuit Integrity.
TASK 26-16-00-710-003-A
Operational Check of Cargo Compartment Smoke Detection by CFDS to Confirm Isolation Valves Latching Circuit Integrity.
Refer to the MPD TASK: 261600-04
OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE DETECTION BY CFDS TO CONFIRM ISOLATION VALVES LATCHING CIRCUIT INTEGRITY.
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 26-16-00-860-052-A ** ON A/C NOT FOR ALL
Subtask 26-16-00-710-052-H ** ON A/C NOT FOR ALL
Subtask 26-16-00-860-053-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 04:59:28 UTC
Operational Check of Cargo Compartment Smoke Detection by CFDS to Confirm Isolation Valves Latching Circuit Integrity.
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 261600-04
OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE DETECTION BY CFDS TO CONFIRM ISOLATION VALVES LATCHING CIRCUIT INTEGRITY.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 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 31-32-00-860-005-A | Procedure to Get Access to the SYSTEM REPORT/TEST FIRE PROT Page |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 26-16-00-860-052-A ** 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) On the overhead panel 22VU, make sure that the FWD ISOL VALVE pushbutton switch is on (the OFF light is off).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Make sure that the ENGINE/WARNING page comes into view on the ECAM upper display unit.
(5) On one MCDU get the SYSTEM REPORT/TEST FIRE PROT menu (Ref. AMM TASK 31-32-00-860-005).
Subtask 26-16-00-860-052-B ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 22VU, make sure that the FWD ISOL VALVE pushbutton switch is on (the OFF light is off).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Make sure that the ENGINE/WARNING page comes into view on the ECAM upper display unit.
(5) On one MCDU get the SYSTEM REPORT/TEST FIRE PROT menu (Ref. AMM TASK 31-32-00-860-005).
NOTE: You must visually monitor the two isolation valves in the forward cargo-compartment during the test.
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 22VU, make sure that the AFT ISOL VALVE pushbutton switch is on (the OFF light is off).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Make sure that the ENGINE/WARNING page comes into view on the ECAM upper display unit.
(5) On one MCDU get the SYSTEM REPORT/TEST FIRE PROT menu (Ref. AMM TASK 31-32-00-860-005).
Subtask 26-16-00-860-052-D ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 22VU, make sure that the AFT ISOL VALVE pushbutton switch is on (the OFF light is off).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Make sure that the ENGINE/WARNING page comes into view on the ECAM upper display unit.
(5) On one MCDU get the SYSTEM REPORT/TEST FIRE PROT menu (Ref. AMM TASK 31-32-00-860-005).
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 22VU, make sure that the AFT ISOL VALVE pushbutton switch is on (the OFF light is off).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Make sure that the ENGINE/WARNING page comes into view on the ECAM upper display unit.
(5) On the ECAM control panel, push the COND pushbutton switch and make sure that the COND page comes into view on the ECAM lower display unit.
(6) On one MCDU get the SYSTEM REPORT/TEST FIRE PROT menu (Ref. AMM TASK 31-32-00-860-005).
Subtask 26-16-00-865-066-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 22VU, make sure that the AFT ISOL VALVE pushbutton switch is on (the OFF light is off).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) Make sure that the ENGINE/WARNING page comes into view on the ECAM upper display unit.
(5) On the ECAM control panel, push the COND pushbutton switch and make sure that the COND page comes into view on the ECAM lower display unit.
(6) On one MCDU get the SYSTEM REPORT/TEST FIRE PROT menu (Ref. AMM TASK 31-32-00-860-005).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/SDCU/CHAN1 | 11WQ | C06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/CIDS/DIR ESS/2 | 157RH | G02 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/CIDS/DIR ESS/1 | 150RH | G01 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/AFT CARGO/VENT/CTL & MONG | 31HN | C07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/AFT CARGO/VENT & HTG/CTL & MONG | 31HN | C07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/CIDS/SDF/DIR2 ESS | 18WH | C06 |
| 49VU | AIR COND/CIDS/SDF/DIR1 ESS | 15WH | C05 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/CARGO FIRE/EXTIG/BTL1 | 1WX | C03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/CARGO FIRE/EXTIG/BTL2 | 8WX | C04 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM DIR ESS/2 | 157RH | G02 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/CARGO/FIRE/EXTIG/BTL1 | 1WX | C03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/FWD CARGO/VENT/CTL & MONG | 2HN | C08 |
| 49VU | COM NAV/CIDS/DIR2 ESS | 157RH | G02 |
| 49VU | COM NAV/CIDS/DIR1 ESS | 150RH | G01 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/CARGO FIRE/EXTIG/BTL2 | 8WX | C05 |
| 49VU | AIR COND/CARGO/FIRE/EXTIG/BTL1 | 1WX | C04 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | COM NAV/CIDS/DIR NORM/2 | 156RH | M06 |
| 121VU | COM NAV/CIDS/DIR NORM/1 | 151RH | M05 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | COM NAV/CIDS/DIR NORM/2 | 156RH | M07 |
| 121VU | COM NAV/CIDS/DIR NORM/1 | 151RH | M06 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | COM NAV/CIDS/DIR2 NORM | 156RH | M06 |
| 121VU | COM NAV/CIDS/DIR1 NORM | 151RH | M05 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/SDCU/CHAN2 | 12WQ | T18 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/ZONE TEMP CTL/28VDC/SYS2 | 4HK | V20 |
| 122VU | AIR COND/ZONE TEMP CTL/28VDC/SYS1 | 3HK | V19 |
| 122VU | AIR COND/ZONE TEMP CTL/115VAC/SYS2 | 2HK | V18 |
| 122VU | AIR COND/ZONE TEMP CTL/115VAC/SYS1 | 1HK | V17 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/CARGO/FIRE/EXTIG | 1WX | T19 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/AFT CARGO VENT/FAN | 30HN | S22 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/CIDS/SDF/DIR NORM/2 | 14WH | T18 |
| 122VU | AIR COND/CIDS/SDF/DIR NORM/1 | 17WH | T17 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | FWD CARGO VENT AND HTG/FAN | 1HN | T22 |
Subtask 26-16-00-710-052-H ** ON A/C NOT FOR ALL
A. Test of the Cargo-Compartment Smoke-Detection System
Subtask 26-16-00-710-052-J ** ON A/C NOT FOR ALL NOTE: Make sure that the SDCU is supplied with power for at least one minute before you start the test.
NOTE: Procedure messages related to the red message will be shown on the ECAM upper display unit. These procedure messages are automatic procedures and can be ignored.
| ACTION | RESULT |
|---|---|
1.On the MCDU:
| On the MCDU:
|
|
|
|
|
| | On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
2.On the MCDU:
| On the MCDU:
|
| | All warnings and indications are canceled. |
|
|
| | On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
| | On the ECAM upper display unit:
|
| | On the ECAM lower display unit:
|
3.On the MCDU:
| On the MCDU:
|
4.On the circuit breaker panel 49VU:
| On the ECAM lower display unit:
|
| On the ECAM upper display unit:
|
| | On the cockpit overhead panel 22VU:
|
| | All warnings and remaining indications are canceled. |
A. Test of the Cargo-Compartment Smoke-Detection System
(1) Make sure that the SDCU is supplied with power for at least one minute before you start the test.
Subtask 26-16-00-710-052-AA ** ON A/C NOT FOR ALL (1) Make sure that the SDCU is supplied with power for at least one minute before you start the test.
| ACTION | RESULT |
|---|---|
1.On the MCDU:
| On the MCDU:
|
|
|
|
|
| | On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
2.On the MCDU:
| On the MCDU:
|
| | All warnings and indications go out of view. |
|
|
| | On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
| | On the ECAM lower display unit:
|
3.On the MCDU:
| On the MCDU:
|
| | All warnings and indications go out of view. |
4.On the circuit breaker panel 49VU:
| On the ECAM lower display unit:
|
A. Test of the Cargo-Compartment Smoke-Detection System
(1) Both CIDS-SDF channels and all cargo-compartment smoke-detectors must be supplied with power for a minimum of 30 seconds before you start the test.
(2) Do this test procedure:
Subtask 26-16-00-710-052-AB ** ON A/C NOT FOR ALL (1) Both CIDS-SDF channels and all cargo-compartment smoke-detectors must be supplied with power for a minimum of 30 seconds before you start the test.
(2) Do this test procedure:
NOTE: Procedures related to the red message will be shown during the test on the ECAM upper display-unit. These procedures are automatic and can be ignored.
| ACTION | RESULT |
|---|---|
1.On the MCDU:
| On the MCDU: If SDCU indication is displayed:
|
| | If SMOKE indication is displayed on the MCDU:
|
If SDCU indication is displayed on the MCDU:
| On the MCDU:
|
If SMOKE indication is displayed on the MCDU:
| On the MCDU:
|
2.On the MCDU:
| On the MCDU:
|
|
|
| | On glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display-unit:
|
| | On CARGO SMOKE panel 22VU:
|
| On the MCDU: The SMK DET FWD LDCC TEST page comes into view and the message: TEST OK shows. |
| | In the cockpit:
NOTE: There is a delay of some seconds between the time when you push the YES indication and until the warnings go out of view and the chime stops. |
3.On the MCDU:
| On the MCDU:
|
| On the MCDU:
|
| | On the ECAM lower display:
|
| |
| On glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display-unit:
|
| | On CARGO SMOKE panel 22VU:
|
| | On the ECAM lower display-unit:
|
| | On the MCDU:
|
|
|
| In the cockpit:
|
| | On the ECAM lower display-unit:
|
| | On the MCDU:
|
4.On circuit breaker panel 49VU:
| On the ECAM lower display-unit:
|
| On the MCDU:
|
5.On the MCDU:
| On the MCDU:
|
|
|
Open, safety and tag this(these) circuit breaker(s):
|
|
6.On the MCDU:
| On the MCDU: If SDCU indication is displayed:
|
| | On the MCDU:
|
If SDCU indication is displayed on the MCDU:
| On the MCDU:
|
7.On the MCDU:
|
|
| On the MCDU:
|
| | On the ECAM lower display:
|
| |
| On glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display-unit:
|
| | On CARGO SMOKE panel 22VU:
|
| | On the ECAM lower display-unit:
|
| | On the MCDU:
|
|
|
| In the cockpit:
|
| | On the ECAM lower display-unit:
|
| | On the MCDU:
|
8.On circuit breaker panel 49VU:
| On the ECAM lower display-unit:
|
| On the MCDU:
|
9.On the MCDU:
| On the MCDU:
|
|
|
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
|
|
A. Test of the Cargo-Compartment Smoke-Detection System
(1) Both CIDS-SDF channels and all cargo-compartment smoke-detectors must be supplied with power for a minimum of 30 seconds before you start the test.
(2) Do this test procedure:
Subtask 26-16-00-710-052-IR ** ON A/C NOT FOR ALL (1) Both CIDS-SDF channels and all cargo-compartment smoke-detectors must be supplied with power for a minimum of 30 seconds before you start the test.
(2) Do this test procedure:
NOTE: Procedures related to the red message will be shown during the test on the ECAM upper display unit. These procedures are automatic and can be ignored.
| ACTION | RESULT |
|---|---|
1.On the MCDU:
| On the MCDU: If SDCU indication is displayed:
|
| | If SMOKE indication is displayed on the MCDU:
|
If SDCU indication is displayed on the MCDU:
| On the MCDU:
|
2.On the MCDU:
| On the MCDU:
|
|
|
| | On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
| On the MCDU: The SMK DET FWD LDCC TEST page comes into view and the message: TEST OK shows. |
| | In the cockpit:
NOTE: There is a delay of some seconds between the time when you push the YES indication and until the warnings go out of view and the chime stops. |
3.On the MCDU:
| On the MCDU:
|
| On the MCDU:
|
| | On the ECAM lower display:
|
| |
| On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
| | On the ECAM lower display unit:
|
| | On the MCDU:
|
|
|
| In the cockpit:
|
| | On the ECAM lower display unit:
|
| | On the MCDU:
|
4.On the circuit breaker panel 49VU:
| On the ECAM lower display unit:
|
| On the MCDU:
|
5.On the MCDU:
| On the MCDU:
|
|
|
Open, safety and tag this(these) circuit breaker(s):
|
|
6.On the MCDU:
| On the MCDU: If SDCU indication is displayed:
|
| | If SMOKE indication is displayed on the MCDU:
|
If SDCU indication is displayed on the MCDU:
| On the MCDU:
|
7.On the MCDU:
|
|
| On the MCDU:
|
| | On the ECAM lower display:
|
| |
| On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
| | On the ECAM lower display unit:
|
| | On the MCDU:
|
|
|
| In the cockpit:
|
| | On the ECAM lower display unit:
|
| | On the MCDU:
|
8.On the circuit breaker panel 49VU:
| On the ECAM lower display unit:
|
| On the MCDU:
|
9.On the MCDU:
| On the MCDU:
|
|
|
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
|
|
A. Test of the Cargo-Compartment Smoke-Detection System
(1) Both CIDS-SDF channels and all cargo-compartment smoke-detectors must be supplied with power for a minimum of 30 seconds before you start the test.
(2) Do this test procedure:
5. Close-up(1) Both CIDS-SDF channels and all cargo-compartment smoke-detectors must be supplied with power for a minimum of 30 seconds before you start the test.
(2) Do this test procedure:
NOTE: Procedures related to the red message will be shown during the test on the ECAM upper display unit. These procedures are automatic and can be ignored.
| ACTION | RESULT |
|---|---|
1.On the MCDU:
| On the MCDU: If SDCU indication is displayed:
SDF2 |
If the SDCU indication is shown on the MCDU:
| On the MCDU:
|
2.On the MCDU:
| On the MCDU:
|
|
|
| | On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
| On the MCDU: The SMK DET AFT LDCC TEST page comes into view and the message: TEST OK shows. |
| | In the cockpit:
NOTE: There is a delay of some seconds between the time when you push the YES indication and until the warnings go out of view and the chime stops. |
3.On the MCDU:
| On the MCDU:
|
| On the MCDU:
|
| | On the ECAM lower display:
|
| |
| On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
| | On the MCDU:
|
|
|
| In the cockpit:
|
| | On the ECAM lower display unit:
|
| | On the MCDU:
|
On the circuit breaker panel 49VU:
| On the ECAM lower display unit:
|
4.On the MCDU:
| On the MCDU:
|
|
|
|
|
Open, safety and tag this(these) circuit breaker(s):
|
|
On the MCDU:
| On the MCDU: If the SDCU indication is shown:
|
If the SDCU indication is shown on the MCDU:
| On the MCDU:
|
On the MCDU:
| On the MCDU:
|
| On the MCDU:
|
| | On the ECAM lower display:
|
| |
| On the glareshield panels 130VU and 131VU:
|
| | On the ECAM upper display unit:
|
| | On the CARGO SMOKE panel 22VU:
|
| | On the MCDU:
|
|
|
| In the cockpit:
|
| | On the ECAM lower display unit:
|
| | On the MCDU:
|
On the circuit breaker panel 49VU:
| On the ECAM lower display unit:
|
5.On the MCDU:
| On the MCDU:
NOTE: If you receive this message, the test result is satisfactory. |
On the MCDU:
| On the MCDU:
|
|
|
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
|
|
Subtask 26-16-00-860-053-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).