Operational Check of Override Function (BLOWER and EXTRACT)
TASK 21-26-00-710-002-A
Operational Check of Override Function (BLOWER and EXTRACT)
Refer to the MPD TASK: 212600-02
OPERATIONAL CHECK OF OVERRIDE FUNCTION (BLOWER AND EXTRACT)
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 21-26-00-040-074-A ** ON A/C NOT FOR ALL
Subtask 21-26-00-710-051-A ** ON A/C NOT FOR ALL
Subtask 21-26-00-860-055-A
[Rev.10 from 2021]
2026.04.01 04:35:33 UTC
Operational Check of Override Function (BLOWER and EXTRACT)
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 212600-02
OPERATIONAL CHECK OF OVERRIDE FUNCTION (BLOWER AND EXTRACT)
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 21-26-12-000-802-A | Removal of the Avionics-Ventilation Comfort Duct-Temperature-Sensor |
| TASK 21-26-12-400-802-A | Installation of the Avionics-Ventilation Comfort Duct-Temperature-Sensor |
| 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 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 21-26-00-040-074-A ** ON A/C NOT FOR ALL
A. Deactivation of the Avionics-Ventilation Comfort Duct-Temperature-Sensor
(1) Disconnect the electrical connector from the duct temperature sensor (Ref. AMM TASK 21-26-12-000-802).
Subtask 21-26-00-865-051-A (1) Disconnect the electrical connector from the duct temperature sensor (Ref. AMM TASK 21-26-12-000-802).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 21-26-00-941-087-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | AIR COND/AVNCS VENT/CTL | 6HQ | D06 |
| 49VU | AIR COND/AVNCS VENT/CTL | 5HQ | D05 |
| 122VU | AIR COND/AVNCS/VENT/MONG | 3HQ | Y17 |
| ** ON A/C NOT FOR ALL | |||
| 123VU | AVNCS VENT/EXTC/FAN | 2HQ | AE02 |
| ** ON A/C ALL | |||
| 123VU | AVNCS VENT/BLOWER/FAN | 1HQ | AD10 |
| ** ON A/C NOT FOR ALL | |||
| 123VU | AVNCS VENT/EXTC/FAN | 2HQ | AC04 |
C. Safety Precautions
(1) Make sure that the engine 1 and 2 throttle control levers are at idle.
Subtask 21-26-00-861-051-A (1) Make sure that the engine 1 and 2 throttle control levers are at idle.
D. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 21-26-00-860-054-C ** ON A/C NOT FOR ALL (Ref. AMM TASK 24-41-00-861-002).
NOTE: The energization of the aircraft electrical circuits starts a full test of the ventilation system. The test continues for 2 minutes approximately.
E. Aircraft Maintenance Configuration
(1) On the VENTILATION section of panel 22VU:
(3) On the ECAM control panel, push the PRESS pushbutton key.
(4) On the lower ECAM display unit:
Subtask 21-26-00-860-054-D ** ON A/C NOT FOR ALL (1) On the VENTILATION section of panel 22VU:
- Make sure that the BLOWER and the EXTRACT pushbutton switches are in the AUTO configuration (the pusbutton switches are pushed and the FAULT and the OVRD legends are off).
(3) On the ECAM control panel, push the PRESS pushbutton key.
(4) On the lower ECAM display unit:
- The CAB PRESS page comes into view and shows the skin air-inlet (INLET) and the skin air-outlet (EXTRACT) valves in the open position (if the outside air temperature is more than or equal to 12 DEG.C (53.6 DEG.F)).
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and the skin air-outlet valves are closed.
NOTE: If the avionics duct temperature is less than 40 DEG.C (104 DEG.F), the skin air-inlet and the skin air-outlet valves are closed.
E. Aircraft Maintenance Configuration
(1) On the VENTILATION section of panel 22VU:
(3) On the ECAM control panel, push the PRESS pushbutton key.
(4) On the lower ECAM display unit:
4. Procedure(1) On the VENTILATION section of panel 22VU:
- Make sure that the BLOWER and the EXTRACT pushbutton switches are in the AUTO configuration (the pusbutton switches are pushed and the FAULT and the OVRD legends are off).
(3) On the ECAM control panel, push the PRESS pushbutton key.
(4) On the lower ECAM display unit:
- The CAB PRESS page comes into view and shows the skin air-inlet (INLET) and the skin air-outlet (OUTLET) valves in the open position (if the outside air temperature is more than or equal to 12 DEG.C (53.6 DEG.F)).
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and the skin air-outlet valves are closed.
NOTE: If the avionics duct temperature is less than 40 DEG.C (104 DEG.F), the skin air-inlet and the skin air-outlet valves are closed.
Subtask 21-26-00-710-051-A ** ON A/C NOT FOR ALL
A. Operational Test of the Override Function
Subtask 21-26-00-710-051-B ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the VENTILATION section of panel 22VU:
| On the VENTILATION section of panel 22VU:
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and skin air-outlet valves stay closed. NOTE: The skin-exchanger isolation valve and the conditioned-air inlet valve open. |
2.On the VENTILATION section of panel 22VU:
| On the VENTILATION section of panel 22VU:
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and skin air-outlet valves stay closed. NOTE: The skin-exchanger isolation valve and the conditioned-air inlet valve close. |
3.On the VENTILATION section of panel 22VU:
| On the VENTILATION section of panel 22VU:
NOTE: The extract fan continues to operate when the OVRD legend is on.
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and skin air-outlet valves stay closed. |
4.On the VENTILATION section of panel 22VU:
| On the VENTILATION section of panel 22VU:
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and skin air-outlet valves stay closed. NOTE: The skin exchanger isolation valve and the conditioned-air inlet valve close. |
A. Operational Test of the Override Function
5. Close-up| ACTION | RESULT |
|---|---|
1.On the VENTILATION section of panel 22VU:
| On the VENTILATION section of panel 22VU:
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and skin air-outlet valves stay closed. NOTE: The skin-exchanger isolation valve and the conditioned-air inlet valve open. |
2.On the VENTILATION section of panel 22VU:
| On the VENTILATION section of panel 22VU:
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and skin air-outlet valves stay closed. NOTE: The skin-exchanger isolation valve and the conditioned-air inlet valve close. |
3.On the VENTILATION section of panel 22VU:
| On the VENTILATION section of panel 22VU:
NOTE: The extract fan continues to operate when the OVRD legend is on.
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and skin air-outlet valves stay closed. |
4.On the VENTILATION section of panel 22VU:
| On the VENTILATION section of panel 22VU:
NOTE: If the outside air temperature is less than 9 DEG.C (48.2 DEG.F), the skin air-inlet and skin air-outlet valves stay closed. NOTE: The skin exchanger isolation valve and the conditioned-air inlet valve close. |
Subtask 21-26-00-860-055-A
A. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
Subtask 21-26-00-862-051-A Subtask 21-26-00-440-067-A ** ON A/C NOT FOR ALL (1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
C. Reactivation of the Avionics-Ventilation Comfort Duct-Temperature-Sensor
(1) Connect the electrical connector to the duct temperature sensor (Ref. AMM TASK 21-26-12-400-802).
(1) Connect the electrical connector to the duct temperature sensor (Ref. AMM TASK 21-26-12-400-802).