Operational Test of the Flow Control and Indicating System
TASK 21-51-00-710-002-A
Operational Test of the Flow Control and Indicating System
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 21-51-00-861-054-A Subtask 21-51-00-865-054-A
Subtask 21-51-00-710-051-A ** ON A/C NOT FOR ALL
Subtask 21-51-00-865-056-A
[Rev.10 from 2021]
2026.03.31 23:05:59 UTC
Operational Test of the Flow Control and Indicating System
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-33-21-618-001-A-01 | Pre-conditioning through the HP Ground Connection |
| 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 |
| TASK 34-10-00-860-002-A | ADIRS Start Procedure |
| TASK 49-00-00-860-005-A | APU Start by External Power |
| TASK 49-00-00-860-005-A-01 | APU Start by Batteries |
| TASK 49-00-00-860-006-A | APU Shutdown by External Power |
| TASK 49-00-00-860-006-A-01 | APU Shutdown by Batteries |
| TASK 49-00-00-860-008-A | APU Start by External Power |
| TASK 49-00-00-860-008-A-01 | APU Start by Batteries |
| TASK 49-00-00-860-009-A | APU Shutdown by External Power (131-9(A)) |
| TASK 49-00-00-860-009-A-01 | APU Shutdown by Batteries (131-9(A)) |
| TASK 71-00-00-710-018-A | Discontinued Start, Restart and Shutdown Procedures |
| TASK 71-00-00-710-043-A | Normal Engine Automatic-Start Procedure |
Subtask 21-51-00-861-054-A Subtask 21-51-00-865-054-A
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 21-51-00-865-055-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/FLOW/CTL &/IND1 | 1HB | D07 |
| ** ON A/C ALL | |||
| 49VU | AIR COND/AVNCS VENT/CTL | 6HQ | D06 |
| 49VU | AIR COND/AVNCS VENT/CTL | 5HQ | D05 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/TEMP CTL/SYS 1 CHAN B/28VDC | 52HH | D08 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/FLOW/MIXER/FLAP | 3HB | V22 |
| 122VU | AIR COND/FLOW/CTL AND IND/2 | 2HB | V21 |
| 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/PACK TEMP/CTL SYS1/2/115VAC | 21HH | W22 |
| 122VU | AIR COND/PACK TEMP/CTL SYS1/2/28VDC | 23HH | W21 |
| 122VU | AIR COND/PACK TEMP/CTL SYS1/1/115VAC | 1HH | X22 |
| 122VU | AIR COND/PACK TEMP/CTL SYS1/1/28VDC | 3HH | X21 |
| 122VU | AIR COND/PACK TEMP CTL SYS2/2/28VDC | 24HH | Y21 |
| 122VU | AIR COND/PACK TEMP CTL SYS2/2/115VAC | 22HH | Y20 |
| 122VU | AIR COND/PACK TEMP CTL SYS2/1/28VDC | 4HH | Y19 |
| 122VU | AIR COND/PACK TEMP CTL SYS2/1/115VAC | 2HH | Y18 |
| ** ON A/C ALL | |||
| 122VU | AIR COND/LAV/GALLEY VENT CTL/EXTRACT FAN/CTL | 5HU | U21 |
| 122VU | AIR COND/LAV/GALLEY VENT CTL/EXTRACT FAN/SPLY | 6HU | U19 |
| 122VU | AIR COND/RECIRC FAN/R/CTL | 11HG | W20 |
| 122VU | AIR COND/RECIRC FAN/R/SPLY | 3HG | W18 |
| 122VU | AIR COND/RECIRC FAN/L/CTL | 2HG | X20 |
| 122VU | AIR COND/RECIRC FAN/L/SPLY | 1HG | X18 |
| 122VU | AIR COND/AVNCS/VENT/MONG | 3HQ | Y17 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN A/115VAC | 53HH | W22 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN A/28VDC | 55HH | W21 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN A/115VAC | 49HH | X22 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN A/28VDC | 51HH | X21 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN B/28VDC | 56HH | Y21 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN B/115VAC | 54HH | Y20 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN B/115VAC | 50HH | Y18 |
| ** 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. Open, safety and tag this(these) circuit breaker(s):
Subtask 21-51-00-860-060-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/ZONE TEMP CTL/115VAC/SYS1 | 1HK | V17 |
D. Preconditioning
(1) Do the Procedure to Start the APU: or
(3) Do the preconditioning with engine bleed.
Subtask 21-51-00-860-051-C ** ON A/C NOT FOR ALL (1) Do the Procedure to Start the APU: or
- (Ref. AMM D/O 49-00-00-86) or,
- (Ref. AMM TASK 49-00-00-860-005) or,
- (Ref. AMM TASK 49-00-00-860-008).
(3) Do the preconditioning with engine bleed.
- Start the engine 1(2) (Ref. AMM TASK 71-00-00-710-043) or (Ref. AMM D/O 71-00-00-86).
- Make sure that the X BLEED selector is at the AUTO position on the AIR COND panel 30VU.
- Make sure that the PACK 1 and the PACK 2 pushbutton switches are in the on position (the FAULT and the OFF legends are off).
- Move the applicable throttle control lever forward until on the BLEED page a pack inlet pressure of 30 psig is shown.
NOTE: Use this alternative procedure if during the test the pack flow indicator does not reach the predetermined position.
E. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(2) On the AIR panel 30VU:
(4) Cockpit Effects
(a) After approximately 60 seconds:
Subtask 21-51-00-860-051-D ** ON A/C NOT FOR ALL (1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(2) On the AIR panel 30VU:
- put the APU BLEED pushbutton switch to the on position (the ON legend comes on) and,
- put the PACK 1 and the PACK 2 pushbutton switches to the on position (the OFF legends go off).
(4) Cockpit Effects
(a) After approximately 60 seconds:
- on the COND page the message ALTN MODE shows above the aircraft symbols and,
- on the upper ECAM display the message, COND ZONE REGUL FAULT, is shown.
E. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(2) Make sure that the ADIRU is activated (Ref. AMM TASK 34-10-00-860-002).
(3) On the AIR panel 30VU:
4. Procedure(1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(2) Make sure that the ADIRU is activated (Ref. AMM TASK 34-10-00-860-002).
(3) On the AIR panel 30VU:
- put the APU BLEED pushbutton switch to the on position (the ON legend comes on) and,
- put the PACK 1 and the PACK 2 pushbutton switches to the on position (the OFF legends go off).
Subtask 21-51-00-710-051-A ** ON A/C NOT FOR ALL
A. Operational Test of the Flow Control and Indicating System:
Subtask 21-51-00-710-051-B ** ON A/C NOT FOR ALL NOTE: The approximate times given in this test can be very different as they are dependant upon:
- the ambient air temperature and altitude above sea level,
- the type and overall condition of the APU installed in the aircraft and,
- the overall condition of the environmental control system.
| ACTION | RESULT |
|---|---|
| 1. FOR [8HB] | |
A.On the panel 30VU:
| The OFF legend in the PACK 2 pushbutton switch comes on. |
| | On the ECAM lower display unit:
|
B.On the panel 30VU:
| On the panel 30VU:
|
| | On the ECAM lower display unit:
|
| | After approx. 180 seconds:
|
| | After approx. 10 seconds:
|
| | After approx. 35 seconds:
|
| 2. FOR [11HB] | |
C.On the panel 30VU:
| The OFF legend in the PACK 1 pushbutton switch comes on. |
| | On the ECAM lower display unit:
|
D.On the panel 30VU:
| On the panel 30VU:
|
| | On the ECAM lower display unit:
|
| | After approx. 180 seconds:
|
| | After approx. 10 seconds:
|
| | After approx. 35 seconds:
|
A. Operational Test of the Flow Control and Indicating System
Subtask 21-51-00-710-051-C ** ON A/C NOT FOR ALL NOTE: The approximate times given in this test can be very different as they are dependant upon:
- the ambient air temperature and altitude above sea level,
- the type and overall condition of the APU installed in the aircraft and,
- the overall condition of the environmental control system.
| ACTION | RESULT |
|---|---|
| 1. FOR [8HB] | |
A.On the panel 30VU:
| The OFF legend in the PACK 2 pushbutton switch comes on. |
| | On the ECAM lower display unit:
|
B.On the panel 30VU:
| On the panel 30VU:
|
| | On the ECAM lower display unit:
|
| | After approx. 180 seconds:
|
| | After approx. 10 seconds:
|
| | After approx. 35 seconds:
|
| 2. FOR [11HB] | |
C.On the panel 30VU:
| The OFF legend in the PACK 1 pushbutton switch comes on. |
| | On the ECAM lower display unit:
|
D.On the panel 30VU:
| On the panel 30VU:
|
| | On the ECAM lower display unit:
|
| | After approx. 180 seconds:
|
| | After approx. 10 seconds:
|
| | After approx. 35 seconds:
|
A. Operational Test of the Flow Control and Indicating System
Subtask 21-51-00-710-051-D ** ON A/C NOT FOR ALL NOTE: The approximate times given in this test can be very different as they are dependant upon:
- the ambient air temperature and altitude above sea level,
- the type and overall condition of the APU installed in the aircraft and,
- the overall condition of the environmental control system.
| ACTION | RESULT |
|---|---|
| 1. FOR [24HB] | |
A.On the panel 30VU:
| The OFF legend in the PACK 2 pushbutton switch comes on. |
| | On the ECAM lower display unit:
|
B.On the panel 30VU:
| On the panel 30VU:
|
| | On the ECAM lower display unit:
|
| | After approx. 180 seconds:
|
| | After approx. 20 seconds:
|
| | After approx. 35 seconds:
|
| 2. FOR [23HB] | |
C.On the panel 30VU:
| The OFF legend in the PACK 1 pushbutton switch comes on. |
| | On the ECAM lower display unit:
|
D.On the panel 30VU:
| On the panel 30VU:
|
| | On the ECAM lower display unit:
|
| | After approx. 180 seconds:
|
| | After approx. 20 seconds:
|
| | After approx. 35 seconds:
|
A. Operational Test of the Flow Control and Indicating System
5. Close-upNOTE: The approximate times given in this test can be very different as they are dependant upon:
- the ambient air temperature and altitude above sea level,
- the type and overall condition of the APU installed in the aircraft and,
- the overall condition of the environmental control system.
| ACTION | RESULT |
|---|---|
| 1. FOR [8HB] | |
A.On the panel 30VU:
| The OFF legend in the PACK 2 pushbutton switch comes on. |
| | On the ECAM lower display unit:
|
B.On the panel 30VU:
| On the panel 30VU:
|
| | On the ECAM lower display unit:
|
| | After approx. 180 seconds:
|
| | After approx. 10 seconds:
|
| | After approx. 35 seconds:
|
| 2. FOR [11HB] | |
C.On the panel 30VU:
| The OFF legend in the PACK 1 pushbutton switch comes on. |
| | On the ECAM lower display unit:
|
D.On the panel 30VU:
| On the panel 30VU:
|
| | On the ECAM lower display unit:
|
| | After approx. 180 seconds:
|
| | After approx. 10 seconds:
|
| | After approx. 35 seconds:
|
Subtask 21-51-00-865-056-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 21-51-00-860-052-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/ZONE TEMP CTL/115VAC/SYS1 | 1HK | V17 |
B. Aircraft Maintenance Configuration
(1) Preconditioning
(a) Do the Procedure to Stop the APU or,
(c) Stop the precondition with engine bleed.
(4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(1) Preconditioning
(a) Do the Procedure to Stop the APU or,
- (Ref. AMM D/O 49-00-00-86) or,
- (Ref. AMM TASK 49-00-00-860-006) or,
- (Ref. AMM TASK 49-00-00-860-009).
(c) Stop the precondition with engine bleed.
- stop the engine 1(2) (Ref. AMM TASK 71-00-00-710-018).
- (Ref. AMM TASK 31-60-00-860-002) or
- stop the engine 1(2) (Ref. AMM D/O 71-00-00-86)
(4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).