W DOC AIRBUS | AMM A320F

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
REFERENCE
QTY
DESIGNATION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Referenced Information
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
3. Job Set-up
Subtask 21-51-00-861-054-A
A. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 21-51-00-865-054-A
B. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR COND/FLOW/CTL &/IND11HBD07
** ON A/C ALL
49VUAIR COND/AVNCS VENT/CTL6HQD06
49VUAIR COND/AVNCS VENT/CTL5HQD05
** ON A/C NOT FOR ALL
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
** ON A/C NOT FOR ALL
122VUAIR COND/FLOW/MIXER/FLAP3HBV22
122VUAIR COND/FLOW/CTL AND IND/22HBV21
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS24HKV20
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS13HKV19
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS22HKV18
122VUAIR COND/PACK TEMP/CTL SYS1/2/115VAC21HHW22
122VUAIR COND/PACK TEMP/CTL SYS1/2/28VDC23HHW21
122VUAIR COND/PACK TEMP/CTL SYS1/1/115VAC1HHX22
122VUAIR COND/PACK TEMP/CTL SYS1/1/28VDC3HHX21
122VUAIR COND/PACK TEMP CTL SYS2/2/28VDC24HHY21
122VUAIR COND/PACK TEMP CTL SYS2/2/115VAC22HHY20
122VUAIR COND/PACK TEMP CTL SYS2/1/28VDC4HHY19
122VUAIR COND/PACK TEMP CTL SYS2/1/115VAC2HHY18
** ON A/C ALL
122VUAIR COND/LAV/GALLEY VENT CTL/EXTRACT FAN/CTL5HUU21
122VUAIR COND/LAV/GALLEY VENT CTL/EXTRACT FAN/SPLY6HUU19
122VUAIR COND/RECIRC FAN/R/CTL11HGW20
122VUAIR COND/RECIRC FAN/R/SPLY3HGW18
122VUAIR COND/RECIRC FAN/L/CTL2HGX20
122VUAIR COND/RECIRC FAN/L/SPLY1HGX18
122VUAIR COND/AVNCS/VENT/MONG3HQY17
** ON A/C NOT FOR ALL
122VUAIR COND/TEMP CTL SYS 2/CHAN A/115VAC53HHW22
122VUAIR COND/TEMP CTL SYS 2/CHAN A/28VDC55HHW21
122VUAIR COND/TEMP CTL SYS 1/CHAN A/115VAC49HHX22
122VUAIR COND/TEMP CTL SYS 1/CHAN A/28VDC51HHX21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/28VDC56HHY21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/115VAC54HHY20
122VUAIR COND/TEMP CTL SYS 1/CHAN B/115VAC50HHY18
** ON A/C NOT FOR ALL
123VUAVNCS VENT/EXTC/FAN2HQAE02
** ON A/C ALL
123VUAVNCS VENT/BLOWER/FAN1HQAD10
** ON A/C NOT FOR ALL
123VUAVNCS VENT/EXTC/FAN2HQAC04
Subtask 21-51-00-865-055-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS11HKV17
Subtask 21-51-00-860-060-A
D. Preconditioning
   (1) Do the Procedure to Start the APU: or
   (2) Do the preconditioning through the HP connector (Ref. AMM TASK 12-33-21-618-001), or
   (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.
Subtask 21-51-00-860-051-C ** ON A/C NOT FOR ALL
E. Aircraft Maintenance Configuration
   (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).
   (3) Make sure that the BLEED page is shown on the ECAM lower display.
   (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.
Subtask 21-51-00-860-051-D ** ON A/C NOT FOR ALL
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:
  • 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) Make sure that the BLEED page is shown on the ECAM lower display.
4. Procedure
Subtask 21-51-00-710-051-A ** ON A/C NOT FOR ALL
A. Operational Test of the Flow Control and Indicating System:
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:
  • push the PACK 2 pushbutton switch to the off position.
The OFF legend in the PACK 2 pushbutton switch comes on.

On the ECAM lower display unit:
  • the right pack flow control valve shows GREEN and closed.
  • the left pack flow indicator is in the LO indication area (between the LO and the 11 o'clock position).
  • after approx. 10 seconds it moves to the HI indication area (between the 1 o'clock and the HI position).
B.On the panel 30VU:
  • push the PACK 2 pushbutton switch to the on position.
On the panel 30VU:
  • the OFF legend in the PACK 2 pushbutton switch goes off.

On the ECAM lower display unit:
  • the right flow control valve symbol shows GREEN and open.
  • the left pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 180 seconds:
  • the right pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 10 seconds:
  • the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).

After approx. 35 seconds:
  • the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
2. FOR [11HB]
C.On the panel 30VU:
  • push the PACK 1 pushbutton switch to the off position.
The OFF legend in the PACK 1 pushbutton switch comes on.

On the ECAM lower display unit:
  • the left pack flow control valve shows GREEN and closed.
  • the right pack flow indicator is in the LO indication area (between the LO and the 11 o'clock position).
  • after approx. 10 seconds it moves to the HI indication area (between the 1 o'clock and the HI position).
D.On the panel 30VU:
  • push the PACK 1 pushbutton switch to the on position.
On the panel 30VU:
  • the OFF legend in the PACK 1 pushbutton switch goes off.

On the ECAM lower display unit:
  • the left flow control valve symbol shows GREEN and open.
  • the right pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 180 seconds:
  • the left pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 10 seconds:
  • the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).

After approx. 35 seconds:
  • the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
Subtask 21-51-00-710-051-B ** ON A/C NOT FOR ALL
A. Operational Test of the Flow Control and Indicating System
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:
  • push the PACK 2 pushbutton switch to the off position.
The OFF legend in the PACK 2 pushbutton switch comes on.

On the ECAM lower display unit:
  • the right pack flow control valve shows GREEN and closed.
  • the left pack flow indicator is in the LO indication area (between the LO and the 11 o'clock position).
  • after approx. 10 seconds it moves to the HI indication area (between the 1 o'clock and the HI position).
B.On the panel 30VU:
  • push the PACK 2 pushbutton switch to the on position.
On the panel 30VU:
  • the OFF legend in the PACK 2 pushbutton switch goes off.

On the ECAM lower display unit:
  • the right flow control valve symbol shows GREEN and open.
  • the left pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 180 seconds:
  • the right pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 10 seconds:
  • the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).

After approx. 35 seconds:
  • the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
2. FOR [11HB]
C.On the panel 30VU:
  • push the PACK 1 pushbutton switch to the off position.
The OFF legend in the PACK 1 pushbutton switch comes on.

On the ECAM lower display unit:
  • the left pack flow control valve shows GREEN and closed.
  • the right pack flow indicator is in the LO indication area (between the LO and the 11 o'clock position).
  • after approx. 10 seconds it moves to the HI indication area (between the 1 o'clock and the HI position).
D.On the panel 30VU:
  • push the PACK 1 pushbutton switch to the on position.
On the panel 30VU:
  • the OFF legend in the PACK 1 pushbutton switch goes off.

On the ECAM lower display unit:
  • the left flow control valve symbol shows GREEN and open.
  • the right pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 180 seconds:
  • the left pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 10 seconds:
  • the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).

After approx. 35 seconds:
  • the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
Subtask 21-51-00-710-051-C ** ON A/C NOT FOR ALL
A. Operational Test of the Flow Control and Indicating System
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:
  • push the PACK 2 pushbutton switch to the off position.
The OFF legend in the PACK 2 pushbutton switch comes on.

On the ECAM lower display unit:
  • the right pack flow control valve shows GREEN and closed.
  • the left pack flow indicator is in the LO indication area (between the LO and the 11 o'clock position).
  • after approx. 20 seconds it moves to the HI indication area (between the 1 o'clock and the HI position).
B.On the panel 30VU:
  • push the PACK 2 pushbutton switch to the on position.
On the panel 30VU:
  • the OFF legend in the PACK 2 pushbutton switch goes off.

On the ECAM lower display unit:
  • the right flow control valve symbol shows GREEN and open.
  • the left pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 180 seconds:
  • the right pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 20 seconds:
  • the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).

After approx. 35 seconds:
  • the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
2. FOR [23HB]
C.On the panel 30VU:
  • push the PACK 1 pushbutton switch to the off position.
The OFF legend in the PACK 1 pushbutton switch comes on.

On the ECAM lower display unit:
  • the left pack flow control valve shows GREEN and closed.
  • the right pack flow indicator is in the LO indication area (between the LO and the 11 o'clock position).
  • after approx. 10 seconds it moves to the HI indication area (between the 1 o'clock and the HI position).
D.On the panel 30VU:
  • push the PACK 1 pushbutton switch to the on position.
On the panel 30VU:
  • the OFF legend in the PACK 1 pushbutton switch goes off.

On the ECAM lower display unit:
  • the left flow control valve symbol shows GREEN and open.
  • the right pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 180 seconds:
  • the left pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 20 seconds:
  • the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).

After approx. 35 seconds:
  • the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
Subtask 21-51-00-710-051-D ** ON A/C NOT FOR ALL
A. Operational Test of the Flow Control and Indicating System
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:
  • push the PACK 2 pushbutton switch to the off position.
The OFF legend in the PACK 2 pushbutton switch comes on.

On the ECAM lower display unit:
  • the right pack flow control unit shows GREEN and closed.
  • the left pack flow indicator is in the LO indication area (between the LO and the 11 o'clock position).
  • after approx. 10 seconds it moves to the HI indication area (between the 1 o'clock and the HI position).
B.On the panel 30VU:
  • push the PACK 2 pushbutton switch to the on position.
On the panel 30VU:
  • the OFF legend in the PACK 2 pushbutton switch goes off.

On the ECAM lower display unit:
  • the right flow control valve unit shows GREEN and open.
  • the left pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 180 seconds:
  • the right pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 10 seconds:
  • the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).

After approx. 35 seconds:
  • the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
2. FOR [11HB]
C.On the panel 30VU:
  • push the PACK 1 pushbutton switch to the off position.
The OFF legend in the PACK 1 pushbutton switch comes on.

On the ECAM lower display unit:
  • the left pack flow control unit shows GREEN and closed.
  • the right pack flow indicator is in the LO indication area (between the LO and the 11 o'clock position).
  • after approx. 10 seconds it moves to the HI indication area (between the 1 o'clock and the HI position).
D.On the panel 30VU:
  • push the PACK 1 pushbutton switch to the on position.
On the panel 30VU:
  • the OFF legend in the PACK 1 pushbutton switch goes off.

On the ECAM lower display unit:
  • the left flow control unit symbol shows GREEN and open.
  • the right pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 180 seconds:
  • the left pack flow indicator moves to the LO indication area (between the LO and the 11 o'clock position).

After approx. 10 seconds:
  • the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).

After approx. 35 seconds:
  • the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
5. Close-up
Subtask 21-51-00-865-056-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS11HKV17
Subtask 21-51-00-860-052-A
B. Aircraft Maintenance Configuration
   (1) Preconditioning
     (a) Do the Procedure to Stop the APU or,
     (b) Stop the preconditiong through the HP connector (Ref. AMM TASK 12-33-21-618-001) or,
     (c) Stop the precondition with engine bleed.
   (2) Do the EIS stop procedure:
   (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
   (4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.03.31 23:05:59 UTC