W DOC AIRBUS | AMM A320F

Operational Test of the Trim Air Check-Valves


TASK 21-63-00-710-005-A
Operational Test of the Trim Air Check-Valves


FIN: 18HM
FIN: 19HM
1. Reason for the Job
Referenced from TSM
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TASK 12-33-21-618-001-A-01
Pre-conditioning through the HP Ground Connection
TASK 12-33-21-618-001-A-02
Pre-conditioning with the APU
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
3. Job Set-up
Subtask 21-63-00-865-073-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
** ON A/C NOT FOR ALL
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS24HKV20
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS13HKV19
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS22HKV18
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS11HKV17
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 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
Subtask 21-63-00-860-056-A
B. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
   (3) Do the pre-conditioning through the HP ground connector (Ref. AMM TASK 12-33-21-618-001) or with the APU (Ref. AMM TASK 12-33-21-618-001)
   (4) On the AIR COND panel 30VU, make sure that:
  • the PACK 1 and PACK 2 pushbutton switches are in the off position (the OFF legends are on).
4. Procedure
Subtask 21-63-00-710-058-A
A. Operational Test of the Trim Air Check-Valves
ACTION
RESULT
1.On the ECAM control panel 11VU:
  • push the BLEED page pushbutton switch.
On the ECAM bleed page:
  • the Pack 1 and Pack 2 outlet temperatures are shown.
2.On the AIR COND panel 30VU:
  • push the Pack 1 pushbutton switch to on.
On the AIR COND panel 30VU:
  • the OFF legend is off.

On the ECAM Bleed page:
  • the Pack 2 outlet temperature does not increase (for approx. 90 seconds).
3.On the AIR COND panel 30VU:
  • push the Pack 1 pushbutton switch to OFF.
On the AIR COND panel 30VU:
  • the OFF legend is on.
4.On the AIR COND panel 30VU:
  • Push the Pack 2 pushbutton switch to on.
On the AIR COND panel 30VU:
  • the OFF legend is off.

On the ECAM Bleed page:
  • the Pack 1 outlet temperature does not increase (for approx. 90 seconds).
5. Close-up
Subtask 21-63-00-860-057-A
A. Put the aircraft back to its initial configuration.
Stop the pre-conditioning through the HP ground connector (Ref. AMM TASK 12-33-21-618-001) or the APU (Ref. AMM TASK 12-33-21-618-001)
   (1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:11:43 UTC