W DOC AIRBUS | AMM A320F

Operational Test of the Computers Engagement/Disengagement


TASK 27-96-00-710-002-A
Operational Test of the Computers Engagement/Disengagement


ZONE: 210
1. Reason for the Job
Do the check of the pushbutton switches related to the ELACs and SECs for their correct operation.
2. Job Set-up Information
 A. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
210
CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD
 B. Referenced Information
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 31-60-00-860-001-A
EIS Start Procedure
TASK 31-60-00-860-002-A
EIS Stop Procedure
3. Job Set-up
Subtask 27-96-00-860-060-A
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
   (2) On the overhead panel 23VU, make sure that:
  • the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).
   (3) On the overhead panel 24VU, make sure that:
  • the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).
   (4) On the center pedestal, on the panel 8VU, make sure that:
  • the SWITCHING/ATT HDG, SWITCHING/AIR DATA, SWITCHING/EIS DMC and SWITCHING/ECAM/ND XFR selector switches are in the NORM position.
   (5) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
   (6) On the center pedestal, on the ECAM control panel:
  • push the F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).
Subtask 27-96-00-865-054-A
B. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
** ON A/C ALL
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
4. Procedure
Subtask 27-96-00-710-054-A
A. Do this test:
NOTE: During the test, ignore the MASTER CAUT and the single chime.
ACTION
RESULT
1.On the overhead panel 23VU:
  • release the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches.
On the overhead panel 23VU:
  • the OFF legends of the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches come on.
2.On the overhead panel 23VU:
  • push the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches.
On the overhead panel 23VU:
  • the OFF legends of the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches go off,
  • the FAULT legends of the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches come on then go off.
3.On the overhead panel 24VU:
  • release the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches.
On the overhead panel 24VU:
  • the OFF legends of the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches come on.
4.On the overhead panel 24VU:
  • push the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches.
On the overhead panel 24VU:
  • the OFF legends of the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches go off,
  • the FAULT legends of the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches come on then go off.
5. Close-up
Subtask 27-96-00-860-061-A
A. Put the aircraft back to its initial configuration.
   (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] 2026.03.31 23:59:54 UTC