W DOC AIRBUS | AMM A320F

Operational Test of the Three-Axis-Accelerometer thru the MCDU


TASK 31-33-00-710-016-A
Operational Test of the Three-Axis-Accelerometer thru the MCDU


FIN: 6TU
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. 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 31-36-00-740-008-A
Access to the Parameter Call-Up Menus
3. Job Set-up
Subtask 31-33-00-861-065-A
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 31-33-00-865-078-A
B. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAUTO FLT/MCDU/111CA1B01
** ON A/C ALL
49VUSDAC/1 AND 2/28VDC/ESS BUS12WVF05
49VUSDAC/1/SPLY3WVF04
49VUSDAC/2/26VAC SYNC/AC ESS BUS6WVF03
49VUSDAC/1/26VAC SYNC/AC ESS BUS5WVF02
** ON A/C NOT FOR ALL
49VUAUTO FLT/MCDU/111CA1H07
** ON A/C NOT FOR ALL
121VUEIS/SDAC/1/BUS1/26VAC SYNC AC9WVQ04
** ON A/C NOT FOR ALL
121VURCDR/DFDR7TUK16
** ON A/C NOT FOR ALL
121VURCDR/ACCLRM9TUK18
** ON A/C NOT FOR ALL
121VUFDIU8TUK17
** ON A/C ALL
121VUAUTO FLT/MCDU/211CA2N20
121VUHYDRAULIC/HYD/QTY/IND1831GQP35
121VUEIS/SDAC/2/SPLY2WVQ06
121VUEIS/SDAC/2/BUS1/26VAC SYNC AC10WVQ05
121VUEIS/SDAC/1/BUS2/26VAC SYNC AC7WVQ03
121VUEIS/SDAC/2/BUS2/26VAC SYNC AC8WVQ02
** ON A/C NOT FOR ALL
121VUAIDS & RCDR/FDIMU5TVK15
** ON A/C NOT FOR ALL
121VURCDR2 CVR&FDR42TUK16
** ON A/C NOT FOR ALL
121VURCDR/ACCLRM9TUK41
121VURCDR2 CVR&FDR42TUK39
121VUAIDS & RCDR/FDIMU5TVK38
4. Procedure
Subtask 31-33-00-710-079-A
A. Test of the Three-Axis-Accelerometer via MCDU
   (1) Get access to the ALPHA CALL up menu (Ref. AMM TASK 31-36-00-740-008).
   (2) Enter the alpha call-up LATA, LONA and VRTA.
   (3) Make sure that these ALPHA CALL ups show the correct value:
  • for LATA the value is between -0.1 and +0.1 ( nominal 0g)
  • for LONA the value is between -0.1 and +0.1 ( nominal 0g)
  • for VRTA the value is between +0.9 and +1.1 ( nominal 1g).
5. Close-up
Subtask 31-33-00-862-065-A
A. Put the aircraft back to its initial configuration.
   (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 08:31:38 UTC