W DOC AIRBUS | AMM A320F

Installation of the Flight Control Accelerometer

TASK 27-92-16-400-001-A
Installation of the Flight Control Accelerometer

ZONE: 131
ZONE: 132
FIN: 12CE1
FIN: 12CE2
FIN: 12CE3
FIN: 12CE4
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
131
FORWARD CARGO COMPARTMENT
132
FORWARD CARGO COMPARTMENT
822, 825
FOR [12CE1] (ACCLRM-1)
FOR [12CE3] (ACCLRM-3)
131MW
131GW
FOR [12CE2] (ACCLRM-2)
FOR [12CE4] (ACCLRM-4)
132KW
132MW
 C. 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 31-21-00-750-002-A
Procedure to Set the Clock
F Flight Control Accelerometer ** ON A/C NOT FOR ALL
F Flight Control Accelerometer ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 27-92-16-860-051-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access door 825.
   (2) Make sure that the access door 825 is open.
   (3) Make sure that the sidewall panel is removed:
     (a) FOR [12CE1] (ACCLRM-1), [12CE3] (ACCLRM-3)
131MW
     (b) FOR [12CE2] (ACCLRM-2), [12CE4] (ACCLRM-4)
132MW
   (4) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access door 825.
   (5) Make sure that the access door 822 is open.
   (6) On the battery power center 105VU:
  • make sure that the protective cover is removed.
Subtask 27-92-16-860-051-B ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access door 825.
   (2) Make sure that the access door 825 is open.
   (3) Make sure that the sidewall panel is removed:
     (a) FOR [12CE1] (ACCLRM-1), [12CE3] (ACCLRM-3)
131GW
     (b) FOR [12CE2] (ACCLRM-2), [12CE4] (ACCLRM-4)
132KW
   (4) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access door 825.
   (5) Make sure that the access door 822 is open.
   (6) On the battery power center 105VU:
  • make sure that the protective cover is removed.
Subtask 27-92-16-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 12CE1 (ACCLRM1)
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
** ON A/C ALL
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
** ON A/C NOT FOR ALL
FOR FIN: 12CE2 (ACCLRM2)
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
** ON A/C ALL
105VUFLT CTL/SEC1/STBY SPLY22CEB01
FOR FIN: 12CE3 (ACCLRM3)
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
FOR FIN: 12CE4 (ACCLRM4)
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
4. Procedure
Subtask 27-92-16-860-050-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Do an inspection of the component interfaces and the adjacent area.
Subtask 27-92-16-420-051-A
B. Installation of the Flight Control Accelerometer
   (1) Install the accelerometer (1) on its mount (2).
   (2) Install the washers (4), the screws (5) and tighten them.
   (3) Remove the blanking cap from the electrical connector (3).
   (4) Connect the electrical connector (3) to the accelerometer (1).
Subtask 27-92-16-861-050-A
C. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 27-92-16-865-052-A
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 12CE1 (ACCLRM1)
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
** ON A/C ALL
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
** ON A/C NOT FOR ALL
FOR FIN: 12CE2 (ACCLRM2)
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
** ON A/C ALL
105VUFLT CTL/SEC1/STBY SPLY22CEB01
FOR FIN: 12CE3 (ACCLRM3)
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
FOR FIN: 12CE4 (ACCLRM4)
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
Subtask 27-92-16-865-053-A
E. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT FLP/POS/IND 11CNB12
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/FCDC1/SPLY20CE1B10
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT FLP/POS/IND 11CNB07
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/FCDC1/SPLY20CE1B05
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
105VUELEC/HOT BUS/702PP SPLY5PB2D02
105VUELEC/HOT BUS/701PP SPLY5PB1D01
105VUELEC/HOT BUS/702PP SPLY12PB2E02
105VUELEC/HOT BUS/701PP SPLY12PB1E01
** ON A/C NOT FOR ALL
121VUPTR/SPLY6TWJ21
121VUCFDS/TEST PLUG/210TWJ20
121VUCFDS/TEST PLUG/19TWJ19
121VUCFDS/CFDIU/SPLY2TWJ18
121VUCFDS/CFDIU/BACK/UP8TWJ17
121VUAUTO FLT/RUDDER/ARTF/FEEL14CAN17
121VUAUTO FLT/STICK/LOCK13CAN16
121VUFLIGHT CONTROLS/SLT FLP/2POS/IND2CNP16
** ON A/C ALL
121VUAUTO FLT/RUDDER/TRIM/IND15CCM20
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
121VUFLIGHT CONTROLS/WTB/FLP/SYS212CVP20
121VUFLIGHT CONTROLS/WTB/SLT/SYS211CVP19
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/FCDC2/SPLY20CE2Q20
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
** ON A/C NOT FOR ALL
121VUPTR/SPLY6TWJ44
121VUCFDS/TEST PLUG/210TWJ43
121VUCFDS/TEST PLUG/19TWJ42
121VUCFDS/CFDIU/SPLY2TWJ41
121VUCFDS/CFDIU/BACK/UP8TWJ40
121VUAUTO FLT/RUDDER/ARTF/FEEL14CAN19
121VUAUTO FLT/STICK/LOCK13CAN18
121VUFLIGHT CONTROLS/SLT FLP/2POS/IND2CNP21
** ON A/C ALL
122VUFLIGHT CONTROLS/WTB/FLP/SYS110CVS07
122VUFLIGHT CONTROLS/WTB/SLT/SYS19CVS06
Subtask 27-92-16-860-052-A
F. Aircraft Maintenance Configuration
   (1) 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).
   (2) 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).
Subtask 27-92-16-710-050-C
G. Do this test :
ACTION
RESULT
1.On the center pedestal, on one MCDU, push the MCDU MENU mode key.
The MCDU shows the MCDU MENU page.
2.Push the line key adjacent to the the CFDS indication.
The MCDU shows the CFDS MENU page.
3.Push the line key adjacent to the SYSTEM REPORT/TEST indication.
The MCDU shows the SYSTEM REPORT/TEST page.
4.Push the line key adjacent to the F/CTL indication.
The MCDU shows the F/CTL page.
5.Push the line key adjacent to the EFCS 1 indication.
The MCDU shows the EFCS 1 page.
6.Push the line key adjacent to the GROUND SCAN indication.
The MCDU shows the EFCS 1 GROUND SCAN page.
7.Push the line key adjacent to the START GROUND SCAN indication and wait two minutes.

8.Push the line key adjacent to the GROUND SCAN STOP indication.

9.Push the line key adjacent to the GROUND REPORT indication.
Make sure that the MCDU shows no accelerometers (12CE1,12CE2,12CE3,12CE4) failure message.
10.On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
The MCDU shows the MCDU MENU page.
5. Close-up
Subtask 27-92-16-410-050-A ** ON A/C NOT FOR ALL
A. Close Access
NOTE: If necessary, adjust the clock (Ref. AMM TASK 31-21-00-750-002).
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the sidewall panel:
     (a) FOR [12CE1] (ACCLRM-1), [12CE3] (ACCLRM-3)
131MW
     (b) FOR [12CE2] (ACCLRM-2), [12CE4] (ACCLRM-4)
132MW
   (3) Close the access door 825.
   (4) Install the protective cover on the battery power center 105VU.
   (5) Tighten the two screws.
   (6) Close the access door 822.
   (7) Remove the access platform(s).
   (8) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 27-92-16-410-050-B ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the sidewall panel:
     (a) FOR [12CE1] (ACCLRM-1), [12CE3] (ACCLRM-3)
131GW
     (b) FOR [12CE2] (ACCLRM-2), [12CE4] (ACCLRM-4)
132KW
   (3) Close the access door 825.
   (4) Install the protective cover on the battery power center 105VU.
   (5) Tighten the two screws.
   (6) Close the access door 822.
   (7) Remove the access platform(s).
   (8) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.03.31 23:58:39 UTC
"Aviabrain" 2025