W DOC AIRBUS | AMM A320F

Removal of the Flight Control Accelerometer


TASK 27-92-16-000-001-A
Removal 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
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 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
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 27-92-16-010-050-A ** ON A/C NOT FOR ALL
A. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 825.
   (2) Open the access door 825.
   (3) Remove the sidewall panel :
     (a) FOR [12CE1] (ACCLRM-1), [12CE3] (ACCLRM-3)
131MW
     (b) FOR [12CE2] (ACCLRM-2), [12CE4] (ACCLRM-4)
132MW
   (4) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
   (5) Open the access door 822
   (6) At the battery power center 105VU:
  • loosen the two screws and remove the protective cover.
Subtask 27-92-16-010-050-B ** ON A/C NOT FOR ALL
A. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 825.
   (2) Open the access door 825.
   (3) Remove the sidewall panel :
     (a) FOR [12CE1] (ACCLRM-1), [12CE3] (ACCLRM-3)
131GW
     (b) FOR [12CE2] (ACCLRM-2), [12CE4] (ACCLRM-4)
132KW
   (4) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
   (5) Open the access door 822
   (6) At the battery power center 105VU:
  • loosen the two screws and remove the protective cover.
Subtask 27-92-16-865-050-A
B. Open, safety and tag 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
4. Procedure
Subtask 27-92-16-020-050-A
A. Removal of the Flight Control Accelerometer
   (1) Disconnect the electrical connector (3) from the accelerometer (1).
   (2) Put CAP - BLANKING on the electrical connectors (3) and (6).
   (3) Remove the screws (5) and the washers (4).
   (4) Remove the accelerometer (1).
[Rev.10 from 2021] 2026.03.31 23:58:38 UTC