W DOC AIRBUS | AMM A320F

Removal of the Avionics-Compartment Forward Door


TASK 52-41-11-000-001-A
Removal of the Avionics-Compartment Forward Door


CAUTION: THIS PART IS A REMOVABLE STRUCTURAL COMPONENT (RSC), WHICH CAN BE MOVED BETWEEN AIRCRAFT. THUS IT CAN HAVE DIFFERENT OPERATION CONDITIONS AND A DIFFERENT LIFE RECORD (FLIGHT HOURS/FLIGHT CYCLES/CALENDAR) FROM THE AIRCRAFT IT IS INSTALLED ON OR REMOVED FROM. THE OPERATOR IS RESPONSIBLE FOR THE SPECIFIC TRACKING AND CONTINUED AIRWORTHINESS OF REMOVABLE STRUCTURAL COMPONENTS. INCORRECT MAINTENANCE OF THESE COMPONENTS CAN CAUSE A RISK FOR THE FLIGHT SAFETY.
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
811
 C. Referenced Information
REFERENCE
DESIGNATION
3. Job Set-up
Subtask 52-41-11-865-050-A
A. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUEIS/SDAC1 AND 2/DOOR/DET/AVNCS46WVP02
Subtask 52-41-11-010-050-A
B. Get Access
   (1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at zone 120.
   (2) Open the door 811.
4. Procedure
Subtask 52-41-11-020-050-A
A. Removal of Avionics-Compartment Forward Door
   (1) Disconnect the bonding leads (2).
   (2) Remove and discard the cotter pins (3).
   (3) Remove the nuts (4) and the washer (9).
   (4) Hold the avionics-compartment forward door (1).
   (5) Remove the pins (7).
   (6) Remove the avionics-compartment forward door (1).
   (7) Remove the bushes (8), (5) and (6).
[Rev.10 from 2021] 2026.04.02 07:23:41 UTC