W DOC AIRBUS | AMM A320F

Removal of the Door Microswitch


TASK 25-45-33-000-001-A
Removal of the Door Microswitch


ZONE: 200
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
CAP - BLANKING
No specific
AR
ELEC CONTACTS INSERTION EXTRACTION TOOL M15.570-22
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
200
UPPER HALF FUSELAGE
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
3. Job Set-up
Subtask 25-45-33-861-050-A
A. Aircraft Maintenance Configuration
   (1) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
Subtask 25-45-33-865-059-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VULAV FWD-OCCUPIED1WJF01
** ON A/C ALL
2000VULIGHT-LAV1LQJ01
** ON A/C NOT FOR ALL
2000VULAV FWD & MID-OCCUPIED1WJF01
** ON A/C ALL
2001VULAVATORY AFT-OCCUPIED11WJB04
4. Procedure
Subtask 25-45-33-020-050-A
A. Removal of the Door Microswitch
   (1) Open the lavatory door to gain access to the door microswitch assembly (1).
   (2) Remove the screws (2).
   (3) Disconnect the electrical connector (4) as follows:
     (a) Carefully release the door microswitch assembly (1) from the door frame.
     (b) Disconnect the electrical connector (4).
NOTE: Use the Insertion/Extraction tool ELEC CONTACTS INSERTION EXTRACTION TOOL M15.570-22 to disconnect the electrical connector (3) type 'B'.
   (4) Remove the door microswitch assembly (1).
   (5) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
[Rev.10 from 2021] 2026.03.31 23:36:41 UTC