W DOC AIRBUS | AMM A320F

Removal of the Sliding Windows


TASK 56-12-11-000-001-A-02
Removal of the Sliding Windows


WARNING: YOU MUST MAKE SURE THAT YOU CAN HOLD THE COMPONENT BEFORE YOU REMOVE/INSTALL IT. THE COMPONENT IS HEAVY. IF IT FALLS, IT CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION: DO NOT USE SHARP AND/OR METALLIC TOOLS OR OBJECTS TO REMOVE/INSTALL THE WINDSHIELD OR A WINDOW. DO NOT USE A LEVER AGAINST THE EDGE OF THE WINDSHIELD OR WINDOW. IF YOU DO NOT OBEY THESE INSTRUCTIONS, YOU WILL CAUSE DAMAGE TO THE WINDSHIELD OR WINDOW.
ZONE: 211
ZONE: 212
FIN: 8DG1
FIN: 8DG2
1. Reason for the Job
NOTE: Two persons are necessary for this procedure.
NOTE: There are alternative procedures for the removal of the sliding windows. This task gives one of the procedures. For the other procedures, refer to the related task in this page block.
NOTE: This procedure is applicable to the glass windows (SGS supplier, P/N SPSA320-3-X-X or SPSA320-4-X-X).
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
SCRAPER - NON METALLIC
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
211
COCKPIT
212
COCKPIT
211BC, 211FC, 211GW, 211KC, 212BC, 212FC, 212GW, 212KC
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 25-13-41-000-803-A
Removal of the Personal Tablet Support
TASK 33-12-12-000-002-A
Removal of the Map Table Lights
TASK 33-12-12-000-003-A
Removal of the Reading Light
TASK 33-12-12-000-804-A
Removal of the Map Table Light
TASK 33-12-18-000-001-A
Removal of the Map Table Light Rheostats
TASK 33-12-18-000-802-A
Removal of the Map-Table Light Control-Box
TASK 46-26-22-000-001-A
Removal of the EFB Display Unit (DU)
TASK 46-26-22-000-002-A
Removal of the EFB Display Unit (DU) Mounting Bracket
TASK 56-12-11-000-803-C
Removal of the Structural Bracket Assembly
TASK 56-12-11-010-001-A
Opening of the Cockpit Sliding Windows
TASK 56-12-11-410-001-A
Closing of the Cockpit Sliding Windows
3. Job Set-up
Subtask 56-12-11-941-077-A
A. Get Access
   (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 210, in front of the sliding window.
Subtask 56-12-11-865-093-A
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUCOM NAV/RADAR/15SQ1K13
** ON A/C NOT FOR ALL
121VUCOM NAV/RADAR/25SQ2K14
** ON A/C ALL
FOR FIN: 8DG1 (WINDOWSLIDING, L)
122VUANTI ICE/WINDOWS/L4DG1X14
122VUANTI ICE/WHC/15DG1X13
123VUANTI ICE/L/WHSLD1DG1AF10
FOR FIN: 8DG2 (WINDOWSLIDING, R)
122VUANTI ICE/WINDOWS/R4DG2W14
122VUANTI ICE/WHC/25DG2W13
123VUANTI ICE/R/WHSLD1DG2AF03
Subtask 56-12-11-020-085-A ** ON A/C NOT FOR ALL
C. Removal of the Component
   (1) Remove the reading lights, if installed (Ref. AMM TASK 33-12-12-000-001):
     (a) FOR [8DG1] (WINDOW-SLIDING, L)
  • 25LE.
     (b) FOR [8DG2] (WINDOW-SLIDING, R)
  • 26LE.
   (2) Remove the personal tablet support, if installed (Ref. AMM D/O 25-13-41-00).
   (3) Remove the Electronic Flight Bag (EFB) Display Unit (DU), if installed (Ref. AMM D/O 46-26-22-00).
   (4) Remove the EFB DU mounting-bracket, if installed (Ref. AMM D/O 46-26-22-00).
Subtask 56-12-11-020-085-B ** ON A/C NOT FOR ALL
C. Removal of the Component
   (1) Remove the map table light (Ref. AMM TASK 33-12-12-000-002):
     (a) FOR [8DG1] (WINDOW-SLIDING, L)
  • 41LE.
     (b) FOR [8DG2] (WINDOW-SLIDING, R)
  • 42LE.
   (2) Remove the map-table light rheostats (Ref. AMM TASK 33-12-18-000-001):
     (a) FOR [8DG1] (WINDOW-SLIDING, L)
  • 39LE.
     (b) FOR [8DG1] (WINDOW-SLIDING, L)
  • 40LE.
   (3) Remove the personal tablet support, if installed (Ref. AMM D/O 25-13-41-00).
   (4) Remove the EFB DU, if installed (Ref. AMM TASK 46-26-22-000-001).
   (5) Remove the EFB DU mounting-bracket, if installed (Ref. AMM TASK 46-26-22-000-002).
Subtask 56-12-11-020-085-D ** ON A/C NOT FOR ALL
C. Removal of the Component
   (1) Remove the map table light (Ref. AMM TASK 33-12-12-000-804):
     (a) FOR [8DG1] (WINDOW-SLIDING, L)
  • 41LE.
     (b) FOR [8DG2] (WINDOW-SLIDING, R)
  • 42LE.
     (c) Remove the map-table light rheostats (Ref. AMM TASK 33-12-18-000-802)
       1 FOR [8DG1] (WINDOW-SLIDING, L)
  • 53LE.
       2 FOR [8DG1] (WINDOW-SLIDING, L)
  • 54LE.
     (d) Remove the personal tablet support, if installed (Ref. AMM TASK 25-13-41-000-803).
     (e) Remove the EFB DU, if installed (Ref. AMM TASK 46-26-22-000-001).
     (f) Remove the EFB DU mounting-bracket, if installed (Ref. AMM TASK 46-26-22-000-002).
4. Procedure
Subtask 56-12-11-020-086-A
A. Removal of the Lining Panels
   (1) Removal of the sliding window lining (16):
     (a) Open the sliding window (Ref. AMM TASK 56-12-11-010-001).
     (b) Remove the screw (5) and the pencil holder assembly (7).
     (c) Remove the screw (21) and the washer (20).
     (d) Remove the screw (19) and the washer (18).
     (e) Remove the handle (6).
     (f) Remove the screw (9) and the washer (8).
     (g) Remove the screw (15) and the washer (14).
     (h) Remove the guide (13).
     (i) Close the sliding window (Ref. AMM TASK 56-12-11-410-001).
     (j) Remove the blanking plug (4), the screw (3) and the washer (2).
     (k) Remove the screws (11) and (12).
     (l) Lift the plate (17).
     (m) Remove the sliding window lining (16).
     (n) Disconnect the electrical connector (10) from the receptacle.
     (o) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
     (p) Remove the structural bracket assembly, if installed (Ref. AMM TASK 56-12-11-000-803).
   (2) Removal of lining panel 211GW( 212GW) (48):
     (a) Remove the screws (41) and the washers (40).
     (b) Loosen the fasteners (42).
     (c) Disengage lining panel 211GW( 212GW) (48).
     (d) Remove the screw (45) and the washer (44).
     (e) Disengage the electrical cable (46).
     (f) Remove lining panel 211GW( 212GW) (48).
   (3) Removal of lining panel 211KC( 212KC) (29):
     (a) Remove lining panels 211BC( 212BC) and 211FC( 212FC) (29).
     (b) Loosen the fastener (1).
     (c) Remove the screws (24) and the washers (25) from the brackets (26).
     (d) Loosen the clamp (28) and disconnect the duct (27).
     (e) Remove lining panel 211KC( 212KC) (29).
Subtask 56-12-11-020-087-A
B. Removal of the Aft Upper Rail
   (1) Remove the bolts (54) and (55) and the nuts (57).
   (2) Remove the aft upper rail (56) from its support.
Subtask 56-12-11-020-088-A
WARNING: BE CAREFUL WHEN YOU REMOVE THE SLIDING WINDOW. THE HANDLE IS SPRING-LOADED AND WILL MOVE SUDDENLY WHEN YOU REMOVE THE SLIDING WINDOW FROM THE TRACK. IF YOU ARE NOT CAREFUL, THE HANDLE CAN HIT YOU.
C. Removal of the Sliding Window
   (1) Move the sliding window assembly (52) until it touches the rear stop.
   (2) Remove the sliding window assembly (52) from the rails (51) and (53).
   (3) When you remove the window, record the data in the IN-SERVICE WINDOW REMOVAL DATA GATHERING form to help Airbus continue to monitor it.
Subtask 56-12-11-110-067-A
D. Cleaning
   (1) Use the SCRAPER - NON METALLIC to remove the sealant from the aft upper rail (56) and from its support.
   (2) Clean the aft upper rail (56) and its support with the Non Aqueous Cleaner-General - - (Material No.08BAA9) and the Textile-Lint free Cotton - (Material No.14SBA1) .
[Rev.10 from 2021] 2026.04.01 02:07:17 UTC