W DOC AIRBUS | AMM A320F

Installation of Adjustable Stops and Roller Guides at the Emergency Exit Door


TASK 52-22-31-400-001-A
Installation of Adjustable Stops and Roller Guides at the Emergency Exit Door


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 833
ZONE: 834
ZONE: 835
ZONE: 843
ZONE: 844
ZONE: 845
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 4M (13 FT)-ADJUSTABLE
No specific
1
SCRAPER - PLASTIC
No specific
1
SCRAPER - WOODEN
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.06AAA1)
Polysulfide Sealant_General Purpose Brushable -
(Material No.06AAB1)
Polysulfide Sealant-General Purpose Fillet -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
833
EMERGENCY EXITS
834
EMERGENCY EXITS
835
MID PASSENGER/CREW DOOR
843
EMERGENCY EXITS
844
EMERGENCY EXITS
845
MID PASSENGER/CREW DOOR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
4
LOCK PLATE
AIPC 52-22-31-01-040
4
LOCK PLATE
AIPC 52-22-84-80-040
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 25-23-47-000-012-A
Removal of the Door Linings of the LH FWD Emergency Exit Door, zone 231
TASK 25-23-47-000-013-A
Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232.
TASK 25-23-47-000-802-A
Removal of the Door Linings of the Emergency Exit, zones 251/252
TASK 25-23-47-400-012-A
Installation of the Door Linings of the LH FWD Emergency Exit Door, zone 231
TASK 25-23-47-400-013-A
Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232.
TASK 25-23-47-400-802-A
Installation of the Door Linings of the Emergency Exit, zones 251/252
TASK 52-22-00-010-001-A
Opening of the Emergency Exit Doors from the Passenger Compartment
TASK 52-22-00-410-001-A
Closing of the Emergency Exit Doors from the Passenger Compartment
TASK 52-22-00-820-002-A
Adjustment of the Emergency Exit Door
TASK 52-22-00-860-003-A
Special Precaution before Maintenance on the Door Damper and Emergency Operation Cylinder
TASK 52-22-00-860-004-A
Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder
3. Job Set-up
Subtask 52-22-31-860-050-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the applicable emergency exit door (referred to as door) is opened as necessary (Ref. AMM TASK 52-22-00-010-001).
   (2) Make sure that the special precaution on the door damper and emergency operation cylinder is completed (Ref. AMM TASK 52-22-00-860-003).
   (3) Make sure that the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE is in position below the partly opened door.
   (4) Make sure that the applicable door linings are removed as necessary (Ref. AMM TASK 25-23-47-000-012) or (Ref. AMM TASK 25-23-47-000-013).
   (5) Make sure that the insulation mat is removed from the inner side of the door.
Subtask 52-22-31-860-050-B ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the applicable emergency exit door (referred to as door) is opened as necessary (Ref. AMM TASK 52-22-00-010-001).
   (2) Make sure that the special precaution on the door damper and emergency operation cylinder is completed (Ref. AMM TASK 52-22-00-860-003).
   (3) Make sure that the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE is in position below the partly opened door.
   (4) Make sure that the applicable door linings are removed as necessary (Ref. AMM TASK 25-23-47-000-802).
   (5) Make sure that the insulation mat is removed from the inner side of the door.
4. Procedure
Subtask 52-22-31-910-050-A ** ON A/C NOT FOR ALL
A. Preparation for Installation
   (1) Use a SCRAPER - PLASTIC or SCRAPER - WOODEN to remove the old sealant from the door frame, the stop fittings (5), the guide rollers (8) and the roller guides (11).
   (2) Clean the component interfaces and the adjacent area.
   (3) Do an inspection of the component interfaces and the adjacent area.
   (4) Apply a layer of Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the mating surface of the stop fittings (5), the guide rollers (8) and the roller guides (11).
   (5) Apply a layer of Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the mating surface of the bolts (1), (7) and (10) and the nuts (2), (9) and (12).
Subtask 52-22-31-420-050-A ** ON A/C NOT FOR ALL
B. Installation of the Adjustable Stops and the Roller Guides
   (1) Install the adjustable stops (5) as follows:
     (a) Put the stop fitting (5) in position at the door member and install it with the bolts (1) and the nuts (2).
     (b) Apply Polysulfide Sealant_General Purpose Brushable - (Material No.06AAA1) around the edges of the stop fitting (5).
     (c) If removed, install the stop bolt (6), the new AIPC 52-22-31-01-040 LOCK PLATE (4) or the new AIPC 52-22-84-80-040 LOCK PLATE (4) and the nut (3).
NOTE: Safety the nut (3) when the skin offset between the door and fuselage is correctly adjusted.
   (2) Install the guide rollers (8) as follows:
     (a) Put the guide roller (8) in position at the door member and attach it with the bolts (7) and the nuts (9).
     (b) Apply Polysulfide Sealant_General Purpose Brushable - (Material No.
06AAA1) around the edges of the guide roller (8).
   (3) Install the roller guides (11) as follows:
     (a) Put the roller guide (11) in position at the door member and attach it with the bolts (10) and the nuts (12).
     (b) Apply Polysulfide Sealant_General Purpose Brushable - (Material No.06AAA1) around the edges of the roller guide (11).
Subtask 52-22-31-820-050-A ** ON A/C NOT FOR ALL
C. Adjustment Procedure
   (1) Pre-adjust the adjustable stops as follows:
     (a) Measure the dimension "A" between the head of the stop bolt (6) and the surface of the stop fitting (5).
       1 The dimension "A" must be between 4.0 mm (0.157 in.) and 6.0 mm (0.236 in.).
     (b) If the dimension "A" is out of tolerance, loosen the nut (3) and turn the stop bolt (6) as necessary.
   (2) Make sure that the skin offset between the fuselage and the door is correctly adjusted (Ref. AMM TASK 52-22-00-820-002).
   (3) TORQUE the nut (3) to between 2.0 m.daN (14.75 lbf.ft) and 2.2 m.daN (16.22 lbf.ft).
   (4) Safety the nut (3) with the lock plate (4).
5. Close-up
Subtask 52-22-31-410-050-A ** 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) Put the insulation mat on the inner side of the door and attach it with the VELCRO tapes.
   (3) Install the door linings on the door (Ref. AMM TASK 25-23-47-400-012) or (Ref. AMM TASK 25-23-47-400-013).
   (4) Do the special precaution for the door damper and emergency operation cylinder (Ref. AMM TASK 52-22-00-860-004).
   (5) Close applicable the door (Ref. AMM TASK 52-22-00-410-001).
   (6) Remove the access platform(s).
Subtask 52-22-31-410-050-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) Put the insulation mat on the inner side of the door and attach it with the VELCRO tapes.
   (3) Install the door linings on the door (Ref. AMM TASK 25-23-47-400-802).
   (4) Do the special precaution for the door damper and emergency operation cylinder (Ref. AMM TASK 52-22-00-860-004).
   (5) Close the applicable door (Ref. AMM TASK 52-22-00-410-001).
   (6) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.02 06:27:44 UTC