DOC AIRBUS | AMM A320FInstallation of Service Door 172AR
TASK 52-42-11-400-001-A
Installation of Service Door 172AR
Self explanatory
2. Job Set-up Information
A. Consumable Materials
B. Work Zones and Access Panels
C. Expendable Parts
D. Referenced Information
3. Job Set-up
Subtask 52-42-11-860-050-A
Subtask 52-42-11-420-050-C
Subtask 52-42-11-410-050-A
[Rev.10 from 2021]
2026.04.02 07:23:48 UTC
Installation of Service Door 172AR
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 170
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Consumable Materials
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.06AAA1) | Polysulfide Sealant_General Purpose Brushable - |
| (Material No.06AAC1) | Polysulfide Sealant-General Purpose Interfay - |
| (Material No.06ABC1) | Polysulfide Sealant-Fuel Tank Interfay - |
| (Material No.06AEA1) | Polysulfide Sealant-Low Adhesion Brushable - |
| (Material No.06CMD9) | Silicone Adhesive Sealant-General Purpose One part legacy |
| (Material No.08BBD1) | Non Aqueous Cleaner-- Isopropyl Alcohol - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 170 | AFT CAB U/FLOOR COMPT AFT BHD OF BULK |
| 172AR |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 9 | JOINT | AIPC 52-42-11-01-030 |
| 10 | JOINT | AIPC 52-42-11-01-040 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 20-28-00-912-802-A | Electrical Bonding - General Maintenance Procedure |
| TASK 20-28-00-912-803-A | Bonding Surface Preparation |
Service Door 172ARSubtask 52-42-11-860-050-A
A. Get Access
(1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at zone 172.
4. Procedure(1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at zone 172.
Subtask 52-42-11-420-050-C
A. Installation of Service Door 172AR
(1) Make sure that the parts retained from the removed component are clean and in the correct condition.
(2) Do a visual inspection of the component interfaces and the adjacent area.
(3) Make sure that the joints (9) and (10) are in the correct condition.
(4) If they are not, replace them as follows:
(a) Remove the joints (9) and (10).
(b) Apply Silicone Adhesive Sealant-General Purpose One part legacy (Material No.06CMD9) on the mating surface between service door 172AR (1) and the joints (9) and (10).
(c) Install the new AIPC 52-42-11-01-030 JOINT (9) and the new AIPC 52-42-11-01-040 JOINT (10).
(5) Clean the component interfaces and/or the adjacent area with the Textile-Lint free Cotton - (Material No.14SBA1) and Non Aqueous Cleaner-- Isopropyl Alcohol - (Material No.08BBD1) .
(6) Apply Polysulfide Sealant-Fuel Tank Interfay - (Material No.06ABC1) or Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) on the mating surface between the steel and the aluminum components. You can apply the sealant on the hinges of service door 172AR (1), the shims (2) and the springs (3).
(7) Put service door 172AR (1) in position on the fuselage cutout.
(8) Install the springs (3), the shims (2) and the screws (6).
(9) Tighten the screws (6).
(10) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant_General Purpose Brushable - (Material No.06AAA1) on the heads of the screws (6) and around the door fitting.
(11) Prepare the surface of the bonding point(s)
(Ref. AMM TASK 20-28-00-912-803).
(12) Install the bonding leads (5), the washers (7), the bolts (8) and the nuts (4) on the hinges of service door 172AR (1).
(13) Tighten the nuts (4).
(14) Do the electrical resistance measurement and the final protection of the bonding point(s)
(Ref. AMM TASK 20-28-00-912-802).
5. Close-up(1) Make sure that the parts retained from the removed component are clean and in the correct condition.
(2) Do a visual inspection of the component interfaces and the adjacent area.
(3) Make sure that the joints (9) and (10) are in the correct condition.
(4) If they are not, replace them as follows:
(a) Remove the joints (9) and (10).
(b) Apply Silicone Adhesive Sealant-General Purpose One part legacy (Material No.06CMD9) on the mating surface between service door 172AR (1) and the joints (9) and (10).
(c) Install the new AIPC 52-42-11-01-030 JOINT (9) and the new AIPC 52-42-11-01-040 JOINT (10).
(5) Clean the component interfaces and/or the adjacent area with the Textile-Lint free Cotton - (Material No.14SBA1) and Non Aqueous Cleaner-- Isopropyl Alcohol - (Material No.08BBD1) .
(6) Apply Polysulfide Sealant-Fuel Tank Interfay - (Material No.06ABC1) or Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) on the mating surface between the steel and the aluminum components. You can apply the sealant on the hinges of service door 172AR (1), the shims (2) and the springs (3).
(7) Put service door 172AR (1) in position on the fuselage cutout.
(8) Install the springs (3), the shims (2) and the screws (6).
(9) Tighten the screws (6).
(10) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant_General Purpose Brushable - (Material No.06AAA1) on the heads of the screws (6) and around the door fitting.
(11) Prepare the surface of the bonding point(s)
(Ref. AMM TASK 20-28-00-912-803).
(12) Install the bonding leads (5), the washers (7), the bolts (8) and the nuts (4) on the hinges of service door 172AR (1).
(13) Tighten the nuts (4).
(14) Do the electrical resistance measurement and the final protection of the bonding point(s)
(Ref. AMM TASK 20-28-00-912-802).
Subtask 52-42-11-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close service door 172AR.
(3) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close service door 172AR.
(3) Remove the access platform(s).