DOC AIRBUS | AMM A320FSpecial Detailed Inspection (ROTO) of Fwd Passenger/Crew Door Cutout, Stop Fittings Holes on FR 16 and FR 20 at Position 1 and 7, LH/RH
TASK 53-11-00-250-805-A
Special Detailed Inspection (ROTO) of Fwd Passenger/Crew Door Cutout, Stop Fittings Holes on FR 16 and FR 20 at Position 1 and 7, LH/RH
Refer to the MPD TASK: 531103-01
SPECIAL DETAILED INSPECTION (ROTO) OF FWD PASSENGER/CREW DOOR CUTOUT, STOP FITTINGS HOLES ON FR 16 AND FR 20 AT POSITION 1 AND 7, LH/RH.
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 53-11-00-010-127-A
Subtask 53-11-00-250-066-A
Subtask 53-11-00-410-126-A
[Rev.10 from 2021]
2026.04.02 06:28:46 UTC
Special Detailed Inspection (ROTO) of Fwd Passenger/Crew Door Cutout, Stop Fittings Holes on FR 16 and FR 20 at Position 1 and 7, LH/RH
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the JobRefer to the MPD TASK: 531103-01
SPECIAL DETAILED INSPECTION (ROTO) OF FWD PASSENGER/CREW DOOR CUTOUT, STOP FITTINGS HOLES ON FR 16 AND FR 20 AT POSITION 1 AND 7, LH/RH.
NOTE: The effectivity of this task is "ALL". To know if this task is applicable to your aircraft, refer to the MPD task applicability.
The information on weight variant groups is given in the MPD and SRM introductions.
2. Job Set-up InformationThe information on weight variant groups is given in the MPD and SRM introductions.
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.12ABC1) | Corrosion Preventive Compound_Water Displacing Soft Film - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 221 | FWD CAB UTILITY AREA |
| 222 | FWD CAB UTILITY AREA |
| 831, 841 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 25-23-45-000-002-A | Removal of the Door Frame Linings from the Right Forward Passenger/Crew Door |
| TASK 25-23-45-000-005-A | Removal of the Door Frame Linings from the Left Forward Passenger/Crew Door |
| TASK 25-23-45-400-006-A | Installation of the Door Frame Linings on the Left Forward Passenger/Crew Door |
| TASK 25-23-45-400-007-A | Installation of the Door Frame Linings on the Right Forward Passenger/Crew Door |
| TASK 25-80-00-000-001-A | Removal of the Insulation Blankets |
| TASK 25-80-00-400-001-A | Installation of the Insulation Blankets |
| TASK 51-78-00-916-001-A | Application of Temporary Protection System (TPS) |
| TASK 52-10-00-010-001-A | Opening of the Passenger/Crew Door |
| TASK 52-10-00-410-001-A | Closing of the Passenger/Crew Door |
| SRM 514200 | |
| NTM 531103 | |
| SRM 511100 | (for corrective action) |
| SRM 512200 | (for corrective action) |
| TASK 25-31-00-00 | FORWARD GALLEY - DESCRIPTION AND OPERATION |
| TASK 25-41-00-00 | FORWARD LAVATORIES - DESCRIPTION AND OPERATION |
Holes of the Stop Fittings at FR 16 and FR 20 at positions 1 and 7, Left and Right SideSubtask 53-11-00-010-127-A
A. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position.
(2) Open the passenger/crew doors 831 and ( 841) (Ref. AMM TASK 52-10-00-010-001).
(3) Remove the necessary door-frame lining panels at FR 16 and FR 20 to get access to the inspection area (Ref. AMM TASK 25-23-45-000-005) (Ref. AMM TASK 25-23-45-000-002).
(4) Remove the forward galleys and lavatories at FR 16 and FR 20, if installed.
To do this, refer to the para. Component Location in the applicable ATA 25 Description/Operation: for the galleys (Ref. AMM D/O 25-31-00-00), for the lavatories (Ref. AMM D/O 25-41-00-00). In this paragraph, you will find the cross-references of the removal/installation tasks.
(5) Remove the necessary insulation blankets at FR 16 and FR 20 to get access to the inspection area (Ref. AMM TASK 25-80-00-000-001).
Subtask 53-11-00-110-145-A (1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position.
(2) Open the passenger/crew doors 831 and ( 841) (Ref. AMM TASK 52-10-00-010-001).
(3) Remove the necessary door-frame lining panels at FR 16 and FR 20 to get access to the inspection area (Ref. AMM TASK 25-23-45-000-005) (Ref. AMM TASK 25-23-45-000-002).
(4) Remove the forward galleys and lavatories at FR 16 and FR 20, if installed.
To do this, refer to the para. Component Location in the applicable ATA 25 Description/Operation: for the galleys (Ref. AMM D/O 25-31-00-00), for the lavatories (Ref. AMM D/O 25-41-00-00). In this paragraph, you will find the cross-references of the removal/installation tasks.
(5) Remove the necessary insulation blankets at FR 16 and FR 20 to get access to the inspection area (Ref. AMM TASK 25-80-00-000-001).
B. Preparation of the Inspection Area
(1) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
(2) If not, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and the Textile-Lint free Cotton - (Material No.14SBA1) .
(3) If there is a TPS layer and if it does not let you do a satisfactory inspection, remove the TPS layer (Ref. AMM TASK 51-78-00-916-001).
(4) Remove the sealant and/or paint from the inspection area if this is necessary for the Nondestructive Testing Manual (NTM) task.
(5) Remove the fasteners to examine the holes ( SRM 514200).
4. Procedure(1) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
(2) If not, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and the Textile-Lint free Cotton - (Material No.14SBA1) .
(3) If there is a TPS layer and if it does not let you do a satisfactory inspection, remove the TPS layer (Ref. AMM TASK 51-78-00-916-001).
(4) Remove the sealant and/or paint from the inspection area if this is necessary for the Nondestructive Testing Manual (NTM) task.
(5) Remove the fasteners to examine the holes ( SRM 514200).
Subtask 53-11-00-250-066-A
A. Inspection
(1) Do a special detailed inspection (ROTO) of the holes of the stop fittings of the forward passenger/crew door cutout. This inspection is applicable at FR 16 and FR 20 at positions 1 and 7. Do this inspection for damage or discontinuities on the left and right sides. Refer to NTM 531103.
(2) Make a report of the damage after the NTM inspection:
(a) Corrosion damage:
Subtask 53-11-00-420-078-A (1) Do a special detailed inspection (ROTO) of the holes of the stop fittings of the forward passenger/crew door cutout. This inspection is applicable at FR 16 and FR 20 at positions 1 and 7. Do this inspection for damage or discontinuities on the left and right sides. Refer to NTM 531103.
(2) Make a report of the damage after the NTM inspection:
(a) Corrosion damage:
- If you find corrosion, refer to the Structural Repair Manual ( SRM 512200) for the corrosion types, inspection, removal and subsequent corrosion protection.
- If you find this type of damage, refer to the Structural Repair Manual ( SRM 511100) for the damage types, classification and corrective action.
B. Installation of the Components
(1) Refer to the installation drawing in the SRM identification section for the new fastener references.
(2) Install the fasteners of the examined holes ( SRM 514200).
Subtask 53-11-00-916-078-A (1) Refer to the installation drawing in the SRM identification section for the new fastener references.
(2) Install the fasteners of the examined holes ( SRM 514200).
C. Check and Application of the TPS Layer
(1) If the TPS was removed at the "Preparation of the Inspection Area", apply a new layer of Corrosion Preventive Compound_Water Displacing Soft Film - (Material No.12ABC1) (Ref. AMM TASK 51-78-00-916-001).
(2) If the TPS was not removed at the "Preparation of the Inspection Area", do a check of the condition and integrity of the TPS layer (Ref. AMM TASK 51-78-00-916-001).
(3) If the TPS layer has local damage, remove the damaged TPS layer and apply a new layer of Corrosion Preventive Compound_Water Displacing Soft Film - (Material No.12ABC1) (Ref. AMM TASK 51-78-00-916-001).
5. Close-up(1) If the TPS was removed at the "Preparation of the Inspection Area", apply a new layer of Corrosion Preventive Compound_Water Displacing Soft Film - (Material No.12ABC1) (Ref. AMM TASK 51-78-00-916-001).
(2) If the TPS was not removed at the "Preparation of the Inspection Area", do a check of the condition and integrity of the TPS layer (Ref. AMM TASK 51-78-00-916-001).
(3) If the TPS layer has local damage, remove the damaged TPS layer and apply a new layer of Corrosion Preventive Compound_Water Displacing Soft Film - (Material No.12ABC1) (Ref. AMM TASK 51-78-00-916-001).
NOTE: If the TPS layer is not in the correct condition, Airbus recommends that you apply a new layer (as a spray) on the existing layer. This is to make sure that the TPS layer continues to give satisfactory corrosion protection.
Subtask 53-11-00-410-126-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the insulation blankets at FR 16 and FR 20 (Ref. AMM TASK 25-80-00-400-001).
(3) Install the forward galleys and lavatories at FR 16 and FR 20, if removed.
To do this, refer to the para. Component Location in the applicable ATA 25 Description/Operation: for the galleys (Ref. AMM D/O 25-31-00-00), for the lavatories (Ref. AMM D/O 25-41-00-00). In this paragraph, you will find the cross-references of the removal/installation tasks.
(4) Install the door frame lining panels at FR 16 and FR 20 (Ref. AMM TASK 25-23-45-400-006) (Ref. AMM TASK 25-23-45-400-007).
(5) Close the passenger/crew doors 831 and ( 841) (Ref. AMM TASK 52-10-00-410-001).
(6) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the insulation blankets at FR 16 and FR 20 (Ref. AMM TASK 25-80-00-400-001).
(3) Install the forward galleys and lavatories at FR 16 and FR 20, if removed.
To do this, refer to the para. Component Location in the applicable ATA 25 Description/Operation: for the galleys (Ref. AMM D/O 25-31-00-00), for the lavatories (Ref. AMM D/O 25-41-00-00). In this paragraph, you will find the cross-references of the removal/installation tasks.
(4) Install the door frame lining panels at FR 16 and FR 20 (Ref. AMM TASK 25-23-45-400-006) (Ref. AMM TASK 25-23-45-400-007).
(5) Close the passenger/crew doors 831 and ( 841) (Ref. AMM TASK 52-10-00-410-001).
(6) Remove the access platform(s).