DOC AIRBUS | AMM A320FSpecial Detailed Inspection of Inboard Double Slotted Flap, Internal Support Brackets of Pylon Aft Fairing Attachment, LH/RH
TASK 57-52-00-220-011-A
Special Detailed Inspection of Inboard Double Slotted Flap, Internal Support Brackets of Pylon Aft Fairing Attachment, LH/RH
Refer to the MPD TASK: 575230-01
SPECIAL DETAILED INSPECTION (ENDOSCOPE) INBOARD DOUBLE-SLOTTED FLAP, INTERNAL SUPPORT BRACKETS PYLON AFT FAIRING ATTACHMENT, LH/RH
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 57-52-00-941-074-A ** ON A/C NOT FOR ALL
Subtask 57-52-00-410-074-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:31:17 UTC
Special Detailed Inspection of Inboard Double Slotted Flap, Internal Support Brackets of Pylon Aft Fairing Attachment, LH/RH
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
CAUTION:
DO NOT APPLY TEMPORARY PROTECTION SYSTEM (TPS) ON THE INSPECTION AREA. IF YOU APPLY TPS ON THE INSPECTION AREA, YOU CAN CAUSE DAMAGE TO THE AIRCRAFT.
1. Reason for the JobRefer to the MPD TASK: 575230-01
SPECIAL DETAILED INSPECTION (ENDOSCOPE) INBOARD DOUBLE-SLOTTED FLAP, INTERNAL SUPPORT BRACKETS PYLON AFT FAIRING ATTACHMENT, LH/RH
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE |
| No specific | AR | LIGHT SOURCE - SPARK-PROOF |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.05RAB9) | Adhesive Film Tape-- Aluminium Foil - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 581 | FLAP N° 1 |
| 681 | FLAP N° 1 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 27-50-00-866-008-A | Extension of the Flaps on the Ground |
| TASK 27-50-00-866-008-A-01 | Extension of the Flaps/Slats on the Ground |
| TASK 27-50-00-866-009-A | Retraction of the Flaps on the Ground |
| TASK 27-50-00-866-009-A-01 | Retraction of the Flaps/Slats on the Ground |
| TASK 51-78-00-916-001-A | Application of Temporary Protection System (TPS) |
| NTM 575230 | |
| SRM 575200 | (for corrective action) |
Inboard Flap - Pylon Fairing Internal Support Brackets - Inspection AreaSubtask 57-52-00-941-074-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) Put a WARNING NOTICE(S) on the flap/slat control lever (panel 114VU) to tell persons not to operate the flaps.
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 57-52-00-860-063-A ** ON A/C NOT FOR ALL (1) Put a WARNING NOTICE(S) on the flap/slat control lever (panel 114VU) to tell persons not to operate the flaps.
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
B. Aircraft Maintenance Configuration
(2) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is installed on the flap/slat control lever on the panel 114VU.
Subtask 57-52-00-865-097-A ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Fully extend the flaps (Ref. AMM TASK 27-50-00-866-008). (2) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is installed on the flap/slat control lever on the panel 114VU.
C. Open, safety and tag this(these) circuit breaker(s):
Subtask 57-52-00-010-072-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
D. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the Rib 12 of the inboard flap at zone 581(681).
(2) Remove and discard the covers to the inspection holes in the lower skin each side of the Rib 12.
(3) Make sure that the applicable inspection holes are clear of unwanted material.
(4) Put the LIGHT SOURCE - SPARK-PROOF adjacent to the inspection area.
Subtask 57-52-00-110-077-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the Rib 12 of the inboard flap at zone 581(681).
(2) Remove and discard the covers to the inspection holes in the lower skin each side of the Rib 12.
(3) Make sure that the applicable inspection holes are clear of unwanted material.
(4) Put the LIGHT SOURCE - SPARK-PROOF adjacent to the inspection area.
E. Preparation of the Inspection Area
(1) Make sure that the inspection area is sufficiently clean to do the inspection of the area.
(2) If necessary, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and a Textile-Lint free Cotton - (Material No.14SBA1) .
(3) Make sure that there is no TPS layer and if there is a TPS layer, remove it (Ref. AMM TASK 51-78-00-916-001).
4. Procedure(1) Make sure that the inspection area is sufficiently clean to do the inspection of the area.
(2) If necessary, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and a Textile-Lint free Cotton - (Material No.14SBA1) .
(3) Make sure that there is no TPS layer and if there is a TPS layer, remove it (Ref. AMM TASK 51-78-00-916-001).
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
Subtask 57-52-00-280-059-A ** ON A/C NOT FOR ALL - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
A. Special Detailed Inspection of Inboard Double Slotted Flap, Internal Support Brackets of Pylon Aft Fairing Attachment, LH/RH
(1) Do a special detailed inspection of the internal support brackets of the pylon aft fairing attachment LH/RH NTM 575230.
5. Close-up(1) Do a special detailed inspection of the internal support brackets of the pylon aft fairing attachment LH/RH NTM 575230.
NOTE: If necessary, refer to the SRM 575200 for the correct repair procedure. If the defect is not included in this repair, you must request a procedure from AIRBUS.
Subtask 57-52-00-410-074-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Remove the LIGHT SOURCE - SPARK-PROOF from the inspection area.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Use Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) , cut to the correct dimensions, to make new covers for the inspection holes.
(4) Install the new covers on the inspection holes.
Subtask 57-52-00-865-098-A ** ON A/C NOT FOR ALL (1) Remove the LIGHT SOURCE - SPARK-PROOF from the inspection area.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Use Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) , cut to the correct dimensions, to make new covers for the inspection holes.
(4) Install the new covers on the inspection holes.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 57-52-00-860-064-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
C. Aircraft Maintenance Configuration
(1) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap/slat control lever.
(2) Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
Subtask 57-52-00-942-073-A ** ON A/C NOT FOR ALL (1) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap/slat control lever.
(2) Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
D. Removal of Equipment
(1) Remove the access platform(s).
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the access platform(s).
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.