Special Detailed Inspection (Endoscope) of Outboard Double Slotted Flap Tab Front Spar, LH/RH
TASK 57-53-00-220-021-A
Special Detailed Inspection (Endoscope) of Outboard Double Slotted Flap Tab Front Spar, LH/RH
Refer to the MPD TASK: 575323-01
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD DOUBLE SLOTTED FLAP TAB FRONT SPAR, 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 57-53-00-941-095-A ** ON A/C NOT FOR ALL
Subtask 57-53-00-280-068-A ** ON A/C NOT FOR ALL
Subtask 57-53-00-410-091-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:31:23 UTC
Special Detailed Inspection (Endoscope) of Outboard Double Slotted Flap Tab Front Spar, LH/RH
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
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.
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: 575323-01
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD DOUBLE SLOTTED FLAP TAB FRONT SPAR, 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 |
|---|---|
| 587 | FLAP N° 2 |
| 687 | FLAP N° 2 |
| 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) |
| SRM 575300 | (for corrective action) |
| NTM 575323 | (for corrective action) |
Subtask 57-53-00-941-095-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 57-53-00-865-137-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. Open, safety and tag this(these) circuit breaker(s):
Subtask 57-53-00-860-128-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) 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.
Subtask 57-53-00-010-092-A ** ON A/C NOT FOR ALL (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.
D. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable zone 587(687).
(2) Put the LIGHT SOURCE - SPARK-PROOF adjacent to the inspection area.
(3) Remove and discard the covers from the inspection holes in the lower surface of the tab.
(4) Make sure that the inspection holes are clear of unwanted material.
Subtask 57-53-00-110-093-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable zone 587(687).
(2) Put the LIGHT SOURCE - SPARK-PROOF adjacent to the inspection area.
(3) Remove and discard the covers from the inspection holes in the lower surface of the tab.
(4) Make sure that the inspection holes are clear of unwanted material.
E. Preparation for Inspection
(2) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean the applicable inspection area.
(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. ProcedureCAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
(1) Make sure that the inspection area is sufficiently clean to do the inspection of the area. - 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.
(2) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean the applicable inspection area.
(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).
Subtask 57-53-00-280-068-A ** ON A/C NOT FOR ALL
A. Special Detailed Inspection (Endoscope) of Outboard Double Slotted Flap Tab Front Spar, LH/RH
(1) Do a special detailed inspection of the internal surface of the front spar of the tab LH/RH. Refer to the NTM 575323 for the inspection procedure.
5. Close-up(1) Do a special detailed inspection of the internal surface of the front spar of the tab LH/RH. Refer to the NTM 575323 for the inspection procedure.
NOTE: If necessary, refer to the SRM 575300 for the correct repair procedure. If the defect is not included in this repair, you must request a procedure from AIRBUS.
Subtask 57-53-00-410-091-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Remove the spark-proof lamp from the inspection area.
(2) Use Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) , cut to the correct dimensions, to make new covers for the inspection holes.
(3) Install the new covers on the inspection holes.
(4) Make sure that the work area is clean and clear of tools and other items.
Subtask 57-53-00-865-138-A ** ON A/C NOT FOR ALL (1) Remove the spark-proof lamp from the inspection area.
(2) Use Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) , cut to the correct dimensions, to make new covers for the inspection holes.
(3) Install the new covers on the inspection holes.
(4) Make sure that the work area is clean and clear of tools and other items.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 57-53-00-860-127-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) Fully retract the flaps (Ref. AMM TASK 27-50-00-866-009).
Subtask 57-53-00-942-092-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) Fully 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) Make sure that the work area is clean and clear of tools and other items.
(1) Remove the access platform(s).
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Make sure that the work area is clean and clear of tools and other items.
Outboard Flap - Front Spar LH/RH - Inspection Area