DOC AIRBUS | AMM A320FDetailed Inspection of Outer Wing, Top Skin, Lower Surface, Overhang from RIB 8 to RIB 11
TASK 57-21-00-220-811-A
Detailed Inspection of Outer Wing, Top Skin, Lower Surface, Overhang from RIB 8 to RIB 11
Refer to the MPD TASK: 572178-01
DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWER SURFACE, OVERHANG FROM RIB 8 TO RIB 11
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 57-21-00-941-118-A
Subtask 57-21-00-220-062-A
Subtask 57-21-00-410-101-A
[Rev.10 from 2021]
2026.04.01 02:11:00 UTC
Detailed Inspection of Outer Wing, Top Skin, Lower Surface, Overhang from RIB 8 to RIB 11
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:
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: 572178-01
DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWER SURFACE, OVERHANG FROM RIB 8 TO RIB 11
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 InformationA. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| 98D27803500001 | 1 | LOCKING TOOL ZERO POS |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.12ABB1) | Corrosion Preventive Compound-Water Displacing Hard Film - |
| (Material No.12ACB1) | Corrosion Preventive Compound-Heavy Duty Hard Film - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 574 | FALSE SPAR BOX |
| 575 | AFT OUTBD SE OF WING AND TE FIXED STRUCT |
| 674 | FALSE SPAR BOX |
| 675 | AFT OUTBD SE OF WING AND TE FIXED STRUCT |
| 573CB, 573EB, 573FB, 575AB, 673CB, 673EB, 673FB, 675AB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 51-78-00-916-001-A | Application of Temporary Protection System (TPS) |
| TASK 57-51-37-000-002-A | Removal of the Access Panels 571AB(671AB), 573AB(673AB), 573BB(673BB), 573CB(673CB), 573EB(673EB) |
| TASK 57-51-37-000-003-A | Removal of the Access Panel |
| TASK 57-51-37-000-004-A | Removal of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB) |
| TASK 57-51-37-400-002-A | Installation of the Access Panels 571AB(671AB), 573AB(673AB), 573BB(673BB), 573CB(673CB), 573EB(673EB) |
| TASK 57-51-37-400-003-A | Installation of the Access Panel |
| TASK 57-51-37-400-004-A | Installation of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB) |
| SRM 511100 | (for corrective action) |
| SRM 512200 | (for corrective action) |
| SRM 512300 | (for corrective action) |
Outer Wing, Top Skin, Lower Surface, Overhang from RIB 8 to RIB 11Subtask 57-21-00-941-118-A
A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat lever.
(3) Put a WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-21-00-010-110-A (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat lever.
(3) Put a WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
B. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below zone 575(675).
(2) Remove the applicable access panels (Ref. AMM TASK 57-51-37-000-002) (Ref. AMM TASK 57-51-37-000-003) (Ref. AMM TASK 57-51-37-000-004):
(a) For the left wing: 573CB, 573EB, 573FB and 575AB
(b) For the right wing: 673CB, 673EB, 673FB and 675AB.
Subtask 57-21-00-110-106-A (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below zone 575(675).
(2) Remove the applicable access panels (Ref. AMM TASK 57-51-37-000-002) (Ref. AMM TASK 57-51-37-000-003) (Ref. AMM TASK 57-51-37-000-004):
(a) For the left wing: 573CB, 573EB, 573FB and 575AB
(b) For the right wing: 673CB, 673EB, 673FB and 675AB.
C. 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 a 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. 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 a 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).
Subtask 57-21-00-220-062-A
A. Inspection
(1) Do a detailed inspection of the outer wing, top skin, lower surface, overhang from RIB 8 to RIB 11, for damage or discontinuities.
(2) Make sure that there is no:
(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.
(b) Other damage (scratches, cracks, gouges, dents, creases):
If you find this type of damage, refer to the Structural Repair Manual ( SRM 511100) for the damage types, classification and corrective action.
(c) Paint layer damage:
If you find this type of damage, refer to the Structural Repair Manual ( SRM 512300) for general data for paint layers.
Subtask 57-21-00-916-055-A (1) Do a detailed inspection of the outer wing, top skin, lower surface, overhang from RIB 8 to RIB 11, for damage or discontinuities.
(2) Make sure that there is no:
(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.
(b) Other damage (scratches, cracks, gouges, dents, creases):
If you find this type of damage, refer to the Structural Repair Manual ( SRM 511100) for the damage types, classification and corrective action.
(c) Paint layer damage:
If you find this type of damage, refer to the Structural Repair Manual ( SRM 512300) for general data for paint layers.
B. 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 Hard Film - (Material No.12ABB1) or a layer of Corrosion Preventive Compound-Heavy Duty Hard Film - (Material No.12ACB1) (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 Hard Film - (Material No.12ABB1) or a layer of Corrosion Preventive Compound-Heavy Duty Hard Film - (Material No.12ACB1) (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 Hard Film - (Material No.12ABB1) or a layer of Corrosion Preventive Compound-Heavy Duty Hard Film - (Material No.12ACB1) (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 Hard Film - (Material No.12ABB1) or a layer of Corrosion Preventive Compound-Heavy Duty Hard Film - (Material No.12ACB1) (Ref. AMM TASK 51-78-00-916-001).
NOTE: If, after the check of the condition and integrity, the TPS layer is 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 57-21-00-410-101-A
A. Close Access
(1) Install the applicable access panels (Ref. AMM TASK 57-51-37-400-002) (Ref. AMM TASK 57-51-37-400-003) (Ref. AMM TASK 57-51-37-400-004):
(a) For the left wing: 573CB, 573EB, 573FB and 575AB
(b) For the right wing: 673CB, 673EB, 673FB and 675AB.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Remove the access platform(s).
Subtask 57-21-00-942-113-A (1) Install the applicable access panels (Ref. AMM TASK 57-51-37-400-002) (Ref. AMM TASK 57-51-37-400-003) (Ref. AMM TASK 57-51-37-400-004):
(a) For the left wing: 573CB, 573EB, 573FB and 575AB
(b) For the right wing: 673CB, 673EB, 673FB and 675AB.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Remove the access platform(s).
B. Removal of Equipment
(1) Remove the SAFETY BARRIER(S).
(2) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(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 SAFETY BARRIER(S).
(2) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.