W DOC AIRBUS | AMM A320F

Detailed Inspection of Outer Wing, Front Spar Forward Face, between Rib 8 and Rib 22, including all Cutouts

TASK 57-21-00-200-006-A
Detailed Inspection of Outer Wing, Front Spar Forward Face, between Rib 8 and Rib 22, including all Cutouts

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.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
WARNING: BEFORE YOU DO WORK IN OR NEAR A FUEL TANK, MAKE SURE THAT YOU OBEY ALL THE SAFETY PROCEDURES. THIS WILL PREVENT INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 522
ZONE: 622
1. Reason for the Job
Refer to the MPD TASK: 572101-01
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS
NOTE: The effectivity of this task is "ALL". To know if this task is applicable to your aircraft, refer to the MPD task applicability.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
1
LIGHT SOURCE - SPARK-PROOF
No specific
1
MIRROR - INSPECTION
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
522
OUTBOARD FIXED L.E STRUCTURE
622
OUTBOARD FIXED L.E STRUCTURE
522AB, 522CB, 522EB, 522FB, 522HB, 522JB, 522KB, 522LB, 522NB, 522QB, 622AB, 622CB, 622EB, 622FB, 622HB, 622JB, 622KB, 622LB, 622NB, 622QB
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 27-00-00-080-002-A
Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 27-00-00-480-002-A
Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 27-80-00-866-004-A
Extending the Slats on the Ground
TASK 27-80-00-866-005-A
Retracting the Slats on the Ground
TASK 51-78-00-916-001-A
Application of Temporary Protection System (TPS)
TASK 57-41-37-000-004-A
Removal of the Pressure Relief Panels
TASK 57-41-37-000-006-A
Removal of the Access Panels
TASK 57-41-37-000-012-A
Removal of the Access Panel
TASK 57-41-37-400-002-A
Installation of the Pressure Relief Panels
TASK 57-41-37-400-006-A
Installation of the Access Panels
TASK 57-41-37-400-012-A
Installation of the Access Panel
SRM 511100
SRM 512200
F Front-Spar Forward Face (all Cutouts Included) at the Outer Wing, between the Ribs 8 and 22
3. Job Set-up
Subtask 57-21-00-941-056-A
A. Safety Precautions
   (1) Put the WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the slats and flaps control lever.
   (2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 57-21-00-860-050-A
B. Aircraft Maintenance Configuration
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 slats (Ref. AMM TASK 27-80-00-866-004).
   (2) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is correctly installed on the slats and flaps control lever (Ref. AMM TASK 27-00-00-480-002).
Subtask 57-21-00-865-060-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 57-21-00-010-054-A
D. Get Access
   (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the wing leading edge, at the zone 522(622).
   (2) Remove the applicable access panels (Ref. AMM TASK 57-41-37-000-004), (Ref. AMM TASK 57-41-37-000-006) and (Ref. AMM TASK 57-41-37-000-012):
Subtask 57-21-00-110-109-A
E. 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 the inspection area is not sufficiently clean, clean it with the 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. Procedure
Subtask 57-21-00-110-055-A
DELETED
Subtask 57-21-00-210-060-A
B. Inspection
   (1) Examine the inspection area with the LIGHT SOURCE - SPARK-PROOF and the MIRROR - INSPECTION.
   (2) Do a detailed inspection of the front-spar forward face (all cutouts included) for damage or discontinuities. Do this inspection at the outer wing, between the ribs 8 and 22.
   (3) Make sure that there is no:
     (a) Corrosion:
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.
Subtask 57-21-00-916-058-A
CAUTION: DO NOT APPLY TEMPORARY PROTECTION SYSTEM (TPS) TYPE 3 ON THE MOVABLE COMPONENTS. USE ONLY TPS TYPE 1 GRADE 2. IF YOU DO NOT OBEY THIS INSTRUCTION, THE MECHANISMS WILL NOT OPERATE CORRECTLY.
C. Check and Application of the TPS Layer
NOTE: There is no special requirement about the TPS layer application in this area. The operator can apply TPS or let the surface stay without protection.
   (1) If you removed the TPS layer at the ”Preparation of the Inspection Area” paragraph, apply a TPS layer (Ref. AMM TASK 51-78-00-916-001).
   (2) If you did not remove the TPS layer at the ”Preparation of the Inspection Area” paragraph:
     (a) Do a check of the condition and integrity of the TPS layer (Ref. AMM TASK 51-78-00-916-001).
     (b) In relation to the condition and integrity of the TPS layer, apply a new TPS layer or not.
   (3) If the TPS layer has local damage, remove the damaged TPS layer and apply a new TPS layer (Ref. AMM TASK 51-78-00-916-001).
5. Close-up
Subtask 57-21-00-410-054-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the applicable access panels (Ref. AMM TASK 57-41-37-400-002), (Ref. AMM TASK 57-41-37-400-006) and (Ref. AMM TASK 57-41-37-400-012):
Subtask 57-21-00-865-061-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 57-21-00-866-058-A
C. Aircraft Maintenance Configuration
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) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the slats and flaps control lever (Ref. AMM TASK 27-00-00-080-002).
   (2) Remove the access platform(s).
   (3) Retract the slats (Ref. AMM TASK 27-80-00-866-005).
Subtask 57-21-00-942-055-A
D. Removal of Equipment
   (1) Remove the SAFETY BARRIERS.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 02:10:08 UTC
"Aviabrain" 2025