Special Detailed Inspection (US) of Outer Wing Box, Upper Surface of Triform Fitting (on First Row of Fasteners from RIB1), between STRG 8 and FR42, LH/RH
TASK 57-10-00-200-024-A
Special Detailed Inspection (US) of Outer Wing Box, Upper Surface of Triform Fitting (on First Row of Fasteners from RIB1), between STRG 8 and FR42, LH/RH
Refer to the MPD TASK: 571182-01
SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX, UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, 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 57-10-00-941-066-A
Subtask 57-10-00-270-051-A
Subtask 57-10-00-390-051-A
[Rev.10 from 2021]
2026.04.02 06:30:30 UTC
Special Detailed Inspection (US) of Outer Wing Box, Upper Surface of Triform Fitting (on First Row of Fasteners from RIB1), between STRG 8 and FR42, 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:
DO NOT GET FUEL IN YOUR MOUTH, EYES OR ON YOUR SKIN. DO NOT BREATHE THE FUMES FROM THE FUEL. KEEP THE FUEL AWAY FROM SPARKS, FLAME AND HEAT. FUEL IS POISONOUS AND FLAMMABLE, WHICH CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
BEFORE YOU INSTALL/REMOVE THE GSE-TOOL, READ THE INSTRUCTIONS IN THE APPLICABLE GSE INSTRUCTION MANUAL. WHILE YOU OPERATE THIS TOOL, CAREFULLY OBEY THEM. IF YOU DO NOT OBEY THE INSTRUCTIONS, DAMAGE TO EQUIPMENT CAN OCCUR.
1. Reason for the JobRefer to the MPD TASK: 571182-01
SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX, UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, 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 and the weight variant data given in the SRM introduction.
2. Job Set-up InformationA. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 2M (6 FT) |
| No specific | AR | FLASHLIGHT |
| No specific | AR | WARNING NOTICE(S) |
| 98D27803500001 | 1 | LOCKING TOOL ZERO POS |
| 98D57004013000 | 2 | HOOK-COVER (RIB 2 SURGE DOORS) |
| 98D57004014000 | 2 | HOOK-COVER (RIB2-SURGE DOORS) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 540 | FUEL TANK |
| 640 | FUEL TANK |
| 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 28-00-00-910-001-A | Fuel Safety Procedures |
| TASK 51-76-12-300-002-A | Repair of the Fuel Tank Fillet |
| TASK 57-27-11-000-001-A | Removal of the Access Panel |
| TASK 57-27-11-400-001-A | Installation of the Access Panel |
| SRM 517612 | |
| NTM 571182 | |
| SRM 511100 | (for corrective action) |
| SRM 512200 | (for corrective action) |
Subtask 57-10-00-941-066-A
A. Safety Precautions
(1) On FLAPS panel 114VU:
(a) Put the 98D27803500001 LOCKING TOOL ZERO POS in position on the flap/slat control lever.
(b) Put a WARNING NOTICE(S) on the flap/slat control lever to tell persons not to operate the flap/slat control lever.
(2) Obey the fuel safety precautions (Ref. AMM TASK 28-00-00-910-001).
Subtask 57-10-00-010-079-A (1) On FLAPS panel 114VU:
(a) Put the 98D27803500001 LOCKING TOOL ZERO POS in position on the flap/slat control lever.
(b) Put a WARNING NOTICE(S) on the flap/slat control lever to tell persons not to operate the flap/slat control lever.
(2) Obey the fuel safety precautions (Ref. AMM TASK 28-00-00-910-001).
B. Get Access
(1) Put an ACCESS PLATFORM 2M (6 FT) in position in zone 540 (640).
(2) Remove the access panels (Ref. AMM TASK 57-27-11-000-001):
(3) Open the RIB2 surge doors:
(4) Install the 98D57004013000 HOOK-COVER (RIB 2 SURGE DOORS) on the forward surge doors.
(5) Install the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) on the aft surge doors.
(6) Use a FLASHLIGHT for the inspection.
Subtask 57-10-00-110-068-A (1) Put an ACCESS PLATFORM 2M (6 FT) in position in zone 540 (640).
(2) Remove the access panels (Ref. AMM TASK 57-27-11-000-001):
(3) Open the RIB2 surge doors:
(4) Install the 98D57004013000 HOOK-COVER (RIB 2 SURGE DOORS) on the forward surge doors.
(5) Install the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) on the aft surge doors.
(6) Use a FLASHLIGHT for the inspection.
C. Preparation for the Inspection Area
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
(1) Remove the sealant from the fasteners (10) between STGR8 to FR42.
(2) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
(3) If it is not sufficiently clean, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and Textile-Lint free Cotton - (Material No.14SBA1) .
(4) Do a visual check of the inspection area for damage or discontinuities.
(5) Make sure that there is no:
(a) Corrosion damage:
4. Procedure
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL (2) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
(3) If it is not sufficiently clean, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and Textile-Lint free Cotton - (Material No.14SBA1) .
(4) Do a visual check of the inspection area for damage or discontinuities.
(5) Make sure that there is no:
(a) Corrosion damage:
- If you find corrosion damage, refer to Structural Repair Manual SRM 512200 for types of corrosion, inspection, removal and corrosion protection.
- If you find this type of damage, refer to Structural Repair Manual SRM 511100 for damage classification and corrective action.
Subtask 57-10-00-270-051-A
A. Inspection
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
(1) Do a special detailed inspection (US) of the first row of the fasteners (10) in the wing tank. This inspection is applicable from RIB1 of the upper surface of the fitting (11), between STGR8 and FR42 (left and right sides). Refer to Non-destructive Testing Manual NTM 571182.
(2) Make a report of damage after NDT inspection:
(a) Corrosion damage:
5. Close-up
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL (2) Make a report of damage after NDT inspection:
(a) Corrosion damage:
- If you find corrosion damage, refer to Structural Repair Manual SRM 512200 for types of corrosion, inspection, removal and corrosion protection.
- If you find this type of damage, refer to Structural Repair Manual SRM 511100 for damage classification and corrective action.
Subtask 57-10-00-390-051-A
A. Sealant Application
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
(1) Clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and Textile-Lint free Cotton - (Material No.14SBA1) .
(2) Apply sealant on the fasteners (10) between STGR8 to FR42, refer to Structural Repair Manual SRM 517612 and (Ref. AMM TASK 51-76-12-300-002).
Subtask 57-10-00-410-077-A
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL
Inspection (US) of the Fasteners on the Upper Surface of the Triform Fitting Of the Outer Wing Box ** ON A/C NOT FOR ALL (2) Apply sealant on the fasteners (10) between STGR8 to FR42, refer to Structural Repair Manual SRM 517612 and (Ref. AMM TASK 51-76-12-300-002).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the 98D57004013000 HOOK-COVER (RIB 2 SURGE DOORS) on the forward surge doors.
(3) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) on the aft surge doors.
(4) Close the RIB2 surge doors:
(5) Install the access panels (Ref. AMM TASK 57-27-11-400-001):
Subtask 57-10-00-942-075-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the 98D57004013000 HOOK-COVER (RIB 2 SURGE DOORS) on the forward surge doors.
(3) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) on the aft surge doors.
(4) Close the RIB2 surge doors:
(5) Install the access panels (Ref. AMM TASK 57-27-11-400-001):
C. Aircraft Maintenance Configuration
(1) Remove the access platform(s).
(2) Remove the WARNING NOTICE(S).
(3) Remove the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(1) Remove the access platform(s).
(2) Remove the WARNING NOTICE(S).
(3) Remove the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.