Special Detailed Inspection (HFEC) of Center Wing Box, Rear Spar, System Holes Near Man Holes
TASK 57-10-00-220-802-A
Special Detailed Inspection (HFEC) of Center Wing Box, Rear Spar, System Holes Near Man Holes
Refer to the MPD TASK: 571101-02
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, REAR SPAR, SYSTEM HOLES NEAR MAN HOLES
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 57-10-00-010-093-A
Subtask 57-10-00-220-064-A
Subtask 57-10-00-410-094-A
[Rev.10 from 2021]
2026.04.02 06:30:31 UTC
Special Detailed Inspection (HFEC) of Center Wing Box, Rear Spar, System Holes Near Man Holes
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: 571101-02
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, REAR SPAR, SYSTEM HOLES NEAR MAN HOLES
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) - ADJUSTABLE |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 147 | MAIN GEAR WELL AND HYDRAULIC COMPARTMENT |
| 148 | MAIN GEAR WELL AND HYDRAULIC COMPARTMENT |
| 734, 744 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 32-12-00-010-001-A | Open the Main Gear Doors for Access |
| TASK 32-12-00-410-001-A | Close the Main Gear Doors after Access |
| SRM 512300 | |
| SRM 512400 | |
| NTM 571101 | |
| SRM 511100 | (for corrective action) |
| SRM 512200 | (for corrective action) |
Subtask 57-10-00-010-093-A
A. Get Access
(1) Open the Main Landing Gear (MLG) door 734 ( 744) (Ref. AMM TASK 32-12-00-010-001).
(2) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position in zone 147 (148).
Subtask 57-10-00-110-081-A (1) Open the Main Landing Gear (MLG) door 734 ( 744) (Ref. AMM TASK 32-12-00-010-001).
(2) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position in zone 147 (148).
B. Preparation of the Inspection Area
(1) Remove the sealant and/or paint from the inspection area if this is necessary for the Non-destructive Testing Manual (NTM) task.
(2) Make sure that the surface of 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) Make sure that there is no:
(a) Corrosion damage:
4. Procedure(1) Remove the sealant and/or paint from the inspection area if this is necessary for the Non-destructive Testing Manual (NTM) task.
(2) Make sure that the surface of 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) 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 57-10-00-220-064-A
A. Inspection
(1) Do a special detailed inspection (HFEC) of the system holes near man holes of the rear spar of the centre wing box. Refer to Non-destructive Testing Manual NTM 571101.
(2) Make a report of the damage after the NDT inspection:
(a) Corrosion damage:
Subtask 57-10-00-910-050-A (1) Do a special detailed inspection (HFEC) of the system holes near man holes of the rear spar of the centre wing box. Refer to Non-destructive Testing Manual NTM 571101.
(2) Make a report of the damage after the 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 other damage, refer to Structural Repair Manual SRM 511100 for damage classification and corrective action.
B. Sealant or Paint Application
(1) Apply sealant ( SRM 512400) or paint ( SRM 512300) on the inspection area, if removed.
5. Close-up(1) Apply sealant ( SRM 512400) or paint ( SRM 512300) on the inspection area, if removed.
Subtask 57-10-00-410-094-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(3) Close the Main Landing Gear (MLG) door 734 ( 744) (Ref. AMM TASK 32-12-00-410-001).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(3) Close the Main Landing Gear (MLG) door 734 ( 744) (Ref. AMM TASK 32-12-00-410-001).
Inspection (HFEC) of the System Holes Near Man Holes of the Rear Spar of the Center Wing Box