Detailed Inspection of Fuselage Skin around Water Service Panel Cutout, between FR 65 and FR 66 and from Stringer 37 to Stringer 43, LH, External...
TASK 53-41-00-210-816-A
Detailed Inspection of Fuselage Skin around Water Service Panel Cutout, between FR 65 and FR 66 and from Stringer 37 to Stringer 43, LH, External...
Refer to the MPD TASK: 534141-01
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WATER SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 53-41-00-010-223-A
Subtask 53-41-00-210-118-A
Subtask 53-41-00-410-217-A
[Rev.10 from 2021]
2026.04.02 06:29:17 UTC
Detailed Inspection of Fuselage Skin around Water Service Panel Cutout, between FR 65 and FR 66 and from Stringer 37 to Stringer 43, LH, External...
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:
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.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 170
1. Reason for the JobRefer to the MPD TASK: 534141-01
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WATER SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE
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 1M(3 FT) |
| No specific | 1 | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 170 | AFT CAB U/FLOOR COMPT AFT BHD OF BULK |
| REFERENCE | DESIGNATION |
|---|---|
| SRM 511100 | |
| SRM 512200 | |
| SRM 512300 | |
Subtask 53-41-00-010-223-A
A. Get Access
(1) Put a WARNING NOTICE(S) in position to tell persons not to operate the flight controls.
(2) Put the ACCESS PLATFORM 1M(3 FT) in position, below the inspection area.
Subtask 53-41-00-110-099-A (1) Put a WARNING NOTICE(S) in position to tell persons not to operate the flight controls.
(2) Put the ACCESS PLATFORM 1M(3 FT) in position, below the inspection area.
B. 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) .
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) .
Subtask 53-41-00-210-118-A
A. Inspection
(1) Do a detailed inspection of the external surface of the fuselage skin around the water service panel cutout, between FR 65 and FR 66 and from stringer 37 to stringer 43, LH, 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 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.
5. Close-up(1) Do a detailed inspection of the external surface of the fuselage skin around the water service panel cutout, between FR 65 and FR 66 and from stringer 37 to stringer 43, LH, 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 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 53-41-00-410-217-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) Remove the WARNING NOTICE(S).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).
External Fuselage Skin around the Cutout for the Potable-Water Service Door