Installation of the Access Panel 575JB(675JB)
TASK 57-51-37-400-006-A
Installation of the Access Panel 575JB(675JB)
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Referenced Information
3. Job Set-up
Subtask 57-51-37-941-063-A
Subtask 57-51-37-420-060-A
Subtask 57-51-37-942-058-A
[Rev.10 from 2021]
2026.04.01 02:15:39 UTC
Installation of the Access Panel 575JB(675JB)
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
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.
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
1. Reason for the Job- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 4M (13 FT) |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| No specific | Torque wrench: range to between 0.45 and 0.4 m.daN (39.82 and 35.40 lbf.in ) ![]() | |
| 98D27803500001 | 1 | LOCKING TOOL ZERO POS |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.06AEA1) | Polysulfide Sealant-Low Adhesion Brushable - |
| (Material No.06AEB2) | Polysulfide Sealant-Low Adhesion Fillet Structure |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| REFERENCE | DESIGNATION |
|---|---|
Subtask 57-51-37-941-063-A
A. Safety Precautions
(1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure that the 98D27803500001 LOCKING TOOL ZERO POS is installed on the flap/slat control lever.
(3) Make sure that the WARNING NOTICE(S) are in position to tell persons not to operate the flaps or slats.
Subtask 57-51-37-860-055-A (1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure that the 98D27803500001 LOCKING TOOL ZERO POS is installed on the flap/slat control lever.
(3) Make sure that the WARNING NOTICE(S) are in position to tell persons not to operate the flaps or slats.
B. Aircraft Maintenance Configuration
(1) Make sure that the ACCESS PLATFORM 4M (13 FT) is in position below the applicable zone 575(675).
4. Procedure(1) Make sure that the ACCESS PLATFORM 4M (13 FT) is in position below the applicable zone 575(675).
Subtask 57-51-37-420-060-A
A. Preparation for Installation
(1) Clean the component interfaces and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 57-51-37-420-061-A (1) Clean the component interfaces and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
B. Installation of the Access Panel 575JB(675JB)
(1) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the aircraft structure/component interface.
(2) Put the access panel (1) in position.
(3) Install the bolts (2) but do not tighten. Make sure that you can move the access panel (1) sufficient to adjust its position.
(4) Set the access panel (1) so that the dimension X is 2.5 mm (0.0984 in.) +/- 1.9 mm (0.0748 in.).
(5) TORQUE tighten the bolts (2) to between 0.45 and 0.4 m.daN (39.82 and 35.40 lbf.in )
.
(6) Fill the clearance (dimension X) between the access panel (1) and the wing skin with Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) .
5. Close-up(1) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the aircraft structure/component interface.
(2) Put the access panel (1) in position.
(3) Install the bolts (2) but do not tighten. Make sure that you can move the access panel (1) sufficient to adjust its position.
(4) Set the access panel (1) so that the dimension X is 2.5 mm (0.0984 in.) +/- 1.9 mm (0.0748 in.).
(5) TORQUE tighten the bolts (2) to between 0.45 and 0.4 m.daN (39.82 and 35.40 lbf.in )
. (6) Fill the clearance (dimension X) between the access panel (1) and the wing skin with Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) .
Subtask 57-51-37-942-058-A
A. Removal of Equipment
(1) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(5) Remove the WARNING NOTICE(S).
(6) Remove the safety barriers.
(1) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(5) Remove the WARNING NOTICE(S).
(6) Remove the safety barriers.
Lower Trailing Edge Access Panel 575JB(675JB)