DOC AIRBUS | AMM A320FPrepare the Vertical Stabilizer Leading - Edge for Anti-Erosion Protection Application
TASK 55-32-11-100-001-A
Prepare the Vertical Stabilizer Leading - Edge for Anti-Erosion Protection Application
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 55-32-11-941-052-A ** ON A/C NOT FOR ALL
Subtask 55-32-11-110-052-A ** ON A/C NOT FOR ALL
Subtask 55-32-11-865-055-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:05:53 UTC
Prepare the Vertical Stabilizer Leading - Edge for Anti-Erosion Protection Application
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.
ZONE: 324
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.04PAH3) | Polyurethane Coating-- Erosion Resistant External Structure |
| (Material No.05EML9) | Epoxy Adhesive-- - Legacy 1 |
| (Material No.05RQB1) | Adhesive Film Tape-Erosion Protective Polyurethane - 0.36mm - |
| (Material No.05RQB9) | Adhesive Film Tape-Erosion Protective Polyurethane - 0.36mm Legacy |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.08BBB1) | Non Aqueous Cleaner-- Petroleum Based - |
| (Material No.14FAB1) | Abrasive-- Scotch Brite Pads - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 324 | VERTICAL STABILIZER TIP |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 29-10-00-864-001-A | Depressurize the Green Hydraulic System |
| TASK 29-10-00-864-002-A | Depressurize the Yellow Hydraulic System |
| TASK 29-10-00-864-003-A | Depressurize the Blue Hydraulic System |
| TASK 51-75-12-300-001-A | Repair of Major Paint Damage on Light Alloy and Composite Material |
| SRM 517512 | |
Cleaning/Repair Area and DimensionsSubtask 55-32-11-941-052-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. AMM TASK 29-10-00-864-001) (Ref. AMM TASK 29-10-00-864-002) (Ref. AMM TASK 29-10-00-864-003).
(2) Put the WARNING NOTICE(S) in the cockpit to tell persons not to operate the flight controls.
(3) Put the ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE in position.
Subtask 55-32-11-865-054-A ** ON A/C NOT FOR ALL (1) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. AMM TASK 29-10-00-864-001) (Ref. AMM TASK 29-10-00-864-002) (Ref. AMM TASK 29-10-00-864-003).
(2) Put the WARNING NOTICE(S) in the cockpit to tell persons not to operate the flight controls.
(3) Put the ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE in position.
B. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B09 |
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | B04 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | B03 |
| 105VU | FLIGHT CONTROLS/ELAC2/STBY SPLY | 16CE2 | A02 |
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | AUTO FLT/RUDDER/TRIM/IND | 15CC | M20 |
| 121VU | AUTO FLT/FAC2/28VDC | 5CC2 | M19 |
| 121VU | AUTO FLT/FAC2/26VAC | 14CC2 | M18 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT3 | 19CE3 | Q17 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT1 | 19CE1 | Q16 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
Subtask 55-32-11-110-052-A ** ON A/C NOT FOR ALL
A. Cleaning
(a) Clean the leading edge surface with a Textile-Lint free Cotton - (Material No.14SBA1) and Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(c) Carefully dry the area with a new and dry lint free cloth.
Subtask 55-32-11-370-050-A ** ON A/C NOT FOR ALL CAUTION:
USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM THE MATERIAL MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA.
(1) Cleaning of the leading edge. (a) Clean the leading edge surface with a Textile-Lint free Cotton - (Material No.14SBA1) and Non Aqueous Cleaner-General - - (Material No.08BAA9) .
- Apply the Non Aqueous Cleaner-General - - (Material No.08BAA9) to the cloth, not the cloth to the Non Aqueous Cleaner-General - - (Material No.08BAA9) . This will prevent the movement of contamination.
- Carefully clean a small area at a time. Remove the Non Aqueous Cleaner-General - - (Material No.08BAA9) before it becomes dry. Change the lint free cloth frequently to prevent the movement of dirt from the cloth to the surface again.
- If necessary use a soft brush to clean out any holes.
(c) Carefully dry the area with a new and dry lint free cloth.
B. Painting
(2) Treatment before Painting:
(b) Clean the surface with the Non Aqueous Cleaner-General - - (Material No.08BAA9) and a clean lint-free cloth Textile-Lint free Cotton - (Material No.14SBA1) .
(c) Remove the Non Aqueous Cleaner-General - - (Material No.08BAA9) before it becomes dry. Do not touch the prepared surface with your hand.
(d) Apply the Polyurethane Coating-- Erosion Resistant External Structure (Material No.04PAH3) to the prepared area on the vertical stabilizer.
(3) Treatment before you apply the erosion-protective tape:
(a) Do a repair if the paint or primer layers are damaged (Ref. AMM TASK 51-75-12-300-001).
(4) Repair of the erosion-protective tape:
(a) Apply the new erosion-protective tape Adhesive Film Tape-Erosion Protective Polyurethane - 0.36mm Legacy (Material No.05RQB9) or Adhesive Film Tape-Erosion Protective Polyurethane - 0.36mm - (Material No.05RQB1) to the leading edge surface SRM 517512.
(5) Application of the bonding and adhesive compound:
(a) After 1 hour after you applied the erosion-protective tape:
5. Close-upWARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
(1) Do a repair if the paint or primer layers are damaged (Ref. AMM TASK 51-75-12-300-001). (2) Treatment before Painting:
CAUTION:
DO NOT USE FORCE TO MAKE THE SURFACE SMOOTH. TOO MUCH FORCE WILL CAUSE:
(a) If necessary, carefully clean the surface to be painted with a fine-grade Abrasive-- Scotch Brite Pads - (Material No.14FAB1) and the Non Aqueous Cleaner-- Petroleum Based - (Material No.08BBB1) . Make sure that the primer layer does not show. - DAMAGE TO THE SURFACE
- DELAMINATION OF THE COMPOSITE STRUCTURE.
(b) Clean the surface with the Non Aqueous Cleaner-General - - (Material No.08BAA9) and a clean lint-free cloth Textile-Lint free Cotton - (Material No.14SBA1) .
(c) Remove the Non Aqueous Cleaner-General - - (Material No.08BAA9) before it becomes dry. Do not touch the prepared surface with your hand.
(d) Apply the Polyurethane Coating-- Erosion Resistant External Structure (Material No.04PAH3) to the prepared area on the vertical stabilizer.
(3) Treatment before you apply the erosion-protective tape:
(a) Do a repair if the paint or primer layers are damaged (Ref. AMM TASK 51-75-12-300-001).
(4) Repair of the erosion-protective tape:
(a) Apply the new erosion-protective tape Adhesive Film Tape-Erosion Protective Polyurethane - 0.36mm Legacy (Material No.05RQB9) or Adhesive Film Tape-Erosion Protective Polyurethane - 0.36mm - (Material No.05RQB1) to the leading edge surface SRM 517512.
(5) Application of the bonding and adhesive compound:
(a) After 1 hour after you applied the erosion-protective tape:
- Apply a layer of the Epoxy Adhesive-- - Legacy 1 (Material No.05EML9) to the edges of the erosion-protective tape and the leading edge surface.
NOTE: We recommend you to apply the bonding and adhesive compound, but it is not mandatory.
Subtask 55-32-11-865-055-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 55-32-11-942-053-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B09 |
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | B04 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | B03 |
| 105VU | FLIGHT CONTROLS/ELAC2/STBY SPLY | 16CE2 | A02 |
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | AUTO FLT/RUDDER/TRIM/IND | 15CC | M20 |
| 121VU | AUTO FLT/FAC2/28VDC | 5CC2 | M19 |
| 121VU | AUTO FLT/FAC2/26VAC | 14CC2 | M18 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT3 | 19CE3 | Q17 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT1 | 19CE1 | Q16 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
B. Aircraft Maintenance Configuration
(1) Remove the access platform(s).
(2) Remove the WARNING NOTICE(S).
(1) Remove the access platform(s).
(2) Remove the WARNING NOTICE(S).