DOC AIRBUS | AMM A320FSpecial Detailed Inspection (ELCH TEST) of the Bonding Layer between Rudder Side Panel Honeycomb Structure and External Skins of the Rudder Side Panels...
TASK 55-40-00-210-006-A
Special Detailed Inspection (ELCH TEST) of the Bonding Layer between Rudder Side Panel Honeycomb Structure and External Skins of the Rudder Side Panels...
Refer to the MPD TASK: 554009-01
SPECIAL DETAILED INSPECTION (ELCH TEST) OF THE BONDING LAYERS BETWEEN RUDDER SIDE PANEL HONEYCOMB STRUCTURE AND EXTERNAL SKINS OF THE RUDDER SIDE PANELS, LH / RH.
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 55-40-00-865-065-A
Subtask 55-40-00-210-055-A
Subtask 55-40-00-865-067-A
[Rev.10 from 2021]
2026.04.01 02:06:21 UTC
Special Detailed Inspection (ELCH TEST) of the Bonding Layer between Rudder Side Panel Honeycomb Structure and External Skins of the Rudder Side Panels...
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 300
1. Reason for the JobRefer to the MPD TASK: 554009-01
SPECIAL DETAILED INSPECTION (ELCH TEST) OF THE BONDING LAYERS BETWEEN RUDDER SIDE PANEL HONEYCOMB STRUCTURE AND EXTERNAL SKINS OF THE RUDDER SIDE PANELS, LH / RH.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE |
| No specific | AR | CLOTH-EMERY (GRADE 280) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BPA1) | Non Aqueous Cleaner-Non structural use - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 300 | STABILIZERS AND TAIL UNIT |
| 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 |
| NTM 511026 | |
| SRM 517511 | |
| NTM 554009 | |
| SRM 554100 | |
| SRM 55410001 | (for corrective action) |
Bonding Layer between Rudder Side Panel Honeycomb Structure and External Skins of the Rudder Side Panels, LH/RHSubtask 55-40-00-865-065-A
A. Open, safety and tag this(these) circuit breaker(s):
Subtask 55-40-00-860-055-A | 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 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B04 |
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | H10 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | H09 |
| ** ON A/C ALL | |||
| 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
(2) Put the WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the flight controls.
Subtask 55-40-00-010-055-A 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 FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
(1) Make sure that the Green, Yellow and Blue hydraulic systems are depressurized (Ref. AMM TASK 29-10-00-864-001), (Ref. AMM TASK 29-10-00-864-002) and (Ref. AMM TASK 29-10-00-864-003). (2) Put the WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the flight controls.
C. Get Access
(1) Put the ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at Zone 326.
Subtask 55-40-00-860-056-A (1) Put the ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at Zone 326.
D. Preparation for Inspection
(1) Make sure that the surfaces of the inspection areas are clean and smooth.
(4) Make sure that you can clearly see the positions of the rivets in the inspection areas.
(5) If necessary, remove the paint from the rivets in the inspection areas SRM 517511.
(6) Make sure the inspection areas are clean and dry before you continue.
(7) If you find damage:
4. Procedure(1) Make sure that the surfaces of the inspection areas are clean and smooth.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
(2) If necessary, clean the inspection areas with the Non Aqueous Cleaner-Non structural use - - (Material No.08BPA1) and a Textile-Lint free Cotton - (Material No.14SBA1) . CAUTION:
DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.
(3) If necessary, make the surface of the inspection areas smooth with the CLOTH-EMERY (GRADE 280). (4) Make sure that you can clearly see the positions of the rivets in the inspection areas.
(5) If necessary, remove the paint from the rivets in the inspection areas SRM 517511.
(6) Make sure the inspection areas are clean and dry before you continue.
(7) If you find damage:
- refer to the ASRM SRM 554100 for the necessary data.
Subtask 55-40-00-210-055-A
A. Special Detailed Inspection
5. Close-upNOTE: Do the inspection procedures which follow in the sequence given below.
(1) Do a special detailed inspection of the bonding layer between rudder side panel honeycomb structure and external skins of the rudder side panels, LH/RH. NOTE: Use the ELCH-inspection of LH/RH Ruddershells as per NTM 554009 (use NTM 511026).
NOTE: If you apply high pressure with your hand to the rudder composite side-panels:
(2) If you find damage, refer to the ASRM SRM 55410001 for the necessary data. - It is possible to hear a noise with the sound of a "click" from the honeycomb core.
This noise has no effect on the condition of the rudder. The rudder is servicable, if no delamination or debonding is found during the inspection procedure.
Subtask 55-40-00-865-067-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 55-40-00-410-056-A | 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 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B04 |
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | H10 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | H09 |
| ** ON A/C ALL | |||
| 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. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the WARNING NOTICE(S).
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the WARNING NOTICE(S).
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.