Detailed Inspection of Aileron, Hinge Fittings and Actuator Attachment Fittings
TASK 57-60-00-200-002-A
Detailed Inspection of Aileron, Hinge Fittings and Actuator Attachment Fittings
Refer to the MPD TASK: 576103-01
DETAILED INSPECTION OF AILERON, HINGE FITTINGS AND ACTUATOR ATTACHMENT FITTINGS
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 57-60-00-941-051-A
Subtask 57-60-00-410-050-A
[Rev.10 from 2021]
2026.04.01 02:18:00 UTC
Detailed Inspection of Aileron, Hinge Fittings and Actuator Attachment Fittings
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
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.
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.
Refer to the MPD TASK: 576103-01
DETAILED INSPECTION OF AILERON, HINGE FITTINGS AND ACTUATOR ATTACHMENT FITTINGS
NOTE: The effectivity of this task is ALL. To know if this task is applicable for 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 5M (16 FT)- ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| 98D27803500001 | 1 | LOCKING TOOL ZERO POS |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 570 | AFT SECTION OF L WING & TE FIXED STRUCT |
| 670 | AFT SECTION OF R WING & TE FIXED STRUCT |
| 575AT, 575KB, 575LB, 575MB, 675AT, 675KB, 675LB, 675MB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 29-10-00-864-001-A | Depressurize the Green Hydraulic System |
| TASK 29-10-00-864-003-A | Depressurize the Blue Hydraulic System |
| TASK 57-51-37-000-005-A | Removal of the Access Panels 575KB(675KB), 575LB(675LB), 575MB(675MB) |
| TASK 57-51-37-000-007-A | Removal of the Access Panel |
| TASK 57-51-37-400-005-A | Installation of the Access Panels 575KB(675KB), 575LB(675LB), 575MB(675MB) |
| TASK 57-51-37-400-007-A | Installation of the Access Panel |
| SRM 576000 | (for corrective action) |
Subtask 57-60-00-941-051-A
A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(3) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(4) Put WARNING NOTICE(S) in position to tell persons not to pressurize the hydraulic systems:
Subtask 57-60-00-860-052-A (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(3) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(4) Put WARNING NOTICE(S) in position to tell persons not to pressurize the hydraulic systems:
- on the ground service panels
- in the cockpit, on the HYD overhead panel 40VU.
B. Aircraft Maintenance Configuration
(1) Make sure that these aircraft hydraulic systems are depressurized:
Subtask 57-60-00-865-052-A (1) Make sure that these aircraft hydraulic systems are depressurized:
- the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001)
- the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
C. Open, safety and tag this(these) circuit breaker(s):
Subtask 57-60-00-010-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 105VU | FLIGHT CONTROLS/ELAC2/STBY SPLY | 16CE2 | A02 |
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
D. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE below the applicable aileron, zone 590 (690).
(2) Remove the applicable access panels:
(a) For the left wing remove:
(b) For the right wing remove:
4. Procedure(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE below the applicable aileron, zone 590 (690).
(2) Remove the applicable access panels:
(a) For the left wing remove:
(b) For the right wing remove:
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
Subtask 57-60-00-110-051-A - 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.
A. Preparation for Inspection
(1) Use a Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean:
Subtask 57-60-00-866-050-A (1) Use a Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean:
- the aileron hinge fittings
- the aileron actuator attachment fittings.
B. Manually move the aileron to get access to the actuators and the hinges.
Subtask 57-60-00-210-051-A NOTE: The internal flutter dampening system of the actuators will keep the aileron in position.
C. Detailed Inspection of Aileron, Hinge Fittings and Actuator Attachment Fittings
(1) Examine the hinge fittings and the actuator attachment fittings. Make sure that:
5. Close-up(1) Examine the hinge fittings and the actuator attachment fittings. Make sure that:
- there is no damage
- there is no corrosion
- there are no cracks
- the components are correctly attached
- the surface protection is in the correct condition.
NOTE: If necessary, refer to the SRM 576000 for the correct repair procedure.
Subtask 57-60-00-410-050-A
A. Close Access
(1) Install the applicable access panels:
(a) For the left wing install:
(b) For the right wing install:
Subtask 57-60-00-865-053-A (1) Install the applicable access panels:
(a) For the left wing install:
(b) For the right wing install:
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 57-60-00-942-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 105VU | FLIGHT CONTROLS/ELAC2/STBY SPLY | 16CE2 | A02 |
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
C. Removal of Equipment
(1) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(2) Remove the WARNING NOTICE(S).
(3) Remove the access platform(s).
(4) Remove the safety barriers.
(5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(2) Remove the WARNING NOTICE(S).
(3) Remove the access platform(s).
(4) Remove the safety barriers.
(5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Aileron - Hinge Fittings and Actuator Attachment Fittings