Detailed Inspection of Outer Wing, Trailing Edge, Aileron Hinge Pins 1 to 5
TASK 57-51-00-220-016-A
Detailed Inspection of Outer Wing, Trailing Edge, Aileron Hinge Pins 1 to 5
Refer to the MPD TASK: 575120-03
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, AILERON HINGE PINS 1 TO 5
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 57-51-00-941-080-A
Subtask 57-51-00-410-082-A
[Rev.10 from 2021]
2026.04.01 02:14:52 UTC
Detailed Inspection of Outer Wing, Trailing Edge, Aileron Hinge Pins 1 to 5
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.
Refer to the MPD TASK: 575120-03
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, AILERON HINGE PINS 1 TO 5
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 3M (10 FT) |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| 98D27104004000 | 5 | SLAVE PIN - AILERON |
| 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, 575JB, 575KB, 575LB, 575MB, 675AT, 675JB, 675KB, 675LB, 675MB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 27-14-41-000-001-A | Removal of the Aileron |
| TASK 27-14-41-400-001-A | Installation of the Aileron |
| TASK 57-51-37-000-005-A | Removal of the Access Panels 575KB(675KB), 575LB(675LB), 575MB(675MB) |
| TASK 57-51-37-000-006-A | Removal of the Access Panel 575JB(675JB) |
| 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 57-51-37-400-006-A | Installation of the Access Panel 575JB(675JB) |
| TASK 57-51-37-400-007-A | Installation of the Access Panel |
| SRM 575100 | (for corrective action) |
Subtask 57-51-00-941-080-A
A. Safety Precautions
(1) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(2) Put WARNING NOTICE(S) to tell persons not to operate the flaps or slats.
(3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 57-51-00-865-105-A (1) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(2) Put WARNING NOTICE(S) to tell persons not to operate the flaps or slats.
(3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 57-51-00-010-081-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. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable aileron, zone 575(675).
(2) Remove the applicable access panels:
(a) For the left wing remove:
4. Procedure(1) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable aileron, zone 575(675).
(2) Remove the applicable access panels:
(a) For the left wing remove:
- 575AT (Ref. AMM TASK 57-51-37-000-007)
- 575JB (Ref. AMM TASK 57-51-37-000-006)
- 575KB 575LB 575MB (Ref. AMM TASK 57-51-37-000-005).
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
Subtask 57-51-00-020-081-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. Remove Items for Inspection
(1) One at a time, remove the five hinge pins from each aileron and replace them with the 98D27104004000 SLAVE PIN - AILERON (Ref. AMM TASK 27-14-41-000-001).
Subtask 57-51-00-110-090-A (1) One at a time, remove the five hinge pins from each aileron and replace them with the 98D27104004000 SLAVE PIN - AILERON (Ref. AMM TASK 27-14-41-000-001).
B. Preparation for Inspection
Subtask 57-51-00-220-081-A WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
(1) Use a Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean the hinge pins. C. Detailed Inspection of Outer Wing, Trailing Edge, Aileron Hinge Pins 1 to 5
(1) Examine the hinge pins for:
Subtask 57-51-00-420-079-A (1) Examine the hinge pins for:
- damage
- scratches and/or scores
- corrosion
- correct condition of the surface protection.
NOTE: If necessary, refer to the SRM 575100 for the correct repair procedure.
D. Install items after Inspection
(1) One at a time, remove the five 98D27104004000 SLAVE PIN - AILERON from each aileron and replace them with the hinge pins (Ref. AMM TASK 27-14-41-400-001).
5. Close-up(1) One at a time, remove the five 98D27104004000 SLAVE PIN - AILERON from each aileron and replace them with the hinge pins (Ref. AMM TASK 27-14-41-400-001).
Subtask 57-51-00-410-082-A
A. Close Access
(1) Install the applicable access panels:
(a) For the left wing install:
Subtask 57-51-00-865-106-A (1) Install the applicable access panels:
(a) For the left wing install:
- 575AT (Ref. AMM TASK 57-51-37-400-007)
- 575JB (Ref. AMM TASK 57-51-37-400-006)
- 575KB 575LB 575MB (Ref. AMM TASK 57-51-37-400-005).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 57-51-00-942-081-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 Pins