Detailed Visual Inspection of the Outer Wing Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIBS 15-16 and 22-23
TASK 57-41-00-200-005-A
Detailed Visual Inspection of the Outer Wing Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIBS 15-16 and 22-23
Refer to the MPD TASK: 572164-01
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN RIB 15-16 AND RIB 22-23.
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 57-41-00-941-055-A ** ON A/C NOT FOR ALL
Subtask 57-41-00-110-059-A ** ON A/C NOT FOR ALL
Subtask 57-41-00-865-059-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:30:57 UTC
Detailed Visual Inspection of the Outer Wing Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIBS 15-16 and 22-23
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:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Refer to the MPD TASK: 572164-01
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN RIB 15-16 AND RIB 22-23.
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 4M (13 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 |
|---|---|
| 540 | FUEL TANK |
| 640 | FUEL TANK |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 28-00-00-910-001-A | Fuel Safety Procedures |
| SRM 572100 | (for corrective action) |
Subtask 57-41-00-941-055-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(3) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(4) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(5) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below the applicable holes in the wing bottom skin, zone 540/640.
Subtask 57-41-00-865-058-A ** ON A/C NOT FOR ALL WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
(1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001). (2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(3) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(4) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(5) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below the applicable holes in the wing bottom skin, zone 540/640.
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/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
Subtask 57-41-00-110-059-A ** ON A/C NOT FOR ALL
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 the wing bottom skin around the fuel tank water drain holes.
Subtask 57-41-00-210-054-A ** ON A/C NOT FOR ALL (1) Use a Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean the wing bottom skin around the fuel tank water drain holes.
B. Inspection
(1) Examine the fuel tank water drain holes in the wing bottom skin between RIBS 15-16 and 22-23.
Make sure that:
5. Close-up(1) Examine the fuel tank water drain holes in the wing bottom skin between RIBS 15-16 and 22-23.
Make sure that:
- there is no damage
- the edges are not corroded
- the surface finish of the edges is in good condition
- there are no signs of fuel leakages.
NOTE: If necessary, refer to the SRM 572100 for the correct repair procedure.
Subtask 57-41-00-865-059-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 57-41-00-942-054-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
B. Removal of Equipment
(1) Remove the access platform(s).
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(1) Remove the access platform(s).
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
Fuel Tank Water Drain Holes in the Outer Wing Bottom Skin