W DOC AIRBUS | AMM A320F

Detailed Inspection of Outer Wing, Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIB 22-23, and Magnetic Level Indicator Position...

TASK 57-41-00-220-801-A
Detailed Inspection of Outer Wing, Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIB 22-23, and Magnetic Level Indicator Position...

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.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
ZONE: 500
ZONE: 600
1. Reason for the Job
Refer to the MPD TASK: 572164-03
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN RIB 22-23, AND MAGNETIC LEVEL INDICATOR POSITION BETWEEN RIB 15-16
2. Job Set-up Information
 A. 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
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
500
LEFT WING
600
RIGHT WING
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 28-00-00-910-001-A
Fuel Safety Procedures
SRM 572100
 (for corrective action)
F Fuel Tank Water Drain Hole in the Outer Wing Bottom Skin
F Magnetic Level Indicator between RIBS 15-16
3. Job Set-up
Subtask 57-41-00-941-070-A ** ON A/C NOT FOR ALL
A. Safety Precautions
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 a WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-41-00-865-090-A ** ON A/C NOT FOR ALL
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 57-41-00-010-057-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below the applicable fuel-tank water drain-holes and magnetic level indicator in the wing bottom skin.
4. Procedure
Subtask 57-41-00-110-066-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
  • The magnetic level indicator and the hole edges.
Subtask 57-41-00-220-050-A ** ON A/C NOT FOR ALL
B. Detailed Inspection of Outer Wing, Bottom-Skin Lower Surface at Fuel-Tank Water Drain-Holes between RIB 22-23, and Magnetic-Level Indicator Position between RIB 15 and 16
   (1) Examine the fuel-tank water drain-holes in the wing bottom skin between RIB 22 and 23. Make sure that:
F Fuel Tank Water Drain Hole in the Outer Wing Bottom Skin ** ON A/C NOT FOR ALL
  • There is no damage
  • The edges are not corroded
  • The surface finish of the edges is in good condition
  • There is no fuel leakage.
NOTE: If necessary, refer to the SRM 572100 for the correct repair procedure.
   (2) Examine the magnetic level indicator between RIB 15 and 16. Make sure that:
F Magnetic Level Indicator between RIBS 15-16 ** ON A/C NOT FOR ALL
  • The hole edges are not damaged
  • The sight collar is in good condition
  • The surface finish of the hole edges is in the correct condition
  • There is no fuel leakage
  • There is no corrosion.
NOTE: If necessary, refer to the SRM 572100 for the correct repair procedure.
5. Close-up
Subtask 57-41-00-865-091-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 57-41-00-942-075-A ** ON A/C NOT FOR ALL
B. Removal of Equipment
   (1) Remove the WARNING NOTICE(S).
   (2) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
   (3) Remove the SAFETY BARRIER(S).
   (4) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.02 06:30:58 UTC
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