W DOC AIRBUS | AMM A320F

Repair of the Washbasin Door in the Latch Area


TASK 25-40-00-340-802-A
Repair of the Washbasin Door in the Latch Area


1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Consumable Materials
REFERENCE
DESIGNATION
(Material No.04JMD9)
Top Coat Polyurethane-- Decorative Furnishing
(Material No.05EML9)
Epoxy Adhesive-- - Legacy 1
(Material No.08BBD1)
Non Aqueous Cleaner-- Isopropyl Alcohol -
(Material No.14SBA1)
Textile-Lint free Cotton -
No specific
abrasive paper, 320-400 grade
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
3. Job Set-up
Subtask 25-40-00-861-066-A
A. Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
Subtask 25-40-00-010-062-A
B. Get Access
   (1) If necessary, remove the component from the aircraft (refer to the related AMM chapter).
4. Procedure
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION: USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM THE MATERIAL MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA.
Subtask 25-40-00-340-059-A
A. Repair of the Washbasin Door in the Latch Area
NOTE: If cracks are longer than 76 mm (3 in.) the washbasin door must be replaced.
   (1) Remove the latch (1).
   (2) Clean the damaged area with the Non Aqueous Cleaner-- Isopropyl Alcohol - (Material No.08BBD1) and clean the moist stain with a Textile-Lint free Cotton - (Material No.14SBA1) .
   (3) Fill the damaged area with the Epoxy Adhesive-- - Legacy 1 (Material No.05EML9) .
   (4) Install a stiffener plate (2) made from material LN 9073AT10 or 6061T6, 1 mm (0.04 in.) thick with the Epoxy Adhesive-- - Legacy 1 (Material No.05EML9) .
NOTE: If the dimensions of 100 x 100 mm are too small to cover all cracks, it is permitted to install a stiffener plate with larger dimensions.
   (5) Make the area smooth with the abrasive paper, 320-400 grade.
   (6) Clean the repaired area with the Non Aqueous Cleaner-- Isopropyl Alcohol - (Material No.08BBD1) and clean the moist stain with a Textile-Lint free Cotton - (Material No.14SBA1) .
   (7) Apply Top Coat Polyurethane-- Decorative Furnishing (Material No.04JMD9) in the related color to the repair area.
   (8) Install the latch (1).
5. Close-up
Subtask 25-40-00-410-065-A
A. Close Access
   (1) If necessary, install the component in the aircraft (refer to the related AMM chapter).
   (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Subtask 25-40-00-862-067-A
B. De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.03.31 23:35:04 UTC