W DOC AIRBUS | AMM A320F

Remove and Detailed Inspection of Piston Type Drain Valves in Lower Fuselage Shell


TASK 53-00-00-210-001-A
Remove and Detailed Inspection of Piston Type Drain Valves in Lower Fuselage Shell


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 100
1. Reason for the Job
Refer to the MPD TASK: 530000-01
REMOVE AND DETAILED INSPECTION OF PISTON TYPE DRAIN VALVES IN LOWER FUSELAGE SHELL
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT)
No specific
1
PROBE - NON METALLIC, FLEXIBLE
No specific
1
SCRAPER - NON METALLIC
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.06AEA1)
Polysulfide Sealant-Low Adhesion Brushable -
(Material No.06AEB2)
Polysulfide Sealant-Low Adhesion Fillet Structure
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.08BPA1)
Non Aqueous Cleaner-Non structural use - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
100
LOWER HALF FUSELAGE INCLUDING RADOME
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 53-35-13-000-001-A
Removal of the Belly Fairing Access Panels
TASK 53-35-13-400-001-A
Installation of the Belly Fairing Access Panels
F Piston-Type Drain Valves ** ON A/C NOT FOR ALL
F Piston-Type Drain Valves ** ON A/C NOT FOR ALL
F Piston-Type Drain Valves ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 53-00-00-010-050-A
A. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) in position.
   (2) If installed, remove access panel 197RB (Ref. AMM TASK 53-35-13-000-001).
Subtask 53-00-00-110-050-A
B. Cleaning Procedure
   (1) Remove the sealant from the inspection area with the SCRAPER - NON METALLIC.
   (2) Clean the drain valves and the adjacent areas of the fuselage skin external-surface with Non Aqueous Cleaner-Non structural use - - (Material No.08BPA1) or Non Aqueous Cleaner-General - - (Material No.08BAA9) and the Textile-Lint free Cotton - (Material No.14SBA1) .
4. Procedure
Subtask 53-00-00-210-050-A
A. Inspection of the Piston-Type Drain Valves of the Lower Fuselage Shell
   (1) Remove the piston-type drain valves from the lower fuselage shell and examine them as follows:
     (a) Remove the basic valves from the drain valve assemblies.
     (b) Make sure that the basic valves are not blocked.
     (c) If they are blocked, remove the blockage.
     (d) Carefully put the PROBE - NON METALLIC, FLEXIBLE in the center of each basic valve to make sure that the valves are open.
     (e) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) on the mating surface of the drain valves and the structure.
     (f) Install the basic valves.
5. Close-up
Subtask 53-00-00-410-050-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) If removed, install access panel 197RB (Ref. AMM TASK 53-35-13-400-001).
   (3) Remove the access platform(s).
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 01:49:43 UTC