W DOC AIRBUS | AMM A320F

Detailed Inspection of NLG Bay, Rear Panel Aft Face, Lower Corners, LH/RH


TASK 53-11-00-210-018-A
Detailed Inspection of NLG Bay, Rear Panel Aft Face, Lower Corners, LH/RH


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 127
ZONE: 128
1. Reason for the Job
Refer to the MPD TASK: 531162-01
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 Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
 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
127
REAR AVIONIC COMPARTMENT
128
REAR AVIONIC COMPARTMENT
824
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 52-41-00-010-002-A
Open the Avionics Compartment Doors for Access
TASK 52-41-00-410-002-A
Close the Avionics Compartment Doors after Access
TASK 53-12-13-000-001-A
Removal of the avionics compartment floor panels
TASK 53-12-13-400-001-A
Installation of the avionics compartment floor panels
SRM 51110001
(for corrective action)
SRM 51220001
(for corrective action)
3. Job Set-up
Subtask 53-11-00-010-060-A
A. Get Access
   (1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at zone 824.
   (2) Open the lateral avionics-compartment door 824 (Ref. AMM TASK 52-41-00-010-002).
Subtask 53-11-00-020-059-A
B. Removal of the Components
   (1) Remove the two quick-release pins (1) and lift and remove the ladder (2), if necessary.
   (2) Remove the necessary floor panel (4) of the avionics compartment (Ref. AMM TASK 53-12-13-000-001).
Subtask 53-11-00-110-077-A
C. Cleaning of the Structure
   (1) Clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and a lint-free cotton cloth Textile-Lint free Cotton - (Material No.14SBA1) , if necessary.
4. Procedure
Subtask 53-11-00-220-082-A
A. Inspection
   (1) Do a detailed inspection of the structure of the NLG well. This inspection is applicable to the rear panel aft face, lower corners, left and right sides.
   (2) Make sure that there is no:
     (a) Corrosion damage:
- If you find corrosion damage, refer to the Structural Repair Manual SRM 51220001 for types of corrosion, inspection, removal and corrosion protection.
     (b) Other damage (cracks, scratches, stress, marks, dents, bumps,...):
- If you find other damage, refer to the Structural Repair Manual SRM 51110001 for damage classification and corrective action.
5. Close-up
Subtask 53-11-00-420-057-A
A. Installation of the Components
   (1) Install the necessary floor panel (4) in the avionics compartment (Ref. AMM TASK 53-12-13-400-001).
   (2) Install the ladder (2) on the floor fittings (3), if necessary, and install the two quick-release pins (1).
Subtask 53-11-00-410-060-A
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the lateral avionics-compartment door 824 (Ref. AMM TASK 52-41-00-410-002).
   (3) Remove the access platform(s).
[Rev.8 from Aug 2017] 2026.04.02 06:28:49 UTC