W DOC AIRBUS | AMM A320F

Special Detailed Inspection (HFEC) of Cockpit Windshield, Lower Front Fitting at FR 4, Lower Attachment, External Surface, LH/RH


TASK 53-11-00-210-039-A
Special Detailed Inspection (HFEC) of Cockpit Windshield, Lower Front Fitting at FR 4, Lower Attachment, External Surface, LH/RH


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 200
1. Reason for the Job
Refer to the MPD TASK: 531170-02
SPECIAL DETAILED INSPECTION (HFEC) OF COCKPIT WINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNAL SURFACE, LH/RH

NOTE: The effectivity of this task is "ALL". To know if this task is applicable to your aircraft, refer to the MPD task applicability.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
No specific
AR
SCRAPER - NON METALLIC
 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
200
UPPER HALF FUSELAGE
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 56-11-11-000-001-A
Removal of the Windshield
TASK 56-11-11-000-001-A-01
Removal of the Windshield
TASK 56-11-11-400-001-A
Installation of the Windshield
TASK 56-11-11-400-001-A-01
Installation of the Windshield
NTM 531170
SRM 511100
(for corrective action)
SRM 512200
(for corrective action)
3. Job Set-up
Subtask 53-11-00-020-054-A
A. Get Access
   (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 210 in front of the windshield.
   (2) Remove the lower retainers (Ref. AMM TASK 56-11-11-000-001).
Subtask 53-11-00-110-087-A
B. Preparation of the Inspection Area
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
   (1) Remove the sealant from the inspection area with a SCRAPER - NON METALLIC.
   (2) Clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and the Textile-Lint free Cotton - (Material No.14SBA1) , if necessary.
   (3) Make sure that the surface of the inspection area is clean and smooth.
   (4) Do a visual check of the inspection area for damage or discontinuities.
   (5) Make sure that there is no:
     (a) Corrosion damage:
If you find corrosion, refer to the Structural Repair Manual ( SRM 512200) for the corrosion types, inspection, removal and subsequent corrosion protection.
     (b) Other damage (scratches, cracks, gouges, dents, creases):
If you find this type of damage, refer to the Structural Repair Manual ( SRM 511100) for the damage types, classification and corrective action.
4. Procedure
Subtask 53-11-00-250-051-A
A. Inspection
   (1) Do a special detailed inspection of the structure of the lower front fittings of the cockpit windshield. This inspection is applicable at FR4, left and right sides NTM 531170.
   (2) Make a report of the damage after the NTM inspection:
     (a) Corrosion damage:
If you find corrosion, refer to the Structural Repair Manual ( SRM 512200) for the corrosion types, inspection, removal and subsequent corrosion protection.
     (b) Other damage (scratches, cracks, gouges, dents, creases):
If you find this type of damage, refer to the Structural Repair Manual ( SRM 511100) for the damage types, classification and corrective action.
5. Close-up
Subtask 53-11-00-420-052-A
A. Close Access
   (1) Install the lower retainers (Ref. AMM TASK 56-11-11-400-001).
   (2) Make sure that the work area is clean and clear of tools and other items.
   (3) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.02 06:28:43 UTC