Detailed Inspection of Pressure Bulkhead, Aft Face, Lower Part of Vertical Struts (200 mm from bottom) at Y= +/-765 mm (2 places)
TASK 53-31-00-220-806-A
Detailed Inspection of Pressure Bulkhead, Aft Face, Lower Part of Vertical Struts (200 mm from bottom) at Y= +/-765 mm (2 places)
1. Reason for the Job
Refer to the MPD TASK: 533188-01
DETAILED INSPECTION OF PRESSURE BULKHEAD, AFT FACE, LOWER PART OF VERTICAL STRUTS (200 MM FROM BOTTOM) AT Y= +/-765 MM (2 PLACES)
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 53-31-00-010-126-A
Subtask 53-31-00-220-070-A
Subtask 53-31-00-410-123-A
[Rev.10 from 2021]
2026.04.02 06:29:07 UTC
Detailed Inspection of Pressure Bulkhead, Aft Face, Lower Part of Vertical Struts (200 mm from bottom) at Y= +/-765 mm (2 places)
1. Reason for the Job
Refer to the MPD TASK: 533188-01
DETAILED INSPECTION OF PRESSURE BULKHEAD, AFT FACE, LOWER PART OF VERTICAL STRUTS (200 MM FROM BOTTOM) AT Y= +/-765 MM (2 PLACES)
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 InformationA. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | FLASHLIGHT |
| No specific | 1 | MIRROR - INSPECTION |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 191 | AIR CONDITIONING COMPT AND FAIRINGS |
| 192 | AIR CONDITIONING COMPT AND FAIRINGS |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 52-30-00-860-001-A | Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
| TASK 52-30-00-860-002-A | Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
| TASK 53-35-13-000-002-A | Removal of the Quick-Release Access Panels from the Belly Fairing Structure |
| TASK 53-35-13-400-002-A | Installation of the Quick-Release Access Panels on the Belly Fairing Structure |
| SRM 533116 | (for corrective action) |
Subtask 53-31-00-010-126-A
A. Get Access
(1) Open the forward cargo-compartment door (Ref. AMM TASK 52-30-00-860-001).
(2) Remove the wing-to-fuselage access panels 191BB, 191EB, 192EB and 192FB (Ref. AMM TASK 53-35-13-000-002).
Subtask 53-31-00-110-140-A (1) Open the forward cargo-compartment door (Ref. AMM TASK 52-30-00-860-001).
(2) Remove the wing-to-fuselage access panels 191BB, 191EB, 192EB and 192FB (Ref. AMM TASK 53-35-13-000-002).
B. Preparation of the Inspection Areas
(1) Make sure that the inspection areas are sufficiently clean to do a satisfactory inspection of the area.
(3) Make sure that the inspection areas are dry before you continue.
4. Procedure(1) Make sure that the inspection areas are sufficiently clean to do a satisfactory inspection of the area.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
(2) If necessary, clean the inspection area with the Non Aqueous Cleaner-General - - (Material No.08BAA9) and a Textile-Lint free Cotton - (Material No.14SBA1) . (3) Make sure that the inspection areas are dry before you continue.
Subtask 53-31-00-220-070-A
A. Detailed Inspection
(1) If necessary, use the FLASHLIGHT and/or the MIRROR - INSPECTION to do the detailed inspection.
(2) Do a detailed inspection of the lower part of the vertical struts (200 mm from the bottom) on the aft face of the pressure bulkhead at Y= +/-765 mm (2 places).
(a) For A320, A319 and A318, do this at FR35. Look for:
5. Close-up(1) If necessary, use the FLASHLIGHT and/or the MIRROR - INSPECTION to do the detailed inspection.
(2) Do a detailed inspection of the lower part of the vertical struts (200 mm from the bottom) on the aft face of the pressure bulkhead at Y= +/-765 mm (2 places).
(a) For A320, A319 and A318, do this at FR35. Look for:
- Cracks
- Corrosion.
- Cracks
- Corrosion.
NOTE: If necessary,refer to the ASRM SRM 533116 for the correct repair procedure.
Subtask 53-31-00-410-123-A
A. Close Access
(1) Install the wing-to-fuselage access panels 191BB, 191EB, 192EB and 192FB (Ref. AMM TASK 53-35-13-400-002).
(2) Close the forward cargo-compartment door (Ref. AMM TASK 52-30-00-860-002).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Install the wing-to-fuselage access panels 191BB, 191EB, 192EB and 192FB (Ref. AMM TASK 53-35-13-400-002).
(2) Close the forward cargo-compartment door (Ref. AMM TASK 52-30-00-860-002).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Lower Part of Vertical Struts on the Aft-Face of the Pressure Bulkhead