DOC AIRBUS | AMM A320FDetailed Inspection of Fuselage Skin, between FR 21 and FR 23 LH and FR 17 and FR 18 RH, from Stringer 31 to Stringer 36
TASK 53-11-00-210-032-A
Detailed Inspection of Fuselage Skin, between FR 21 and FR 23 LH and FR 17 and FR 18 RH, from Stringer 31 to Stringer 36
Refer to the MPD TASK: 531172-01
DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 21 AND FR 23 LH AND FR 17 AND FR 18 RH, FROM STRINGER 31 TO STRINGER 36
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 53-11-00-941-080-A
Subtask 53-11-00-220-088-A
Subtask 53-11-00-942-088-A
[Rev.10 from 2021]
2026.04.02 06:28:43 UTC
Detailed Inspection of Fuselage Skin, between FR 21 and FR 23 LH and FR 17 and FR 18 RH, from Stringer 31 to Stringer 36
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 100
1. Reason for the JobRefer to the MPD TASK: 531172-01
DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 21 AND FR 23 LH AND FR 17 AND FR 18 RH, FROM STRINGER 31 TO STRINGER 36
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 InformationA. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 100 | LOWER HALF FUSELAGE INCLUDING RADOME |
| REFERENCE | DESIGNATION |
|---|---|
| SRM 51110001 | (for corrective action) |
| SRM 51220001 | (for corrective action) |
Fuselage Skin Between FR21 and FR23, Left Side, from STGR31 to STGR36Subtask 53-11-00-941-080-A
A. Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position:
Subtask 53-11-00-110-080-A - for the left side: at the zone 127,
- for the right side: at the zone 126.
B. Cleaning of the Structure
4. ProcedureWARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
(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. Subtask 53-11-00-220-088-A
A. Inspection
(1) Do a detailed inspection of the structure of the fuselage skin:
(a) corrosion damage:
- If you find corrosion damage, refer to the Structural Repair Manual SRM 51220001 for types, inspection, removal and corrosion protection.
(b) other damage (scratches, cracks, gouges, dents, creases):
- If you find other damage, refer to the Structural Repair Manual SRM 51110001 for damage classification and corrective action.
5. Close-up(1) Do a detailed inspection of the structure of the fuselage skin:
- for the left side:
from FR21 to FR23 between STGR31 and STGR36. - for the right side:
from FR17 to FR18 between the STGR31 and STGR36.
(a) corrosion damage:
- If you find corrosion damage, refer to the Structural Repair Manual SRM 51220001 for types, inspection, removal and corrosion protection.
(b) other damage (scratches, cracks, gouges, dents, creases):
- If you find other damage, refer to the Structural Repair Manual SRM 51110001 for damage classification and corrective action.
Subtask 53-11-00-942-088-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).