Service difficulty report · Skin · Airbus A300B4203

Difficulty date
January 13, 2004
Submitted
January 26, 2004
Operation
Air carrier
Aircraft
N365DH
Make and model
Airbus A300B4203
Part
Skin
Condition
Damaged
Location
Fuselage
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

REPAIR AT RIGHT FUSE FR19 STR 23R GOUGED. REMOVED EXISTING DOUBLER AT RIGHT FUSE FR19 STR23R IAW A300 SRM 51-30-30. SMOOTHED OUT FUSELAGE SKIN SECTION NEXT TO DOUBLER AREA AS PER A300 SRM 51-40-11. MAXIMUN MATERIAL LOSS-.011 ORIGINAL THICKNESS 0.63 FOUND TO BE OUT OF LIMITS PER A300 SRM 53-10-00 DIAGRAM 601 PG 610. REMOVED PANEL AT END CARGO COMP AND E&E COMP RT FOR ACCESS TO FUSE REPAIR AS PER A300 SRM 51-30-30. HFEC INSPECTED AREA AT FR19 STR23R IAW A300 NTM 51-30-00 PART 1 NO DEFECTS NOTED. INSTALLED DOUBLER REPAIR AT RT FUSE FR19 STR23R AS PER A300 SRM. INSTALLED PANEL AT FWD CARGO COMP AND E&E COMP RT AS PER A300 SRM.

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