Service difficulty report · Skin · Airbus A300B4203

Difficulty date
January 18, 2006
Submitted
June 21, 2006
Operation
Air carrier
Aircraft
N821SC
Make and model
Airbus A300B4203
Aircraft serial
211
Aircraft time
50,653 hours, 20,839 cycles
Part
Skin
Condition
Corroded
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

DURING INSPECTION, FOUND 3 AREAS OF CORROSION ON FUSELAGE SKIN BETWEEN S26R AND S27R FRAME 58 - 60. REPAIRED PER AVBORNE REPAIR REF 25599-3-01-18-06, (AIRBUS REPAIR DESIGN APPROVAL SHEET RAS/DAHM/40204/2006) REMOVE FASTENERS, SMOOTH BLEND CORROSION, HFEC AND ROTO-TEST TO CONFIRM AREA IS DAMAGE FREE, FLAP PEEN PER SRM 51-40-19 REINSTALL FASTENERS AND RESTORE SURFACE PROTECTION PER SRM 51-40-12.

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