What was found
CORROSION ON FUSELAGE SKIN BETWEEN FRAME 30-31, STRG 54 LT TO RT. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5314-95877 AND RAS/DABRE/7006101/2005 ISSUE A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FUSELAGE SKIN BETWEEN FRAME 30-31, STRG 54 LT TO RT. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5314-95877 AND RAS/DABRE/7006101/2005 ISSUE A.