What was found
EXFOLIATION CORROSION ON INNER FUSELAGE SKIN STA Y=1209 BTW LONGERONS 30 AND 29RT. CORROSION WAS REMOVED AND REPAIR PIECES WERE FABRICATED AND INSTALLED IAW ERA480772-14 REV ORIG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXFOLIATION CORROSION ON INNER FUSELAGE SKIN STA Y=1209 BTW LONGERONS 30 AND 29RT. CORROSION WAS REMOVED AND REPAIR PIECES WERE FABRICATED AND INSTALLED IAW ERA480772-14 REV ORIG.