What was found
FUSELAGE SKIN UNDER FRAME BS 333 IS CORRODED BETWEEN STRINGERS 26 - 27L. REMOVED CORROSION FROM SKIN AT FS 333 IAW SRM 51-21-06-001-001. RECEIVED AND COMPLIED WITH EA 32-2015-331, REV.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN UNDER FRAME BS 333 IS CORRODED BETWEEN STRINGERS 26 - 27L. REMOVED CORROSION FROM SKIN AT FS 333 IAW SRM 51-21-06-001-001. RECEIVED AND COMPLIED WITH EA 32-2015-331, REV.