What was found
FUSELAGE AFT TAIL CONE AREA UPPER SKIN STRUCTURE, BS 1520, CANTED DOUBLER AND SKIN CRACKED AT LONGERON 3R. OEM APPROVED REPAIR AS PERMANENT, SECTION I COMPLETED IAW ER/A 517836-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE AFT TAIL CONE AREA UPPER SKIN STRUCTURE, BS 1520, CANTED DOUBLER AND SKIN CRACKED AT LONGERON 3R. OEM APPROVED REPAIR AS PERMANENT, SECTION I COMPLETED IAW ER/A 517836-14.