As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION INSIDE OF FUSELAGE ON ANGLE BETWEEN FRAMES 86 AND 87 AND STRINGERS 27R AND 28R. REMOVED AND REPLACED ANGLE BETWEEN FRAMES 86 AND 87 AND STRINGERS 27R AND 28R, INSIDE OF FUSELAGE REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.