As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WEAR MARKS ON THE FUSELAGE SKIN (KARMAN STRUCTURE AREA) BETWEEN FRAME 38.1/39 AND STRINGER 30/32 RT. REPAIR WITH SMOOTH BLEND OUT AND REINSTALLATION OF ORIGINAL OR OVERSIZED FASTENERS IAW EA 6-5314-103265 AND RAS/DA/BRE/7006916/2006 ISS "C".