As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT STRINGER 21 RT BS 360 - 400 EXTERIOR FUSELAGE HAS LARGE CREASE SHOWING IMPRESSION OF FRAME & STRINGER. AREAS WERE FOUND TO BE OUT OF LIMITS IAW SRM 51-00-01. REMOVED DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION OF AREA, FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM 51-20-01, 51-40-02 & 53-00-01 PROCEDURE V AND DETAIL XII & XXIV.