As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
OKC - FUSELAGE SKIN IS DENTED AT BS 999 BETWEEN STRINGER 13R-14R. A=1.8 INCH, Y=0.067 INCH, A/Y = 26.9. LOWER EDGE OF DENT PERIPHERY IS 1.2 INCH FROM SKIN LAP JOINT UPPER FASTENER ROW. CUTOUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A STRUCTURAL FILLER, EXTERNAL DOUBLER AND EXTERNAL TRIPLER IAW ASA EA 5330-02010. (M)