As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT SIDE OF FUSELAGE SKIN IS DENTED AND CHAFED AT LAP SEAM BS 950, PLUS 10", STRINGER 26L. CUT OUT DAMAGE AREA IAW SRM 53-30-3 FIG.14. FABRICATED REPAIR PARTS DOUBLER AND STRUCTURAL FILLER IAW SRM 53-30-3 FIG.14 AND 53-30-2 FIG.2. INSTALLED DOUBLER AND STRUCTURAL FILLER IAW SRM 51-30-2