As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHEM MILL CRACK IN FUSELAGE SKIN, BS 500B+5 OVER STRINGER 23 RIGHT. TRIMMED OUT CRACK AT BS 500B+5 ABOVE STR 23 RT IN AN AREA OF 1" X 4". HFEC VERIFIED NO CRACKS. INSTALLED REPAIR PER SRM 53-00-01 REPAIR 31. ASSESSED THE REPAIR TO BE A CATEGORY