As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TUL - FOUND CRACK IN FUSELAGE SKIN AT RIVET LOCATED BS 251.9 AND STRINGER 22L. REMOVED RIVET, CONFIRMED CRACK WITH HFEC. REMOVED 1 INCH DIAMETER AREA OF SKIN TO REMOVE CRACKED AREA, CONFIRMED CRACK REMOVAL WITH HFEC. INSTALLED DOUBLER PER SRM 53-10-3. (M)