As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C, ON REMOVAL OF BLIND FASTENER STRINGER FOUND DAMAGED (CRACKED) AT FUSELAGE HOLE STRINGER 26L AT BS 320. CRACK CONTAINED IAW SRM 53-10-3. HFEC INSP CARRIED OUT ON THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 FIG 4 &16 RESULT. NO DEFECTS FOUND CRACK CONTAINED. REPAIR CARRIED OUT IAW SRM 53-10-3.