As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MHV - DURING NDT INSPECTION OF AIRCRAFT PER SID 53.09.029 CRACKS WERE INDICATED IN THE FUSELAGE SKIN AT 5 RIVETS AT FS 69.550 APPROXIMATELY 15 INCH LEFT OF CENTERLINE OF THE AIRCRAFT. INSPECTED FOUND INITIAL REPAIR PER DRAWING SR09530239 WAS IMPROPERLY INSTALLED. RE-REPAIR ACCOMPLISHED PER SRM 53-04 FIG 12B. (M)