As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AN INSPECTION OF AN EXISTING REPAIR TO FRAME 73 AT STRINGER 15L ADDITIONAL DAMAGE IN THE FORM OF A .75 INCH LONG CRACK, WAS FOUND. REMOVED THE EXISTING REPAIR PERFORMED AN EDDY CURRENT INSPECTION TO CONFIRM CRACK ENDED AT A RIVET HOLE. FABRICATED AN L-SHAPE REINFORCEMENT AND INSTALLED INTO FIR AIRCRAFT. REPAIR DONE IAW MM REPAIR STATEMENT AND STANDARD MFG SRM PRACTICES.