As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME CRACKED AT STA 1580, RIGHT SIDE OF FUSELAGE BETWEEN S8RT AND S9RT IN CABIN. INSTALLED REPAIR PARTS AT STA 1580 RT SIDE OF FUSELAGE BETWEEN STRINGER 8AND 9 REF 53-00-07.DO A SUPPLEMENTAL INSPECTION 12000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR 50000 AIR FRAME CYCLES. WHICHEVER COME FIRST.