As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME IS CRACKED BELOW CABIN FLOOR AND OVERWING ON LT SIDE BS 616 (REFMM53-11-89-801) REF NR13410-2400-0007. MAJOR REPAIR ACP'D. REMOVED DAMAGE AND VERIFIED WITH HFEC. INSTALLED A FILLER AND A REPAIR ANGLE PER MM 53-11-89-801.